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Flight Analysis Branch N74-70654 Unclas 00/99 16238 281989 MANNED SPACECRAFT CENTER HOUSTON.TEXAS April 22,1969 MSC INTERNAL NOTE NO. 69-FM-107 MISSION PLANNING AND ANALYSIS DIVISION VIEWS FROM THE SPACECRAFT DURING APOLLO 10 (MISSION F) MAY 18, 1969 LAUNCH DATE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION " :::-:-:.:-:-:. (NASA-TM-X-69732) VIEWS FROM THE :::::;::::::::SPACECRAFT DURING A1'OLLC 10 (MISSION F) :::::::::::jtU 18. 1969 LAUNCH DATE (NASA) 149 p " \

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Page 1: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

Flight Analysis Branch

N74-70654

Unclas00/99 16238

~PR 281989

MANNED SPACECRAFT CENTERHOUSTON.TEXAS

April 22,1969

MSC INTERNAL NOTE NO. 69-FM-107

MISSION PLANNING AND ANALYSIS DIVISION

VIEWS FROM THE SPACECRAFT

DURING APOLLO 10 (MISSION F)

MAY 18, 1969 LAUNCH DATE

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

"

:::-:-:.:-:-:. (NASA-TM-X-69732) VIEWS FROM THE:::::;::::::::SPACECRAFT DURING A1'OLLC 10 (MISSION F)

:::::::::::jtU 18. 1969 LAUNCH DATE (NASA) 149 p

"

\

Page 2: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

MSC INTERNAL NOTE NO. 69-FM-107

PROJECT APOLLO

VIEWS FROM THE SPACECRAFT DURING APOLLO 10(MISSION F) MAY 18, 1969 LAUNCH DATE

By Alfred N. LundeFI ight Analysis Branch

April 22, 1969

MI SSION PLANNING AND ANALYSIS DIVISION

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

MANNED SPACECRAFT CENTER

HOUSTON, TEXAS

Approved:C~ ~. ~Chari ie C. Allen, ChiefFlight Analysis Branch

APproved:.fld~~ 2k ~hn P. Mayer, Ctiiefr -ission Planning and Analysis Division

Page 3: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••'I'

Figure

1

2

3

4

5

6

FIGURES

Illustration of lunar orbit plane in year 1969 ­inclination angle (i) ~ 28°, right ascensionof ascending equatorial node (n) = 5° . . .

Su~ and moon location at major phases duringApollo 10 (Mission F) . . . . . . .

A schematic of the maneuver attitudes and lightingconditions for the nominal Apollo 10(Mission F) . . .. ....•...

Nominal Apollo 10 (Mission F) projected on a mapof the celestial sphere . . . . • • •

F mission nominal rendezvous

Translunar injection burn

(a) Begin TLI (g.e.t. = 2:33:17.7)(b) Middle of TLI (g.e.t. = 2:36:08.0)(c) End of TLI (g.e.t. = 2:38:59.5)

Page

26

27

28

29

30

323334

7 Translunar coast - constant field of view (earth)

(a)(b)(c)(d)(e)(f)(g)(h)

G.e.t. = 5 hours .G.e.t. = 10 hoursG.e.t. = 20 hoursG.e.t. = 30 hoursG.e.t. = 40 hoursG.e.t. = 50 hoursG.e.t. = 60 hoursG.e.t. = 70 hours

3839404142434445

.'

••

8 Translunar coast - variable field of view (earth)

(a) G.e.t. = 10 hours(b) G.e.t. = 20 hours(c) G.e.t. = 25 hours(d) G.e.t. = 35 hours(e) G.e.t. = 45 hours(f) G.e.t. = 65 hours(g) G.e.t. ~)75· hours

iii

46464646 .474747

Page 4: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

Figure

9 Translunar coast - constant field of view (moon)

(a) G.e.t. = 10 hours(b) G.e.t. = 20 hours(c) G.e.t. = 30 hours(d) G.e.t. = 40 hours(e) G.e.t. = 50 hours(f) G.e.t. = 60 hours(g) G.e.t. = 70 hours

Page

50515253545556

••

10 Trans1unar coast - variable field of view (moon)

11

(a) G.e.t. = 10 hours(b) G.e.t. = 20 hours(c) G.e.t. = 30 hours(d) G.e.t. = 40 hours(e) G.e.t. = 50 hours(f) G.e.t. = 60 hours

Lunar orbit insertion burn

(a) Begin Lor (g.e.t. = 75:45:43.2)(b) Middle of LOr (g.e.t. = 75:48:43.2)(c) End of LOr (g.e.t. = 75:51:44.7) ..

575757575858

606162 •

12 Lunar orbit phase

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)

(i)

Begin DOr burn - front window (g.e.t. =99: 33: 51) . . . . . . .. ...

Begin DOr burn - docking window (g.e.t. =99: 33: 51) .. .

End DOr burn - front window (g.e.t. =99: 34: 26) .... .....

End DOr burn - docking window (g.e.t. =99:34:26) .

Begin phasing burn - front window (g.e.t. =100:64:21) .. . .

Begin phasing burn - docking window (g.e.t. =100:46:21) . . .

End phasing burn - front window (g.e.t. =100: 47 : 03) .. ..... .....•

End phasing burn - docking window (g.e.t. =100:47:03) .

Descent stage jettison (end burn) - frontwindow (g.e.t. = 102:33:28) .

iv

64

65

66

67

68

69

70

71

72

••

Page 5: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

•Figure Page

(j) Descent stage jettison (end burn) - docking

• window (g.e.t. = 102:33:28) · · · · · · · 73(k) Begin insertion burn - front window (g.e.t. =

102:43:18) · · · · · · · · · · · · · · · · 74(1) Begin insertion burn - docking window

(g.e.t. = 102:43:18) · · · · · · · · · · 75(m) End insertion burn - front window (g.e.t. =

102:43:33) · · · · · · · · · · · · · · · · 76(n) End insertion burn - docking window (g.e.t. =

102:43:33) · · · · · · · · · · · · · 77(0) Begin CSI burn - front window (g.e.t. =

103:33:46) · · · · · · · · · · · · · 78(p) End CSI burn - front window (g.e.t. =

103:34:18) · · · · · · · · · · · · · 79(q) End CSI burn - docking window (g.e.t. =

103:34:18) · · · · · · · · · · · · · · · 80(r) Begin CDH burn - front window (g.e.t. =

104:31:42) · · · · · · · · · · · · · · · 81(s) Begin CDH burn - docking window (g.e.t. =

• 104:31:42) · · · · · · · · · · · · · · · 82(t) End of CDH burn - front window (g.e.t. =

104:31:45) · · · · · · · · · · · · · · · 83(u) End of CDH burn - docking window (g.e.t. =

104:31:45) · · · · · · · · · · · · · · · 84(v) Begin TPI burn - front window (g.e.t. =

105: 08: 57) · · · · · · · · · · · · · · · 85(w) Begin TPI burn - docking window (g.e.t. =

105:08:57) · · · · · · · · · · · · · · · 86(x) End TPI burn - front window (g.e.t =

105:09:13) · · · · · · · · · · · · · · · 87(y) End of TPI burn - docking window (g.e.t. =

105:09:13) · · · · · · · · · · · · · · · 88

13 Transearth injection burn

.' (a) Begin TEI burn (g.e.t. = 137:20:22.4) 90(b) Middle of TEI burn (g.e.t. = 137:21:52.4) 91

• (c) End of TEI burn (g.e.t. = 137: 23 :11. 3) · · 92

14 Post TEI

(a) G.e.t. = 137: 29 :11. 3 · · · · 96"(b) G.e.t. = 137:29:18.5 97(c) G.e.t. = 137:29:25.7 98

• (d) G.e.t. = 137:29:32.9 .:99

v

Page 6: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

•Figure Page

15 Transearth coast - constant field of view (moc;ml

(a) G.e.t. = 140 hours 102 •(b) G.e.t. = 150 hours . . 103(c) G.e.t. = 160 hours 104(d) G.e.t. = 170 hours . • 105(e) G.e.t. = 180 hours 106(r) G·.e.t. = 190 hours 107

16 Transearth coast variable field of view (moon).,

(a) G.e.t. = 140 hours 108(b) G.e.t. = 150 hours 108(c) G.e.t. = 160 hours 108(d) G.e.t. = 170 hours 108(e) G.e.t. = 180 hours 109(r) G.e.t. = 190 hours 109

17 Transearth coast - constant field of view (earth)

(a) G.e.t. = 150 hours 112 •(b) G.e.t. = 160 hours 113(c) G.e.t. = 170 hours 114(d) G.e.t. = 180 hours 115(e) G.e.t. = 190 hours 116

18 Transearth coast - variable field of view (earth)

(a) G.e.t. = 138 hours 117(b) G.e.t. = 139 hours 111(c) G.e.t. = 140 hours 117(d) G.e.t. = 141 hours 117(e) G.e.t. = 142 hours 118(r) G.e.t. = 143 hours 118(g) G.e.t. = 144 hours 118(h) G.e.t. = 145 hours 118(i) G.e.t. = 146 hours 119 ..(j) G.e.t. = 141 hours 119 •(k) G.e.t. = 148 hours 119(1) G.e.t. = 149 hours 119(m) G.e.t. = 150 hours 120(n) G.e.t. = 151 hours 120(0) G.e.t. = 152 hours 120(p) G.e.t. = 153 hours 120(q) G.e.t. .- 154 hours 121

vi •

Page 7: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

•Figure Page

(r) G.e.t. = 155 hours 121

• (s) G.e.t. = 156 hours 121(t) G.e.t. = 157 hours 121(u) G.e.t. = 158 hours 122(v) G.e.t. = 159 hours 122(w) G.e.t. = 160 hours 122(x) G.e.t. = 161 hours . . . · 122(y) G.e.t. = 162 hours 123(z) G.e.t. = 163 hours 123(aa) G.e.t. = 164 hours 123(bb) G.e.t. = 165 hours 123( cc) G.e.t. = 166 hours 124(dd) G.e.t. = 167 hours 124(ee) G.e.t. = 168 hours 124( t'f) G.e.t. = 169 hours 124(gg) G.e.t. = 170 hours 125(hh) G.e.t. = 171 hours 125(ii ) G.e.t. = 172 hours 125(jj) G.e.t. = 173 hours 125

• (kk) G.e.t. = 174 hours 126(n) G.e.t. = 175 hours 126(mm) G.e.t. = 176 hours 126(nn) G.e.t. = 177 hours 126(00) G.e.t. = 178 hours 127(pp) G.e.t. = 179 hours 127(qq) G.e.t. = 180 hours 127(rr) G.e.t. = 181 hours 127(ss) G.e.t. = 182 hours 128(tt ) G.e.t. = 183 hours 128(uu) G.e.t. = 184 hours 128(vv) G.e.t. = 185 hours 128(ww) G.e.t. = 186 hours 129(xx) G.e.t. = 187 hours 129(yy) G.e.t. = 188 hours 129(zz) G.e.t. = 189 hours 129(aaa) G.e.t. = 190 hours 130,.'

• 19 Entry phase

(a) 15 min prior to entry (g.e.t. = 191:35:32.2) 132·(b) 13 min prior to entry (g.e.t. = 191:39:32.2) 133(c) 11 min prior to entry (g.e.t. = 191:39:32.2) · 134(d) 9 min prior to entry (g.e.t. = 191:41:32.2) 135(e) 7 min prior to entry (g.e.t. = 191:43:32.2) 136

•(r) 5 min prior to entry (g.e.t. = 191:45:32.2) 137

vii

Page 8: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

Figure

(g) 3 min prior to entry (g.e.t. = 191:47:32.2)(h) 1 min prior to entry (g.e.t. = 191:49:32.2)(i) Entry interface (g.e.t. = 191:50:32.2)

viii

•Page

138139 •140

-'.,

••

Page 9: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

,,'

••

VIEWS FROM THE SPACECRAFT DURING APOLLO 10 (MISSION F)

MAY 18, 1969 LAUNCH DATE

By Alfred N. Lunde

SUMMARY

The purpose of this document is to visually depict various aspectsof the Apollo 10 (Mission F) lunar flight. Views of the earth and themoon as seen from the spacecraft are shown during the translunar andtransearth coast phases as well as the view from the spacecraft duringcritical maneuvers. The data should prove invaluable in assuring thecrew that maneuver attitudes are correct. All data presen~ed in thisreport are for the first opportunity, 72° launch azimuth, May 18, 1969launch date.

INTRODUCTION

The geometry of a lunar mission can be very difficult to visualize.The primary objective of this report is to provide views from the space­craft during Apollo 10 (Mission F) because a knowledge of how the space­craft should be oriented with respect to familiar objects visible fromthe spacecraft window would be invaluable for performance of the variousmaneuvers.

A detailed visual representation of Apollo 10 (Mission F) for theMay 17, 1969 launch date is presented in reference 1. Because ofthe I-day slip in the launch date, most of the data in reference 1 areno longer applicable to the Apollo 10 flight. A discussion of thetrajectory geometry and the general information are presented inreference 1.

In the figures for the lunar orbit phase section, the location ofthe planets Venus, Mars, Jupiter, and Saturn has been shown .

Page 10: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

2 •e.g.

CDR

CM

center of gravity

constant delta height

command module

SYMBOLS

•CSI concentric sequencing initiation

CSM command and service modules

DOl descent orbit insertion

EI entry interface

g.e.t. ground elapsed time

hE altitude above earth's surface

altitude above moon's surface

LOI lunar orbit insertion

LM lunar module

PTC passive thermal control

RE

radius from center of earth

~ radius from center of moon

SM service module

SEQ star identification number

TLC translunar coast

TLI translunar injection

TEC

~I

~I

V.1

transearth coast

transearth injection

terminal phase initiation

inertial velocity

••

Page 11: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

3

DISCUSSION OF THE DATA

The geometry associated with the Apollo 10 lunar mission ispresented in figures 1 through 5. A detailed description of figures 1through 4 can be found in reference 1. The nominal F mission rendezvousis presented in figure 5.

Translunar Injection Burn

The beginning, middle, and end of the TLI burn are shown infigure 6. The maneuver is executed in a heads down position. Thehorizon is in darkness until toward the end of the burn. The TLI burnplaces the spacecraft on its lunar trajectory so that at the end ofthe burn the velocity is 35 591 fps.

Earth and Moon Views During TLC

The earth is shown in figure 7 with a constant field of view.Because the earth gets quite small as the spacecraft progresses on itslunar trajectory, the earth with a variable field of view is presentedin figure 8. The purpose of the enlarged views of the earth is to showdetails such as continents and terminator. Because these views are almostidentical to the views shown on pages 60 through 77 in reference 1,only a few TLC variable field views are shown in this report. Thereader who desires to find out what portion of the earth is visible tothe crew every hour during TLC should consult the above mentionedpages in reference 1.

Views of the moon are presented in figures 9 and 10. Because ofthe earth-moon-sun geometry at this particular time, the moon will bealmost totally dark as viewed from the spacecraft on the approachtrajectory.

Lunar Orbit Insertion Maneuver

The beginning, middle, and end of the LOI burn are depicted infigure 11. There is a rather large yaw attitude component during this.burn designed to place the spacecraft in an orbit similar to that of thelunar landing mission. The crew are in a heads down position duringthis burn, and the burn is performed in a retrograde attitude to brakethe trajectory speed so that a lunar orbit may be achieved.

Page 12: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

4

Lunar Orbit Phase

Various 1M events after separation from the CSM and prior todocking again with the CSM are shown in figure 12. The view from thecommander's front 1M window and from the docking window are shownwith the correct burn attitude for DOl burn, phasing burn, 1M descentstage jettison burn, insertion burn, CSI burn, CDR burn, and the TPIburn. The reader should consult figure 5 for a better understandingof those views.

Transearth Injection Maneuver

As with TLI and LOI, the beginning, middle, and end of the TElburn are shown in the correct burn attitude. This maneuver is aposigrade burn designed to free the spacecraft from the lunargravitational attraction. The spacecraft attains a velocity of8958 fps at the end of the burn to return the spacecraft to earth inapproximately 54.5 hours.

Post-TEl Views

The four post-TEl views depict the view from the spacecraft asthe earth comes into view over the lunar horizon. The Southeast Asiaportion of the earth is visible at this time.

Transearth Coast

As with the translunar coast, the views of the earth and the moonare shown at various times during the coast period (figs. 15, 16, 17,and 18). During this coast period, approximately half of the earth andmoon are in sunlight as seen from the spacecraft. The spacecraftleaves the lunar gravitational sphere of influence at approximately148 hours g.e.t., at which time the velocity will gradually increaseuntil it reaches 36 309 fps at entry.

Entry

The entry phase is shown in figure 19. The SM is jettisonedapproximately 15 minutes prior to entry interface, and the CM is in aheatshield forward attitude. The angle between the spacecraft X-axisand the earth horizon is held at +31.7°, which can be monitored on the31.7° scribe on the window. The moon is visible during part of theentry phase. The entry REFSMMAT's were obtained from reference 2.

••

••

Page 13: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

5

(Most of the vectors needed to generate the data shown in this reportwere obtained from reference 3.)

CONCLUSIONS

An understanding of spacecraft attitudes with respect to the sun,earth, moon, and stars is particularly useful to verify maneuver attitudesnormally described by IMU gimbal angles. This information is especiallyuseful for Apollo 10 (Mission F) because IMU gimbal angles are referencedto several specific inertial orientations (REFSMMAT) instead of topreferred platform alinements.

This report has presented numerous figures which depict the viewfrom the Apollo 10 (Mission F) windows: star field, earth and moonterminators, and horizon orientations are included. This informationshould prove invaluable in assuring the crew that maneuver attitudes arecorrect .

Page 14: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

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Page 18: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

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Page 24: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

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Page 32: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

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Page 33: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

LUNAR ORBIT PHASE

••

25

~»»»»»»»»~

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Page 34: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

ECLIPTICPLANE

LINE OF INTERSECTION LUNAR,ORBIT PLANE TO ECLIPTIC

PLANE (ASCENDING NODE)

... DIRECTION OF PRECESSION...... IN ECLIPTIC PLANE

y

Figure I.-Illustration of lunar orbit plane in year 1969 - inclinationangle (j):::::: 28 0

I right ascension of ascending equatorial node (n) =5 0•

••

••

Page 35: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

27

«~»\Equatorial plane

Ecliptic plane

:;:;:;:;:;:;;;:;: Lunar plane:.:.:.:.:.:.:.:.:

• Equatorial plane

Ecliptic plane

Sun at EI (63°)Sun at TLI (55°)

Lunar and solarLi ne of nodes

••

Figure 2.- Sun and moon location at major phases during Apollo 10 (Mission F>.

Page 36: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

--LOI- - -TEl

28

NOTE: For all maneuvers crew in heads-downposition relative to the earth or moon

Begin

••

•Figure 3.- A schematic of the maneuver attitudes and lighting conditions for the

nominal Apollo 10 (Mission F).

Page 37: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

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Page 38: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

30

Figure 5. - F mission nominal rendezvous.

Terminal phase

••

••

Page 39: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••,,'

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31

Page 40: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

32 •SEC

)C

V

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22 ,!;)lA <=13~ ;13

984 1044 1041'112 13 ~

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RE

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20

10 10

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-20 -20

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(a) Begin TLI (g.e.t. =2:33:17.7).

•Figure 6. - Translunar injection bum.

Page 41: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 33

" '02 -too -..

6) 7]

1 10"2 ,

22 ~520 "11

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•-20

(b) Middle of TLI (g.e.t. = 2:36:08.0).

Figure 6.- Continued.•-20 -10 o

X, nd

10 20

Page 42: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

20

22 Z~ ~1 41 ., 63 73 " AD 10822 -11 '2 l' 21 J 12 J .8 .,;;2 =22 :l ., 1 -6 -1 =5 -8 .!

144 1t;Q 151 186 ~i5 10.4n :3 1 "4 -i6 11I; 7 1\ 10 11 -;0

hE =196 stat. mi.

Field of view =1000v. =24 267 mph

I

SEQ "II; 7~

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= 3613 n. mi.

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20

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Page 43: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

3')

TRANSLUNAR COAST

Page 44: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

! :..........

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••

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Page 45: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

37

»»»»»»>;2' EARTH VIEW~««14««««.

Page 46: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

•R

E=24019n.mi.

Vi =13 352 fps Field of view =40 0

hE = 23 681 stat. mi.

V. =9104 mphI

20 20

-10-10

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,

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•-20 -20

-20 -10 o 10 20

X, nd

Ca) G.e.t. = 5 hours.

Figure 7. - Translunar coast - constant field of view (earth).

Page 47: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 39

R =52 882 n.mi .E

v. =8541 fpsI

•7,D 79J

2J •2' 2S

797 IO~

1" •2.. 22

136 1111 • lit lit

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hE = 56 896 stat. mi.

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••

2020

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Figure 7. - Conti nued.

10 20

Page 48: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

RE=93 028 n. mi.

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>-

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.... 20

- 10

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Figure 7.- Continued.

I

10

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••

Page 49: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

• >-

20

10

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sie I~~ '~I 171• -, -_ 0, 2~ 17 I'

RE =123 687 n. mi.

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41

Field of view =40°

,Nunki'• •

hE =138 375 stat. mi.

V. =3260 mphI

20

10

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-20 -10 oX, nd

Cd) G.e.t. =30 hours.

Figure 7.- Continued •

10 20

-20

Page 50: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

""CC

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E= 149 206 n. mi.

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20 ~

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-10 I-

42

Field of view - 40 0

/Nunki•

hE = 167 742 stat. mi.

Vi - 2773 mph

- 20

- 10I

-<- 0

- -10

••

-20 ~

I

-20

I

-10

I

oX, nd

(e) G.e.t.:: 40 hours.

Figure 7.- Continued.

I

10

I

20

- -20

••

Page 51: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

•>-

51; •• a '71Il -.. 0y 2 a 20

R =171265 n. mi.E

V. 3557 fps

20 I-

10 r-

o -

-10 I-

43

Field of view =40 0

/Nunki• •

h =193 127 stat. mi.EV. =2425 mph

I

-20

; 10

• 0

• -10

-<::s0.

••

-20 I-

l

-20 -10

l

oX, nd

(f) G.e.t. =50 hours.

Figure 7.- Continued •

I

10

I

20

- -20

Page 52: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

44

SEQ "1 871X ... U., 23 Z2

RE

= 190 809 n. mi.

V. = 3182 fpsI Field of view =40 0

-r "'i , i , , ii' i , , , , • , i , , • if' , i , ,

hE =187 368 stat. mi.

V.= 2170 mphI

••

20

10

o

-10

-20

-20

•Nunki./

-10

oX, nd

10 20

20

10

o

-10

-20

-< •

•(g) G.e.t. = 60 hours.

Figure 7. - Conti nued. •

Page 53: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

20 - . - 20/" Nunki

~10 I- - 10

••

• -0s::::..>-

SEQ e~~ Abl 871 "0• -ZZ -Ib -12 1&y 23 lR 20 _ZI

RM

= 15 709 n. mi.

V.=4031fps. I

o ~

-10 I-

Field of view = 40°

hM =16 997 stat. mi.

V. =2748 mphr

- 0

- -10

-<..

••

-20 -

I

-20

I I I

-10 0 10

X, nd

(h) G.e.t. = 70 hours •

Figure 7.- Concluded.

- -20•

I

20

Page 54: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

46 ••

hE = 103 440 stat. mi.

Vi. 4043 mph

X, nd

(bl G.e.t. " 20 hours.

RE " 93028 n. mi.

Vi" 5930 Ips Field of view. 6"......-~~~~~~--.-~~~~-

hE. 56 896 stat. mi.

Vi" 5823 mph

X, nd

Field of view s: 9 D

Ca) G.e.t. =10 hours.

RE " 52 882 n. mi. IVi" 8541 fps

:< :<-g it "~,,:

RE " 109163 n. mi.

Vi" 5275 Ips Field of view = 4°

hE" 121 661 stat. mi.

Vi" 3597 mph

RE=136 957 n. mi.

Vi =4390 Ips Field of view = 3°

hE =153 646 stat. mi.

Vi = 2993 mph

X, nd

(c) G.e.t. = 25 hours.

X, nd

Cd) G.e.t. =35 hours.

Figure 8.~ Translunar coast - variable field of view (earth).

••

Page 55: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 47

•RE =160 600 n. mi.

Vi =3793 fps Field of view = 3°

hE .. 180 853 stat. mi.

Vi" 2586 mph

;<it

(e) G.e.t. c 45 hours.• RM = 27 254 n. mi. hM=30284 stat. mi.

Vi =3844 fps Field of view =30 Vi = 2621 mph, " " " "~~.......:-;.:.;::,.:.;~::;:..;:...~~~~~........,

X. nd

R = 3055 n. mi. hM

= 2436 stat. mi.

VM=5591 Ips V. = 3821 mph

"":'i-'~~~~=~~~....'F!:;i~el~d~ofC,'v~iew~=:..=.3°~~~~_Ih-~~~~, ,

;<;<~

~

~

~

it,::

•Figure 8.- Concluded.•

X, nd

(f) G,e.t. =65 hours.(g) G.e.t... 75 hours.

Page 56: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

~;;;;;;;;;;»»»4

~<~~~<~;~;««««:

Page 57: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

SEQXy

ISU lab 20521 a II

-17 -21 -3

50

2U7 222 23020 21 -20

!> 9 -17

2312

-I

2'18 2bc; 270-7 -2-' 1'1-3 -9 17

271~

12

2(; I

-IIb

301-21

8

••

RE=52 882 n. mi.

v. =8541 fpsI

20 -

Field of view = 40°

hE =56 896 stat. mi.

v. =5823 mphI

- 20

10 ~

o ~

V Betelgeuse

-10 """'

capella~

- 10

•• - 0

..-<• ~

- -10

Aldebaran~

•-20 ~

I

-20

I

-10

L

oI

10

I

20

- -20

•X, nd

(a) G.e.t. =10 hours.

Figure 9.- Translunar coast-constant field of view (moon). •

Page 58: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

RE=93 028 n. mi.

v. =5930 fpsI

hE = 103 440 stat. mi.

V. =4043 mphI

••

SEQ I""II 16y -2U

I~C 186

21 0-II -18

2059

o

51

207 222 23D17 17 -20I I l!a -17

Field of view = 40°

2 3 1a2

2 .. 11_9

-I

2 7 01021

~ 71 211

l -I"1ft 7

20 -

•- 20

capella~

- 10

• ,>-

10 I-

o ~

• • - ,-<.o::Ic..

-10 L- - -10

Aldebaran~

••

-20 I-

I

-20

I

-10

1

oX, nd

t

10

I

20

- -20

•(b) G.e.t. = 20 hours.

Fi gure 9. - Conti nued •

Page 59: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

Field of view =40°

RE=123 687 n. mi.

V. =4782 fpsI

hE=138375 stat. mi.

V. =3260 mphI

,>-

S[,~ l'i'! ISnx I it 20y -16 -7

20 I-

10 I-

o I-

-10 I-

lSi I db 2"52 'i [1 7

1 -1,<;, 3

52

207 222 230 23\ 2'i8 270I~ l'i -20 -2 -10 6l'i 18 -16 'i 0 2'i

capella~

271 281o -17

18 8

- 20

- 10

:-. 0

- -10

-<

••

Aldebaran~

-20 ~

I

-20

I

-10

I

oX, nd

sun~

I

10

20

- -20

•(e) G.e.t. =30 hours.

Figure 9.- Continued.

Page 60: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 53

Sl:.lij 1'1" I!)U I !) I 18 b 20!) 207 222 HO Ul 2'" 2713 271 III~ 10 20 2'1 i.1 7 IS 1'1 .20 .2 _10 I» 0 _I'

•y -Ie ·7 I -16 J 1'1 18 ·1. " 0 2" 18 •

RE= 149 206 n. mi. hE = 167 742 stat. mi.

V. = 4067 fps Field of view =40 0 V. =2773 mphI I

i.

20 I-

10 -

o ~

-10 ~

•capella~

o

- 20

- 10

-<- 0'

~c..

- -10

-20 -

Aldebaran~

sun~ .

- -20

...

••

I

-20

I

-10

I

oX, nd

(d) G.e.t. =40 hours.

Figure 9.- Continued •

I

10

I

20

Page 61: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

Field of view = 40°

hE:: 193 127 stat. mi.

v.:: 2425 mphI

SEQ I~~ ISO lSIX IS 17 21Y -12 -2 "

RE=171265 n. mi.

v. :: 3557 fpsI

Itl/, 2nS-, ~

-1:1 6

207 22210 '1IA 22

230-21-16

231 2~8

-S -13~ I

271 281-s -2120 ,

••

20 .- ~capella - 20

10 .- - 10

!

-c e· -< •s::: 0..

0 - - ~..>- c..

-10 ~

Aldebaran~

-20 -

sun"'@

- -10

- -20

I

-20

I

-10

I

oX, nd

I

10

I

20

..

•(e) G.e .t. =5 0 hours.

Fi gure 9.- Conti nued.

Page 62: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 55

s~w I .... I So I!>I IAl> lll5 207 222 l30 231 2'18 271 211II IS 17 21 -I .. 10 9 _21 _5 _13 .5 .21

• ., -12 -2 II -13 6 18 22 -Ill 6 1 20 ,

RE=190 809 n. mi.

V. =3182 fpsI

20 ~

Field of view =40°•

capella~

hE =215 619 stat. mi.

V. =2170 mphI

- 20

10 ~ - 10.

• •"'C -<t:0 - - 0 .... ;j

>- a.

..

-10 I"'"'

-20 ~

I

-20

Aldebaran~

. "

I

-10

I

oX, nd

sun~

I

10

I

20

- -10

- -20

•(f) G.e.t. =60 hours.

Figure 9.- Continued.

Page 63: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

-20

-20 -10 oX, nd

(g) G•e .1. = 7 0 hours .

Figure 9.- Concluded.

10

20

-20

••

Page 64: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• .57

hE =103440 stat. mi.

Vi =4043 mph

hE = 167 742 stat. mi.

Vi = 2773 mphField of view =2°

Fi~ld of view:c 1 0

Cbl G.e,t, = 20 hours.

RE

= 149206 n. mi.

V. = 4067 fpsI

RE

= 93 028 n. mi.

V. =5930 fpsI

hE = 56 896 stat. mi.

V. =5823 mphI

Field of view = 1 0

(0) G.e.t. = 10 hours.

RE = 52 882 n. mi.

Vi =8541 fps

RE = 123 687 n. mi" hE = 138375 stat. mi.

,...,.-V.:-i ~=~4~7~8_2~f~P~S~~~~~~ ::~I~O~f~v~ie~.:'. 2', • , , ~i~=~3~2~6~__m~Ph~~~..,

~

::<=.< =,,:

~=~

• X, ndY, no

::<

(d G.e.t. = 30 hours. Cd) G.e.t. = 40 hours.

•Figure 10.- Translunar coast - variable field of view (moon),

Page 65: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

R E=

171

26

5n.

mi.

V;=

35

57

fps

Fiel

dof

view

=2°

hE=

19

31

27

stat

.m

i.

Vj=

24

25

mph

RE

=1

90

80

9n.

mi.

V;=

31

82

fps

Fie

ldof

view

=4°

hE=

21

56

19

stat

.m

i.

V.=

21

70

mph

I

-g ,:

X,

nd

CelG

.e.t

.=

50

hour

s.

:;< ~ 0.

~,

nd

enG

••.t

.=

60

hour

s.

:;< ~ 0.

Vl

OJ

••

Fig

ure

10

.-C

oncl

uded

.

••

Page 66: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

59

Page 67: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

60 •"it tJ ".)!, I," \ r,bq 5/'n '.II'f t;9Y ~IO 03'1 6'11 b'lS b!:>1

X 'j -JO .;; J :'f -l~ -.l:S \\ ;a -In -\Fl 17y -?'I -11 [I -, 't II '+ -s -'I 7 IS -I

JI. 'I 061J U8 6'HJ /1'" 713 1'15 7 .... 1 ' 755 759 •~ -16 -1'1 19 -', _ r, 1 t~ -,., 2'1 -'f

v 10 13 .. I 1 1 " ; J [ " 10 7.U

•-20

20

-10

Denebola,

hM =102 stat. mi.

'~~;~B~~~lil··.~,m~h,R

M=1028 n. mi.

V, =8251 fpsI

, iii iii' i i

20

-20

-10

10 10•

" •"• ""'C '0 -<!::

0 0~

~~

>- • c..•

(a) Begin LOI (g.e.t. =75:45:43.2).

-20 -10 oX, nd

10 20

•Figure 11.- Lunar orbit insertion burn.

Page 68: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

2020

\

• 61

liQ ,~!) ,4Q ,,1 56$ '70 5'7 "0 ,.' to-X 1 22 -p -I ;;4 2. i! -.1' -12y -~o "'2~ ·~O r.7 "'11 c16 "'15 0 -u

• iU 610 6~96

4! 651 160 6'~ ;-t 1ttX 8 i' -! 1- "'18 l' 16 as.y -6 ..5 10 -2 11 , •RM =1001 n. mi. hM = 71 stat. mi.V. = 7013 fps

Field of view = 100 0 V. =4782 mphIIiii iii ii' • i i , , • i , , , , i , • , , , , • i , i i i i , , , ,

• 1010 •

./

• ;I'./

'8 rAlphecca

-<'"t:l

0~

c 0 •::l

~

0->- ..•

-10Alka~d,

-10

Gienah J

•.

• -20 FDenebola-20

-20 -10 0 10 20

X, nd

I • (b) Middle of LOI (g.e.t. = 75:48 :43.2),

Figure 11.- Continued.

Page 69: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

62 •SEQ ~J~ 5a :~~

566 5;7 !:80 ,82 !589 592 "5 60. ~n tt3 9 6:~ •X -2 -19 ZC 11 -1 -22 20 -16 18 Hy "20 -22 -10 -6 -1 7 "1!5 -11 1 -15 0 -12 I -6 2

RM =997 n. mi. hM =67 stat. mi.

V. =5485 fps Field of view =100 0 V.=3740mphI I

20_...

/"Gienah

20

-10

10 10

•,/,/

,/

-0 '0 -<c 0 .... 0 ~>- • 0..

-20 renebola

(el End of LOI (g.e.t. =75:51:44.7>.

-20 -10 oX, nd

•Figure 11.- Concluded.

--- -----

Page 70: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

63

LUNAR ORBIT PHASE

Page 71: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

o

-20

-10Castor

POIIUX~

"=procyon

RegUIU~~·

••

o

-20

64 •~t. Q it71 281 ,)01 HZ 3'4' 3S. H2 31' H7 ,)81 "21 .... g .. 73 "iU

It 2'4 17 12 -I't 17 3 1'1 -2U -12 -2'1 .. 23 -7 1 i

1 -I' -2'1 -23 -2'1 -13 -49 -13 -1' -19 -I' -13 •• 0 1

SEQ ~u7 ~u9 !il1~ ~J~ ~'tU ~~1 Ii •• !"a7U S77 !iI¥U ill !"aU S9) !"a'SX U it't .1 U ;,r:u -I. -2U .., 4/1 1 I .a 21 -IS -21 •Y It 9 *' I I 1.1 I I 12 1. U 19 2U 20 20 111

SEQ .0'1 1081X III -!I

Y 23 lU

RM

=996 n. mi. hM

=67 stat. mi.

Vo = 5349 fps Field of view =1000Vo =3647 mph

II

Spi~a,Alkaoid-'

• 2020 •

Denebola"JUPit~r, .

10 '-Gienaho• 10 ••

-10

,>-

• •

(a) Begin 001 burn - front window (g.e.t. =99:33:51).

Figure 12.- Lunar orbit phase.

-20 -10 oX, nd

10 20

Page 72: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

65·

St. .. !I'Ir. !l°1 ~60 fto9 ~7'1 ftU it;) 119~ 199 olD '1 7 '21 'Z'I ''IIIt -2J -2'1 -9 -21 -0/" -13 0 -, ·2D U -ZZ -1& 17 -lly .1f. - I J -2'1 -J" -IU -10 -21 -II -, -21 ., -12 -I' -.

SEQO'tJ o .. ~ Oil '~!I OOU 073 ,Ill "U 70 U 717 71' 72'1 7H 7.. JX -.t1 -1~ 21 (J -12 .. "10 zz 12 ;'2 -I D -2 -zy -3 -0 -1~ -11 -, -(j -2 -, -. "Z ..2 -2 0 1

SEQ 7... 7!)1 7!1J 7ft7 7ft' I7U 7a 1 789 7'0 193 19~ 797 ·02 '03X 21 .. ,1 !it -2J ... J "U -, -u -7 17 "IU •• &JY -~ 2 1 .. J ~ 7 .. , • , 8 , i

SEQ I:IJo 1:1 .. 1 ...... 1:101 811 'ilJ lulUX -J -0 -I -2 -.. -~U ·1Y 1 J I J 1'1 I 1 17 19 J

RM= 996 n. mi. hM

= 67 stat. mi.

V. = 5.349 fps V. = .3647 mphI Field of view =1000 Il' ~~1l~:1I1~' O. o. 0 OJ

-<o ..:::ICo

20

10

-20

-10

20

Alphecca",

Rasalhag~e ./

10

20'-Peacock Nun~i:,

.. •

10•• ••

•'Atria • ja.r:,,-

"'C •C 0 Antar~s/· •-; . ••'-Ri9il

• ••Beta Crucis •

-10 •Menkent,

•• •

•-20

Spica,

-20 -10 0

X, nd

••

Cb) Begin 001 burn - docking window Cg.e,t. =99:.3.3:51>,

Figure 12,- Continued.

Page 73: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

66 •SEQ ;'! 1 c 1 301 3 4 2 34c; "c;

~6" ~ 7f 377 JEll -27 4-0 47"5 4.,,0 507X i:'-' , I 1? " 14 17 - ~ 14 -2e "12 -24 -23 -7 . 5 22"Y-1; .. ')4 -23 :024 -13 "'19 -1~ "H -1 9 -19 -1 3 -8 n 1 9 •SEQ ~r')9 c;l"i 5'35 54n 551 56~ 5,0 r:;7Z !5" ii ~II; 592 :9) 595 604 lCR1

X ::,4 "5 0 2,., -16 -20 -9 21 i l' -, ~1 -1~ -21 18 .5Y 9 I~ 11 1) 11 1? 1- 6 111 19 2n ~r ?~ 1/1 7.3 1('

RM=996 n. mi. hM=67 stat. mi.

V. =5278 fpsField of view =100 0 Vi =3599 mphI

~r-r -... -,--,.--, j . , , , , , , • i •

_..rSPica AlkaidJ20 • 20~

~

••

-20

-10

!

-. 10

•-<..0 :::3

0..

20

~PolluX

CastorJProcyon

Jupiter rDenebola_/ - .r

'--Regulus

••

.

Figure 12.- Continued.

/Alphard

(c) End 001 burn .. Front window (g.e.t. =99:34:26>.

-20L-A.............~.....................~...........................-ll....................~'~.-I-l.-~_L ~.........-...........................IIL......'...................,-J'.....·.i..i.....' ....-'-'-..........~

-10 0 10

X, nd

o

10

-10

-20

..>-

Page 74: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 67

SEQ =41'; ~ I' 1 566 569 574 5"9 C;9 :3 ;;9c: !599 610 61 7 621 624 641 6.3.. ..X -V -?41 -9 -21 -24 °13 0 .. ~ '"20 16 -22 "11 l' -12 '"21

-1'3 ~U -2. -14 -le "'16 -21 -18 -9 -21 -~ -12 -1~ -It -3YSEQ 645 ~51 655 66n 673 68~ 6°0 ;00 7i? 'i' 72 4 7"16 743 745 751

X -1 5 21 C -12 4 -10 '2 12 -, -1" n -;2 -2 21 -)

Y -6 ~15 -11 -6 -8 -2 -9 "6 -, -, -? 0 1 =2 2

• SEQ 7"i) '57 75Ci 770 71'1 78 9 79 0 79, 795 797 8n2 "0:3 8'36 8411 &44X 5 ~,"S -f :5 -16 -7 -1:3 -7 17 -10 -8 1) -3 -~ -1Y 1 4 :! ~ 7 " 7 q 6 8 9 II 13 13 14

SEQ 1161 871 t n8"X -2 -41 ~1

y 17 :;7 '3

RM =996 n. mi. hM =67 stat. mLv. =5278 fps v. =3599 mphI I

Page 75: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

68 ••

20

-20

-10

hM

= 17 stat. mi.

v. = 3761 mphIField of view = 100 0

RM

= 954 n. mi.

v. = 5516 fpsI

20

-20

-10

10 10

•"0

0~

t:: 0 :::~ a.

>-

Figure 12.- Continued.

(e) Begin phasing burn - front window (g.e.t~ =100:64:21).

-20 -10 oX, nd

10 20

Page 76: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

2010oX, nd

-10-20

• 69Sl.Q SIIS S61 h9 S711 sa' sn '" .17 u. .,.. '.. • .. .1 ... 5 .i.

x -22 -Z3 ·zu ·211 -.2 •• .. ' .22 ·.0 Ii ·.2 -,. •• 5 20y ·7 ·3 ... ..z •• •• 0 , •• ., • I .1 ••

S[lil ... ..0 673 "1 ''0 700 717 7.' 7ZIt 736 ,-.a ,... 75. 71.)X U "12 II ·.0 Z2 12 .,~I 0 ., -, 21 • .1 •• y

CI 3 1 7 0 3 • • I 10 II , U IISEQ 757 75' 770 71. 71' 790 79,) 7U- 797 10Z ,03 'u I". .....X "'II -. 3 -17 ·7 •• 11 ·7"

-10 ·1 .11 ·11 ., ·1Y 12 III 16 U II .7 II I' II .. 11 211 'II IiSEQ 1010

X ••Y I .1

RM=954 n. mi. hM =17 stat. mi.

V. =5516 fpsField of view =1000 V. =3761 mph

I I

20 20•.. • ••

~

Rasalhague,

• • 'rMars

'-Atria Antares, •10 10.' . •

• •

. '-Ri9il •• ••-c • -<c

Alphec~a~ 0..0 • ::J

... • Menke~t""- •>- c..

'- Beta Crucis•• • •• • Arctur~s "-

-10 -10

• -20 -20

•(f) Begin phasing burn - docking window (g.e.t. =100:46:21).

Figure 12.- Continued.

Page 77: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

(g) End phasing burn - front window (g.e.t. =100:47:03>.

20

10

o

-10

-20

RM

= 955 n. mi.

V. =5680 fpsI

-20

70

X, nd

10

hM

=19 stat. mi.

V. =3873 mphI

20

20

10

o

••

••Figure 12.- Continued.

Page 78: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

71,:>7" !589 5'5 ~99

;~~ 621 624 A4i '43 '~'5-2" -12 -6 -1' -10 15 -1 -21 -1'5-2 ;:6 -8 " ~ '''1 "9 1 5 :51!7) 61\8

6~~ 'ii.,.,

71" '24 ;3t .,4' '~54 -10 !2 -1 0 -, ., 211 7 0 :5 ~ a 8 1" ii 6'59 "0 781 7~~ 79 0 79) 79, 797 802 8rJ3.;;~ 3 -1' -7 -1 4 -7 1" -10 .." 1~14 16 16 H 1 7 18 16 18 l' 1 8

10"0-113

20

••

/Atria • r Mars

• •10 Antares . .

·rRigil

••-c

/B~taCrucist: 0 /Menkent Jr..~>-

Alphecca~-<..

20

o

10

hM=19 stat. mi.

V. = 3873 mph

"":""""'l

.Rasalhague.,

•Field of view =100°

• I " ._ i I •••••••• i

•!I"<

SEQ !5~~ 5~3 569X -~2 -2 -20Y =1 -;5 "6

SEQ 6~~ 6556~~

• 'X 0 -tY -6 0 ::5

SEQ 751 75) 7':>7X -J 5 -24Y 1~ 11 12

SEQ Ry> 8~1 ~44

X -" -6 -1Y 2" ?4 25

RM=955 n. mi.

V. =5680 fpsI

••

-10

-20

-20 -10 oX, nd

Arcturus,

10 20

-10

-20

(h) End phasing burn - docking window (g.e.t. =100:47:03>­

Figure 12.- Continued.

Page 79: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

72 •St., JII' HZ

II 21 UT -II -u •RM= 964 n. mi.

v. = 5631 fpsI Field of view = 1000

hM= 29 stat. mi.

V. =3839 mphI

20 20

••

-10

2010oX, nd

-10

(j) Descent stage jettison (end burn)- front window (g.e.t.= 102:33:28).

Figure 12.- Continued.

-20

-10

-20

10 10

•-<""C ..s:: 0 0.. :::I

>- 0.

Page 80: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 73

• SE., 136 l! If 1 81f1l 161 17.1 .'.011 '07 .te• 913 1001

,x .. 3 ,., ... 1 ,"2 ·If ,16 15 .10 .·19 .It., , 6 7 10 10 ,17 II .1& 13 U

RM= 964 n. mi. hM =29 stat. mi.

V. = 5631 fpsField of view =1000

V. = 3839 mphI I

-10

-20

-20 -10 o 10 20

-10

-20

•X, nd

(j) Descent stage jettison (end burn)- docking window (g.e.t. =102:33:28).

Figure 12. - Continued.

Page 81: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

RM = 946 n. mi. hM

= 9 stat. mi.

Vi = ~~ ~3i f; ~_. •--r- n- r-r--r-r-...,..F...,.i...:..,eI..:.,d..--o.,...f-rvi:.;.ew........=.......1 O.:.,.,O,:..o...............-r--T-.-......-..-V.;..i....=...,.3...,.9....,0..--2...m.....p..-h...,

20 20

-10

• • . J .

2010°-10.....O .. C •• I"",., .• I, .• ,.

-20

-10

-20

10 10

•o·-c -<s::: 0 ~

~ 0 :;]> Co

X, nd

(k) Begin insertion burn - front window (g.e.t. =102:43:18).

Figure 12.- Continued. •

Page 82: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

75

'II '4, 63 73 7!) lie 1WB III 112-IJ -23 -'I -I" -5 8 " -10 -II

11 7 1S 9 13 I" 10 !:> ..1 !;Ij 1110 }u!;, .i Hi UI lu7' 10'2

-<t " -s 1.l IS 0 Il' -~ -!;I -!;, -5 22 1:1

Field of view =1000............,--.-r,~r--r-, ....., ....... or,. iii • i • I , ,

hM=: 9 stat. mi.

V. =.3902 mphI

20

'-Saturn

• ..>-

10

o

Mirfa~J •

••

l~sun

'-Menkar 10

o-<..

••

-10

-20

AldebaranJ•

RigelJ

, , I , ' ....---.. I , I , I ,

-20 -10 0 10 20

X, nd

(I) Begin insertion burn - docking window (g.e.t. = 102:4.3:18).

Figure 12.- Continued.

-20

Page 83: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

76 ••

20

RM

=946 n. mi.

V. =5536 fpsI Field of view =100 0

hM=9 stat. mi.

V. =3775 mphI

20

••

-20

2010oX, nd

-10

Figure 12.- Continued.

(m) End insertion burn - front window (g.e.t. =102:43:33).

-20

-20

-10

10 10

•"0 -<C 0 0

.... :3

> c..

Page 84: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 77

SEQ If 22 J I "I 1f7 63 73 7S 80 Ice 1 I 1 11 2X -1'1 -~3 .~ .. -I J -23 -'I -1'1 -5 e 6 -Ill -IIY 23 Ie a 16 7 15 9 I J 16 Ie 5 II

• SEQ 12C I .... I :oc 15 I 186 215 221 Ie 7l; 10 1 2X -IS -2 -5 -" 2 13 IS r Iy I 2 1 0 -2 -~ -S 2, 15

20

RM

=946 n. mi.

V. = 5536 fpsI

Alpheratz/

Field of view = 100 0

./Vellus_o'

hM =9 stat. mi.

V. =3775 mphI

20

10

• Ul:: 0,>-

-10

./Mirfak ~sun

/Menkar

Aidebaran

•. /Rigel

10

o

(n) End inserti'l; hurn - dockinq window (g.e.t. = 102:43:33).

Figure 12. - Continued.

••

-20

-20 -10 oX, nd

10 20

-20

Page 85: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

78 •SEW 8~~ ~bl 871

l l'i 12 10Y -2'i -22 -22 •

20

-20

-10

20•

10o-10-20

RM

= 982 n. mi. hM =50 stat. mi.

V. = 5338 fps Field of view = 1000 V. = 3640 mph

I •••••••••••••••~I••••

-10

-20

10 10

•-<'J

..t:: 0 0 ~

.. c..

>-

X, nd

(0) Begin CSI burn - front window (g.e.t. =103:33:46>.

Figure 12.- Continued. •

Page 86: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 79

• 5£, .~~ "1 '~1,x III 12 1ty ·211 -22 -2~

20

-10

-20

hM = 50 stat. mi.

V. = 3670 mphI

RM=982 n. mi.

V. = 5388 fpsI

20

-20

-10

10 10

• -<...""00 ::3c:

0 c....>-

•(p) End CSI burn - front window (g.e.t. =103:34:18>.

Figure 12. - Continued.•-20 -10 o

X, nd

10 20

Page 87: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

80 •

Field of view = 1000

3(1 311' J" 2.2-2C , •• II

15 20 23 ,IahM

= 50 stat. mi.

V. =3670 mphI

SEQ 116 205 20 7 215X -2 5 10 ~13

Y 14 5 3

SEQ 214M 2~2 256 265

X t ,-12 -1' -7Y • 8 8 1t

RM= 982 n. mi.

V. = 5388 fpsI

221-15

14

~7t

1110

222,11

6

~71

710

231 aU:I .·~1

7 5

3Cl,-3,15

217 239-11 .~2C

7 5

all. a'"~111 ."11

7 1 •Procyo~/

20 20

./"Sirius

•-20

-10

•Betelgeus~,

10 10

rBellatriX·Elnath ./capella•. • •.

RigeiJ· -<,

"'C 0 0 ~

s::: c..

>-..

Figure 12. - Continued.

(q) End CSI burn - docking window (g.e.t. = 103:34:18).

-20 -10 oX, nd

10 20

Page 88: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 81

SEQ 7ftl 7ftS 757 759 770 781 789 790 nJ 795

X -.. 21 -22 -8 -I -18 -II -16 -I I •Y 15 -8 I 8 -2 II 0 II 17

• SEQ 797 .02 803 836 8"1 ..... 161 871 1010X -I" -13 S -12 -I" -10 -13 -15 -J

Y 2 .. 16 10 9 12 1.. I .. 3

RM

=981n.mi. hM = 49 stat. mi.

V. = 5391 fpsField of view =100 0 V. = 3676 mph

I I

20 RaSalhagUe~ 20

-10

20

. ,. ,

Figure 12. - Continued.

, I . . , I .-10 0 10

X, nd

(r) Begin CDH burn - front window (g.e.t. = 104:31:42)•

-20

'-Atria-10

-20

10 10•

• •-<

-c0 ~t: • 0

,>-

••

Page 89: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

82 •SEQ II 7 1S 2S .. 1 '0 .. .b7 '0' .33 no

X 13 6 -20 -II 1" 16 1" 10 -ZO ZetY 16 IS 3 1 1 Z.. -I. -16 -17 -II -3

SEQ .... "0 1001 1010 1028 10"1 10 .... 10'" 107. •X 10 -I -17 -2 .. -18 -11 15 • 0y -Z -7 -9 "'10 -6 "'I 9 7 ZO

RM=981 n. mi. hM=49 stat. mi.

V. =3591 fpsField of view = 100 0 V. =3676 mph

I I• , .. T-r", • i ••• : , , i , , , , , • I i

20Venu.s,

20/AIPheratz

•DiPhda~

10•

•'"0

0c:Fomalhau~, •..

/"Enif>

-10 •

/peacoCk.Altair""" •

•-20

10

..-< •0:::la.

.~

-20 -10 oX, nd

10 20

-10

-20

•(5) Begin CDH bum - docking window (g.e.t. = 104:31:42).

Figure 12.- Continued. •

Page 90: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 83

-20

-10

2010oXI hd

Figure 12. - Continued.

-10

(t) End of CDH burn - front window (g.e.t. =104:31:45).

-20

-10

-20

SEQ 7i1 7SS 7h 770 781 7., 7,0 7,3 1qSX -10 II -13 -6 -2 .. -17 -22 -17 S

• Y, 20 8 IS .. II 6 I I 2..

SEQ 7,7 'Oz '03 836 8"1 8 .... '61 .71 10'0

X -zO -II I -17 -19 -16 -I' -20 -,Y

, I I 2 .. 18 16 20 22 21 I I

RM =981 n. mi. hM =49 stat. mi.V. =5390 fps

Field of view =100 0 v. =3675 mphI I

/NunkiRasalhague

20 20

10 10

•"'0c::

0 0>- 5-

••

Page 91: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

84 •SEQ 7 IS 25 711 7" 1O) 13' ... 1 ..... "1-- 171 'o~

X 6 -21 -11 -I' 20 IS .... -, -I "2 -.. IIY Z'l 10 ZO -Z .. -23 -2 .. -22 -21 -21 -II -17 .,

SEQ '07 '0' 933 'SO ,a .. 99o 1001 1010 1021 10"1 10.... 1"6 •X III 10 "19 211 10 -I -17 -23 -18 -11 U •Y -7 -a -1O 3 6 2 -I -3 1 7 17 ..

. RM=981 n. mi. hM=49 stat. mi.

V. =5390 fpsField of view =100 0 V. =3675 mph

I I

20DiPhda,

20

••

10 • 10

Fomalha~t,Enif,

••

•• -<"'C

t: 0,

, • 0 ::;,

>- c.!

.Altai.r"". .

-10 /""Peacock •-10

(u) End of CDH burn - docking window (g.e.t.·= 104:31:45).

Figure 12.- Continued.

-20

-20 -10

• /""Nunki

••

oX, nd

10

Rasalhague~

20

-20

••

Page 92: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 85

•20

-20

hM=49 stat. mi.

Vi = 3676 mph

RM = 981 n. mi.

V. =5391 fpsI

20

-10

-20

10 10

•~ -<c:: 0, 0

>- c..

•(v) Begin TPI burn - front window (g.e.t. =105:08:57).

Figure 12.- Continued.•-20 -10 o

X, nd

10 20

Page 93: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

86 •SEQ J" .... 0 117,J 118e so' U5 535 1110 '11' III ." U'X .-.21 -10 0 II 23 , 6 211 -211 ,-' ., -12

Y -II ,-s elf -If -, 1, ,"3 18 II ~. u

SEQ 170 110 Sl2 589 593 &'. , 10 62 If '&I lOll •X ,I 20 I -Ilf 0 ., 15 1'1 22 1Y IS , IS 211 22 Z.. II 20 20 I

RM= 981 n. mi. hM

= 49 stat. mi.

V. = 5391 fps Field of view = 100 0 Vi = 3676 mphI

• '-SPica Arctur~s,.20 • 20

• •

10Jupiter 10

/Denebola• •

""C ~ -<c: 0

~

• 0~

::l

> c.

Alphard"•

RegUlu~/ •

-10 -10

-20 -20

•(w) Begin TPI burn - docking window (g.e.t. =105:08:57>.

Figure 12.- Continued.

-20 -10 oX, nd

10 20

Page 94: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 87

•20

-10

-20

hM= 49 stat. mi.

V. =3676 mphI

RM=9809 n. mi.

V. = 5413 fpsI

20

-10

-20

10 10

•~ -<s::: 0 0~ ::l

>- c..

•Figure 12.- Continued.

(x) End TPI burn - front window (g.e.t. =105:09:13),•-20 -10 o

X, nd

10 20

Page 95: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

88 •SEQ J17 ""0 1173 ..10 i07 lIS US S"O SIIS SSI 5.. It,X -II -10 a .. 2J 7 • 211 -Zit -7 -, ·ZIY -II -s -Il -Il -7 a I -3 II IS 18 ZI

RM = 9809 n. mi.

r-V~i...=..,....,.5..,4"""3...1....f.,..PS............,..,,...,.............~ _~i~l~ pfrv,i~w, =: ~ 9~o i

• SPiC~,

20

SEQXY

i701

II

58020

•582

•III

589-Ill

Zit

-.

!t93a

22

5ts-721l

610ISII

62 It1720

'SI lOll22 I19 •

hM

=49 stat. mi.

V. =3676 mphI

ii' , iii i , • i i •

•20

-10

,>

10

o

Alphard"

• •

10

•-<,0 ::s

c.

-•

-10

Figure 12.- Concluded.

(y) End of TPI burn - docking window (g.e.t. =105:09:13).

-20

-20 -10 oX, nd

10 20 ••

Page 96: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

Page 97: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

90 •~t;;Q ;'2 \ I "I '17 63 /1 7~ 80 10 8 11 1 I 1 ol 120 1'1'1 ISO I!> 1 IIle

X -/J -24 -1~ -l..\ -°1 -1.\ -'. 8 6 -10 -1 I -IS -2- -6 -Ill 2

y 'I -,. -, -'i 0 -j -I I -It -q -If -II -12 -13 -1'1 -17..

SU" olOf> 207 21<' al 222 2 30 231 233 2)7 23' ?'l<, ')'l~ 2">l 2!>2 2!.6

x -e - i I 1'1 I b -I J 8 -3 23 U 22 I 'l 13 (1 13 1 ~

Y -20 -olD -I" -18 -21 -22 -23- -17 -22 -I' -7.1 -22 -7.'i - 2;\ -V •R

M=996 n. mi. hM= 66 stat. mi.

V. =5349 fps Field of view =1000 V. =4758 mphI I

i i I I , i i , i i , i i i

2020

10 10

•"'C

• -<s:: •

0 II 0,

.. •>-~

• a.

• /,Menkar• •

-10 •/Mirfak

-10

••

-20

/""5 un<!> rAldebaran

rCapella •

• .r'Rigel• -20 •

Ca) Begin TEl burn Cg.e.t. = 137:20:22.4).

-20 -10 oX, nd

10 20

•Figure 13.- Transearth injection burn.

Page 98: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 91

IU -:i ~I13 15 8g 10' !U cUi 12& 1'. 1;i l'i 11' 201• -16 -7 :5 '-1 -1 •• "1 0 -.y 2 g -4 -1 1 -4 ..., '-10 -12 -12 "'1~ -1 4 "1' -20

• IU 20' 21' 221 22i 232 2~! 233 231 239 245 ,.- 2'2 21.• -14 12 1. -1 21 10 l' 13 11 11 "jY "'20 -18 -19 -22 -22 -23 .1'

-22 -1' -2, -22 -2] ''''22

RM=995 n. mi. hM=67 stat. mi.V. =6978 fps

Field of view =1000 V. =3647 mphII• i ••-r~T-i iii • i , • . , • i , , , • i , i , . , . i , , i i

20

10

20

10

"'C • -<s::::0 • • 0.; ~• c..

• /Menkar

-10 ••/"Mirfak'

-10

••

(b) Middle of TEl bum (g.e.t. = 137:21:52.4).

-20• /Rigel •

if5un

• '-Aldebaran

-20Capell.a" • •

/ Bel~atrjX •/Elnath •••

-20 -10 0 10 20X, nd!.

Figure 13.- Continued.

Page 99: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

92 •SUI 'I 22 J 1 'II '17 1a3 73 n 10 101 1 11 112 12U 1.... lltO 111II -,2 -2J -2'1 -12 -23 -'I -1'1 eft 7 • -lU -11 -li -2 -. -10y 9 a -3 I -'I U -.. -I 0 • i -9 -10 -12 -13 -1'1 -I'

:»E~ 1•• 20~ 2U 7 :l1~ 221 2./.",- 2Ju 231 U~ h1 2H 2'1, ,.., 2iZ 2U

l( 2 -. -12 1'1 I' -13 It -3 2.1 12 22 ar. U U 11 •y -til -21 -21 -1' -1' -ll -4tJ -2'1 -1 1 ·'3 -I' -22 _23 -2~ .2.1

RM

=998 n. mi. hM = 68 stat. mi.

........V....;.i-,=-,-8....9...,.5-,8-,f.....-p

S.----.--.,----,._ , _r.. T • Ei~ I~ ?f,v~e~ := .1,Q9-:-.-,---,----,---,,---.--.........,V-,!;.-=-r-,"T~--,~_O,....,8-r,-r~_phr-,...., ...,.,-,

••

•-<

o

10

20

-20

-10

20

10

_. /Rigel •

/ Bellatrix.•••

o

/Sun@ /Aldebaran

X, nd

/Elnath

-10

(c) End of TEl burn (g.e.t. = 137:23:11.3).

.rMirfak

Alpheratz~

-20

10

20

-20

•-c •s::::0 •, •

>- • ••

• .rMenkar

-10

Figure 13.- Concluded.

Page 100: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

93

TRANSEARTH COAST

Page 101: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 95

~ POST TEl "~"~»~>«««« «~«~erred

?',»»»>

••

Page 102: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

..>-

RM =1109 n. mi.'

V. == 8632 fpsI

.

Field of view =100

-

X, nd

Ca) G.e.t. =137:29:11.3.

Figure 14. - Post TEl.

hM=198 stat, mi.

V. =5885 mphI

••

••

Page 103: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

..:>

RM

=1113 n. mi.

v. =8622 fpsI

97

Field of view =10°

X, nd

Cb) G.e. t. =137 :29:18.5.

Figure 14.- Continued•

hM:I: 200 stat. mi.

v. =5879 mphI

Page 104: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

,>

RM

:= 1117 n. mi.

V. =8612 fpsI Field of view =1 0

X, nd

ee) G. e. t. = 137:29:25.7.

Figure 14.- Continued.

hM z: 205 stat. mi.

V. =5872 mphI

••

••

Page 105: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

•>-

RM =1121 n. mi.

V. =8602 fpsI

99

Field of view =10°

hM =209 stat. mi.

V. = 5865 mphI

''''''j

-<

n..

••

X, nd

(d)G.e.t. = 137:29:32.9 .

Figure 14.- Concluded.

Page 106: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

101

7»»»»»»» ~;I. MOON VIEWS««ecccccc««<

Page 107: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

102 •SEQ fl51 SU 570 582 593 sn

X -17 -21 .. 21 -2 -I.y -" , -7 -" 9

"R

M== 8528 n. mi. h

M== 8724 stat. mi. •V. == 5462 fps Field of view = 40°

V. == 3724 mphI I

-,.. i i i I , i i i i I i i i i I

20

10

o

-10

-20

20

10

o

-10

-20

-< 41

-20 -10 oX, nd

(a)G.e.t. = 140 hours.

10 20

Figure 15.- Transearth coast-constant field of view (moon>.

Page 108: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 103

• SEG 53~ 55 1 566 570X 16 -17 ~23 3y -16 ~ 10 4

RE=179 288 n. mi.

V. = 4876 fpsI Field of view =40 0

hE = 202 358 stat. mi.

V. =3324 mphI

20

-20

-10

20

Denebola~

10oX, nd

-10-20

(b) G.e.t. =150 hours.

Fi gure 15.- Conti nued .

20

-20

-10

lal. 10

• "'0 -<s::: 0 0 ~

0-r

••

Page 109: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

104 •SEG 53'3 !:Sl

)( 16 -1 7'( -15 6

!:66 ::7G-22 4

14 e

~82 50320 .~

(') 23 •R

E= 149473 n. mi.

V. = 5338 fpsI Field of view = 40°

hE = 168 046 stat. mi.

V. = 3640 mphI

20

-20

-10

2010

Denebola"

o-10-20

20

-20

-10

10 10

•""0

~-<

s::: 0 0 ::l

>c..

X, nd

<d G.e.t. =160 hours.

Fi gure 15.- Continued. •

Page 110: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 105

• SEG 5j5 551 566X 15 -1 7 -21y -15 9 17

570 ~a2

4 217 7

RE = 116265 n. mi.

V. = 6097 fpsI Field of view = 40°

hE = 129 832 stat. mi.

V. =4157 mphI

20

-20

-10

2010

Denebola,

o-10-20

20

-20

-10

10 l 10

• -<""0

G' 0t: 0 ~, 0-r

••

X, nd

Cd) G.e.t. =170 hours.

Figure 15.- Continued.

Page 111: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

106 •SElf 5.:35 551

X 14 -16y -13 1~ •RE

= 77 138 n. mi.

v. = 7571 fpsI Field of view = 40 0

hE =84 807 stat. mi.

V. = 5162 mphI

20 20

•-20

-10

/Denebola

2010o-10-20

-20

-10

10 10

•-c -<s:::: 0 0

~

::s.. 0-r

X, nd

(e) G.e.t. =180 hours.

Figure 15.- Continued. •

Page 112: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 1107'

• SEQ 515)( 15'Y .~~

535 5511~ -16

-11 15

5705

12

RE =22 296 n. mi.

V. =14 318 fpsI Field of view = 40°

hM =25 658 stat. mi.

V. =9762 mphI

-20

-10-10

-20

20

/G;enah/\ /l 20

10 l 10

•u -<l:: 0 0 :::l

>- a.

• -20 -10 o 10 20

•X, nd

(f) G.e.t. =190 hours.

Figure 15.- Concluded.

Page 113: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

loS ,.. ••

h = 202 358 slal. mi.

VE= 3324 mnh

IField of view == 4-

R = 179 288 n. mi.

/ =4876 fps

:.<5.

hM=8734 slat. 1111.

V. = 3724 mphIField of view ~ 20 c

cC) 0

. '. \'. fE>".. c).{ 0

V • °cl:?G c _.,

'cat·, .l-~c:q.o III• • ot:PoAr:P· b ~ X . 0!.t.?l •o· 0 p (): ~.~. :00\ .

\ •• 00 0""'-0.' • . ~".4> ••[)".~oe". 0"' .. 0Wf.lo· o' '.. • 4> 0~C c.' 0 '0' • 0 Ii ~ 0~ \:1:.(1 060 0

o 0 0 b 0oo

R =8528 n. mi.

V~ 5462 (ps

X, nd

laIG.e.t. = 140 hours ..

X, nd

!bIG.e.I.: 150 hours. •R =149473 n. mi.E

Vi - 5338 fnsField of view ~ 4°

~ : 168 046 slal. mi.

V = 3640 mphI

R : 116265 n. mi.

V\ 6097 Ips Field of view = 2°

E : 129 832 slat. mi.

V.: 4157 mphI

:.< :.<&.

•X, nd

Ie' G.e.I.= 160 hours.

rth coasl variable field of view (moon).Figure 16. - Transea

X, nd

(dIG.e.l. =170 oour5.

Page 114: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

•~

••

RE=

77

13

8n.

mi.

V.=

75

71

fps

IF

ield

ofvi

ew=

20

hE=

84

80

7st

at.

mi.

V.=

51

66

mph

I

RE

=2

22

96

n.m

i.

V.=

14

31

8fp

sI

Fie

ldof

view

=1

0

hE=

21

69

4st

at.

mi.

V.=

97

62

mph

." l: ;;

X,

nd

(e)

G.e

.t.=

18

0ho

urs.

~ a

X,

nd

(f)G

.tl.

t.=

19

0ho

urs.

;< ::> 0.

g

Fig

ure

16

.-C

oncl

uded

.

Page 115: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

1] 1

•~»»»»»»>% EARTH VIEWS III>~""""", t"",e

Page 116: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

•112

•~~,~ " .. U I.J"\

l 1I J. J »T

••

•10

-10

20

20

. I ,

l rl.c.t. = 150 hours.

/I

/

.l ' . I 0, I ,

10 0 10

X, ml

//

!/

//

/'

/X //

/, /, / "- '

-In

//

R _= 179 283 II. Illi _ hE c_ .~02 358 stat. mi.L

'J := 487h fps V == 3324 1:11'11I Field ()f v;r-w = 40° I- ---=-:.~,-:.-:=r -~r--.-~--'--

Ll

~

"

1n

-10

-(, L< L

fi<lllr2 1 i . I ',lllsrartll CO.1st-constant field of VIr-IN (earth).

Page 117: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 113'

• Slt "0 10"1l 0 21, I" 2

RE=149 473 n. mi.

V. =5338 fpsI Field of view =40°

hE =168 046 slat, mi.

V. = 3640 mphI

-20

-10-10

-20

20 20

10 l 10

• Fomalhaut""

-<-0

0t: 0 ::;,c..>-

..

••

-20 -10 oX, nd

(b) G.e.t. =160 hours.

Figure 17.- Continued.

10 20

Page 118: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

•114

•Sto.,j Y'IU 1 u'i I

l\ IJ 2.lY I I '::> •

RE=116 265 n. mi.

V. = 6097 fpsI Field of view =40°

, , iii. , i ; i i

hE =120 832 stat. mi.

V. =4157 mphI

iii i , t , I I , ---,..

20

-10

-20

20

-10

-20

10Fomalhaul~ 10 •

-<- 0 0~

a..>-

-20 -] 0 oX, nd

(d G.c.t. =170 hours.

Figure 17.- Continued.

10 20

Page 119: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

115

SI:.\il 99U IU'f1

A U ZJy 2 J I I

-<o -;.

c..

10

-20

-10

Fomalhaut""

RE = 77 138 n. mi. hE = 84 807 stat. mi.

V.=7571fps F' Id f' 400 V.= 5162 mphI Ie 0 vIew = I

o

20 ['.""""""';""~"""~'"""" ,,", ] 20

10

-10

-20

••

-20 -10 oX, nd

Cd) G.e.t. = 180 hours.

10 20

Fig"re 17.- Continued.

Page 120: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

116••St.1lI 7 I J'.

'"-\'> 2

y - l -I" •

RE

= 22 296 n. mi.

V == 14 318 fpsI Field of view =40°

hE = 25 658 stat. mi.

V. =9762 mphI

->-

20

1U

o

-10

-20

20

10

-<o

~

-10

-20 •-20 -1 () o

X,llri

(c) G.e.t. == 190 hours.

Figure 17.- Concluded.

10 20

Page 121: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

RM" 1922 n. mi.

Vi" 7266 fps'. ,,--, ...... ' .. Field of view::: 3°

-I~----'

I

hM " 1132 stat. mi.

V." 4954 mph....... !..1'~~ ..-,...., ,·t

117

RM .. 5296 n. ml. hM

'" 5014 stat. mi.

Vi" 5823 Ips Field of view =3' Vi =3970 mph~~~~~~~~r' ,-~~.:-.-..-..~

• X, nd

Ca) G.e.1. " 138 hours.

:<&.

X, nd

I G.e.t. =139 hours.

:<

Field of view::: 3°

RM =8528 n. mi. hM

" 8734 stat. mi.

Vi :':;6,2, f.ps, , , , , , , . , Field of view = 3' Vi" 3724 mph. """"I'~~~~' ~~

RM'" 11666 n. mi.

V." 5297 fps----!....-_~~~.......... '''~'l

hM" 12 346 stat. mi.

Vi =3~_~~~~h .' .,

(d) G.e.1. = 141 hours.

X, ndX, nd

Figure 18.- Transearth coast - variable fieid of view (earth),

(e) G.e.t. =140 hours.

~ ..,~ ..~~

•-g .< , .<;; 5- - =.

0.

••

Page 122: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

RM

.. 14 '47 n. mi. hM

-15891.101. mi.

Vi .. 52~0_2~Ip~S~~~_~~~F~i~'~ld_O_I.,vriew......."_3~'~~~~V+-.-~3_5_4_7~mp~h_~.....,

,1.

ItM

-11792n,ml.

V. - 5140 /11. Field of view = 3·

hM - 19 394 .tat. ml.

VI" 3505 mph

••

X. nd

fe) G.e.1. = 142 hours.

RM =20 812 n. mi. hM =22 869 stat. mi.

Vi =5098 Ips Field 01 vi.w =3' Vi =3476 mph~ r~,."", rr~~~~

X, nd

(g) G.•. t. = 144 hours.

::<5.

X, nd

en G.•.1. =143 hours.

RM

=23813 n. mi. hM = 26 324 stat. mi.

Vi =5068 Ips Field 01 view" 3' V. =3455 mph~ ~." ".,.",.,.r'1~·r,~~.-"!-.--, ,r~-. . , .. ,

X, nd

fh) G.•.1. =145 hours.

::<5.

••Figure 18. - Continued.

Page 123: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 119

hM= 33 191 stat. mi.

Vi" 3~-=-1 mph. ._.

X, nd

I.

Field of view:: 3°

0) G.e.t." 147 hours.

RM

=29781n.mi.

V. .. 5032 fps

:<&.

hM" 29 763 .tat. mi.

Field of view:: 3° Vi := 3441 mph.~,~._~ ~l"""""';"~~

X, nd

RM" 26 802 n. mi.

V... 5047 fpsI

(j) G.e.t." 146 hours.•

••

RE

" 184 976 n. mi. hE" 208 903 stat. mi.V." 3282 mph

V. " 4813 fps Field of view" 3" _~~--.!'c......_~~~~.......,..--ll~~~~~~""""il~-

"E" 182 141 n. mi.

Vi" 4843 fps Field of view = 3°

hE" 205 640 stat. mi.

V." 3302 mphI

:.< :.<"" "c

" Q.

,: Q.

••

X, nd

(k) G.e.t." 148 hours •

Figure 18.- Continued.

X. nd

(I) G.e.t." 149 hours.

Page 124: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

RE =179 288 n. mi.

V. = 4876 rpsI Field of view ~ 1°

120

IRE " 176 416 n. mi.

V." 4911 rpsI Field of view = 3-

hE" 199053 stat. mi.

Vi" 3348 mph

••

X, nd

(m)G .•• t." 150 hours.

X, nd

(n) G.•. t. = 151 hours.

•R[ = 173 523 n. <ni.

V. = 4940 ipsI Field of view::::: 3 n

hE = 195724 stat. mi.

V." 3374 mphI

~E = 170 609 n. mi.

V = 4990 rpsI Field of view = 3°

hE .. 192 370 stat. mi.

Vi =3402 mph

X, nd

Co>G.C'.t. - 152 hours.

X, nd

(p) G.e.t. = 153 hours.

Fiqure 18.- Continued.

.<

••

Page 125: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

..<it

:<

hE = 185536 stal. mi.

VI· 3462 mph

hE" 178 667 stat. mi.

V." 3528 mphI

X, nd

Field 01 vi.... 3·

ft) G.•.I." 157 hou,s.

(,) G.e.I." 155 hours.

RE " 158 702 n. mi.

VI" 5174 Ips

~.

liE· 164 707 n. mi.

VI. 5077 ""

hE .. 182 139 stat. mi.

Vi" 3494 "",h

Figure 18.- Continued .

"E. 1 1lIf .,

VI. J4J2 ""'"

X, nd

X. nd

Field 01 vi..... 3·

CqIG.e.t." 154 hours •

Csi G.•. t. =156 hours.

RE " 167 671 n. 011'1VI" 5033 Ipi

RE~ 161 718 n. mi.

Vi =5125 Ips

~

c

,:

•••

..•

Page 126: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

122

"'[ ~ 155656 n. mi.V; ~ 5226 Ips - " 175 163 ltAl. mi ••

r~~~~~~_~~_.!.F~ie~ld~Of view= '3" Vi := 3563 mph I

I~' ..~.~..:-.-.-...,........;..-~

~~~\"

X, nd

(ulG.e.t. = 158 h0urs.

RE~ 149473 n. mi.

V; ~ 5338 Ips

X, nd

IwlG .•. t. = 160 hours.

;'-E. 15! 580 n. m;.

Vi = 5280 Ip,

RE~ 146 332 n. mi.

V;~ 5398 Ips

Stat. ml,

Fip.lrl of Vlew:= 30 \Ii ="bOU mph_._~.~~~~~

X. nd

(v) G.e.t. = 15'1 hours.

hE = 164 433 SUllo III I .

Vi ~ 3680 mph

X, nd

(xl G.e.t. = 161 hours.

:;<a.

••..

••Figure 18.- Continued.

Page 127: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

• 123

hE =157 082 stat. mi.

Vi =3768 mph

X, nd

Field of View = 3-

(z) G.e.t. = 163 hours.

"RE '" 139 944 n. mi.

.~ Vi'" 5526 fps

hE = 160 779 stat. mi.,

Vi = 3723 mph .

X, nd

CyIG .•. t. = 162 hours.

RE

= 143 157 n. mi.

V. = 5460 IpsI

'<~ :' ;<c

:: a. ~~

Figure 18. - Continued.

••

RE

= 136 694 n. mi. hE

= 153 342 stat. mi.

rV';-i-~-~5_5Q~.5~f~p~s~~~-=:;F~i.:Jd=O::;;f~Vi=:.W~=~3~':-=~~V'-,.i=~38_1_5_m~p_h~~...,

X, nd

Caa) G••. t. = 164 hours.

RE

= 133 403 n. mi.

Vi = 5668 Ips Field of view = 4°

X, nd

Cbb) G••. t. = 165 hours .

hE =149 555 stat. mi.

Vi = 3865 mph

Page 128: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

>-'

130070 n. mi .

. 1)744 rns

R[ ~ 123 267 n. m, .

Vi = 5911 fps

Field of view ~ 4°

(cd G,e.t. = 166 hours.

Field of view:= 4°

hE = 145 719 stat. mi

Vi ~ 3916 mph

hE =137 891 stat. m,

Vi =4030 mph

124

RE=126692 n. mi.

Vi =5825 Ips

RE = 119793 n. mi.

Vi = 6001 Ips

Field of view = 4°

X, nn

CddlG,e.1. '" 167 hours.

Field of view = 4 11

hE =141 832 stat. mi.

Vi'" 3972 mph

hE =133 892 stal. mi.

Vi =4092 mph

••

•X, nd

(ee) G.e.t. = 168 hours.

Figure 18.- Continued.

X, nd

(If) G.e.1. '" 169 hours.

Page 129: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

•••

RE = 116 265 n. mi.

Vi = 6097 fps Field of view = 4"

X, nd

(gg) G.••t. =170 ho"rs.

hE = 129 832 stat. mi.

Vi = 4157 mph

125" f

f RE=1126111 n, mi.

Vi" 6199 fpsField of view '" 4"

X, nd

(hh)G ••• t. = 171 hours.

hE" 125 709 slat. mi.

Vi'" 4227 mph

Figure 18.- Continued.

••

RE =109 038 n. mi.

Vi = 6308 fpsField of view = 4°

X, nd

(ij) G.e.t. = 172 hours.

hE =121 515 stat. mi.

Vi = 4301 mph

;<

i5.

RE '" 105331 n. mi.

Vi'" 6425 fps~~~~~~~~~~,::F,:-i.~ of view'" 4"

X, nd

(jj} G••• t. = 173 hours.

hE =117250 slat. mi.

Vi = 4381 mph

Page 130: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

:<

..<il.

hE =99 342 stat. mi.

Vi = 4658 mph

hE = 108 478 stat. mJ.

Vi = 4559 mph

I t"

X, nd

Field of vi~ = 5°

lIll G••. t. =175 hours.

':RE=89 769 n. mi.

Vi = 6991 Ips

:<il.

126

T! ~E = 97 708 n. mi.

Vi = 6686 Ips

hE = 112 906 stat. mi.

Vi =4467 mph

hE =103959 stat. mi.

Vi = 4658 mph

Field of view =5'

X, nd

Field of Yiew:: •

(kkl G.••1. = 174 hours.

RE =101 556 n. mi.

Vi = 6551 Ips

RE = 93 781 n. mi.

Vi =6832 Ips

X, nd

(mmIG.e.t. =176 hours.

'tre 18. - Continued.

X, nd

(nn) G.••t. =177 hours.

Page 131: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

."C

RE =85 664 n. mi.

Vi" ?l66 fps

RE

= 77 138 n. mi.

Vi = 7571 fps

X, nd

(oolG .•• t. =178 hours.

Field of view = 6 0

hE" 94 618 stat. ml~Vi =4886 Iftph

hE = 84 807 stat. mi.

Vi =5162 mph

• RE

= 81457 n. mi.

, V." 7357 IllsI

RE

= 72 695 n. mi.

V. = 7809 fpsI

Field of view =6'

X, nd

(pp) G••. t. =179 hours.

Field of view = 6 0

hE =89 776 stat. mi.

Vi" 5016 mph

hE =79 692 stat. mi.

V = 5324 mphI

••

X, nd

(qql G.•.t. = 180 hours.

Figure 18.- Continued.

X, nd

(") G.e.t. = 181 hours .

Page 132: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••

••

:<

/

hE = 57 396 sta!. mi.

V. = 6254 mphI

hE = 68 964 stat. mi.

V. = 5718 mphI

X, nd

X, nd

Field of view = 8°

Field of view = 10·

(vv' G.•. !. = 185 hours.

(ttl G.•.!. = 183 hours.

-I

\

RE =53320n.mi.

V. = 9172 IpsI

I .RE = 63 372 n. mi.

V. = 8387 Ip.I

Figure 18.- Continued.

hE = 63 302 stat. mi.

V. = 5963 mphI

128

hE = 74 420 .tat. mi.

V. = 5078 mphI

X, nd

X, nd

Field of view= 8°

Field of view = 8°

(uul G.•.!. = 184 hours.

(.,) G••.!. = 182 hours.

RE = 58 451 n. mi.

V. = 8746 IpsI

RE = 68112 n. mi.

V. = 8078 fpsI

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••

RE =47 938 n. mi.

Vi = '1689 fps

RE = 36182 n. mi.

Vi = 11192 Ips

Fi.ld of view = 10'\ I

X, nd

(ww) G••• t. = 186 hours.

Field of view::;;: 13°

hE =51 204 stat. mi.'Vi'" 6606 mph

hE = 37674 stat. mi.:

V. = 7631 mphI

RE " 42 252 n. mi.

: Vi -10338Ips

RE =29 603 n. mi.

Vi =12399 Ips

Fietd of view::: 13-

X, nd

(xx, G.e.t. = 187 hours.

Field of view::: 20°

I, hE " 44 661 stat. mi.

V." 7049 mph. I

hE = 30103 stat. mi.

V. = 9762 mphI

••

X, nd

(yy) G.e.t. =188 hOllrs.

Figure 18.- Continued.

X, nd

(zz' G.e.t. = 189 hours.

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"'0C~

>-

130

RE =22 296 n.. mi. hE =21 694 stat. mi.

V. = 14318 fps Field of view =20° V. = 9762 mph......:,..1.............,........,.......,........-,-.......,........-,-............,.....,,.....,-.,.................,.~......"'T.......-,-..,.........., ....i~..........-.-. ,~-,.- -r -.--r-~....,......,~......,......,.....,.....r- iii • ~ • •

X, nd

(aaa) G.e.t. =190 hours.

Figure 18.- Concluded.

••

••

Page 135: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

e

e

e

e

131

...1

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132

SEQ ill•• 290 lUI \'f9 3r.6 JU :.77 If If 0 .7.1 .. Ia '07 lOtX '0 2'f 22 -J 10 -1 lJ 12 0 _J -21 -J:IY '1 IS 12 1J 9 1 1 I -I -6 ., a 1

SEQ ltl!l SJIt 1i 1f 0 lit'0X •• •• .l.2 -20Y -II -16 ... -I"

••

20

10

RE =5426 n. mi.

V. =29 175 fp5.I ..,..,='7;';'JI':'~ Field of view =1000

hE =2283 stat. mi.

V.= 19 892 mphI

rProcyon

20

10

•"'C • -<t: •0 0

,, • •>- ~c..

• AIPhard"Reg~lus,

-10Pollux """- -10

Denebola,

Moon~

-20 -20 •(a) 15 min prior to entry (g.e.t. =191:35:32.2).

-20 -10 oX, nd

10 20

•Figure 19.- Entry phase.

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•133

-<..o

20

10

/procyon

Alphard~

o

20

10

SEQ no .108 3S6 362 377 .... 0 "'3 '1'0 ~07 S09 S 1f~ S3S .ltDX 2'1 23 1 (j -1 23 12 0 -3 -21 -23 .. 6 "S .22Y Ie IS 13 IS 'I -1 -2 -2 3 'I -7 -12 0

SEQ SSI S70 S80 S82 610 '51

• X 7 -1 -20 -v ·16 -Z4Y -22 -2~ -10 -21 -23 -23

hE =1891 stat. mi.ro,

Field of view =1000

l--r-,.. • , •

••

-10•

Denebola, Moon,

•-10

-20

20

Figure 19. - Continued.

-10

(b) 13 min prior to entry (g.e.t. =191:39:32.2).

-20

Gienah,

'-'--_..L...&.~...............................-L..~~~_~~ ~.~~~--,---,-L~~~"",--,,,,,,,,,.o.....L -....I

o 10

X, nd

-20

••

Page 138: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

,

••

o

10

-10

hE = 1512 stat. mi.

V. =21 251 mphIField of view = 1000

RE=4756 n. mi.

V. =31 168 fpsI

134

SEQ ,)n' 177 ItItQ .. 7,) ItID i07 5o, it. .fI3S ftltO 5ltil i'l ...X 'II 2,) 12 0 -,) -21 -2,) -, . -Ii _22 Z" 7 ,Y I' It 2 2 2 7 _i -2" -1 ,) -21 -~a -Zt

SEQ i7U illO lJI2 It.J .U;l U .. 'iiiX -1 -19 .i U -lit .1 7 -2,)

Y -17 -. -I' -, .. -I' -20 -19

20

/10

//~••

AIPhard",

• ~/ .;-Regulus

-cs::

0 •>•

• Denebola~

Moon~-10

(c) 11 min prior to entry (g.e.t. =191:39:32.2>'

Figure 19. - Continued.

-20

Arcturus,

••

-20 -10

••

Spica

Gienah"

oX, nd

10 20

-20

••

Page 139: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

o

10

20

Alphard"

Regulus

•Denebola,

••

10

• "0I::

0,>-

135

• SEQ ~77 ""0 'f7J 4110 fi07 509 51i flJIi '''0 ... s 551 50.. iUX ,.. 12 0 -.1 -21 -211 -, -i -22 2:1 7 9 21Y ., 7 7 a 11 12 2 .2 7 .1 1 -12 -., -lg

SEQ 507u ilto !ilM2 !:tA9 50U ,9i '10 '2" 'filX -I -19 _8 1.1 (J • -Ii -17 -22

• Y -12 -2 -11 -,J -1 9 _22 -1" -I' -1ft

RE = 4446 n. mi. hE = 1247 stat. mi.

V. = 32 242 fps Field of view = 1000 V. = 21 983 mphI I

~Moon

-10 -10

••

-20

-20

• Gienah,•

•SPica,

••

-10 0 10

X, nd

Cd) 9 min prior to entry Cg.e.t. =191 :41 :32.2) •

Figure 19.- Continued.

20

•-20

Page 140: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

20

10

136,

•U'l .... U .. 71 lIao 507 lili S.U i.1I0.--'" .U1 UJ U-' . i .. lJj3II 12 0 -3 -ll -0 -5 -23 U 7 211 I aD -I,

I J 1.. ...u U • 3 11.. -a. -6 -u -, _~.1S -.~iJO ill U9 lte.l 59ft it9 .. 0 '17 '21 62 .. 051 ... J ...II -19 -. 12 0 fa 20 -111 23 10 -10 -21 -a -,. •, 2 -50 -17 -,2 -1ft -20 -a -23 -ll -10 -.g -aa .~

RE = 4161 n. mi.

V. = 33 330 fps~I

20

10

Page 141: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

20

20

• 137

SEQ In us S"o S"S SSI S61 SU U, S70 S7" SIO 58 2 S89 S'3 Inx . ...- .!I ._--Z""t"'-~r -a- 2J .- .--...- -"1 7'l -W· ..•• 12

... -0...5"

V IS 10 11 ·7 a ·10 ·2 ., I ·12 9 I -10 ·li ••

• SEQ r.99 610 617 6 2 1 62" 6,,1 6"3 '''S '51 ,u 660 673 688 69O 7C10X 19 ·111 22 10 ·16 12 21 III ;;;21 -I 12 ., 10 -211 ai'V -I" ·1 ·17 ·1" ... ·18 .20 -I' ... ·1' -2O -17 -23 ., .1 7

~

RE = 3910 n. mi. hE = 540 stat. mi.V. = 34 384 fps Field of view =1000 V. = 23 444 mphI I

10 10•

•"'0 • Gienah"". -<t:

0~

0 II~~

a.>- •Arctur~s, •

SPica,•

Alphecca-10 • -10•

Beta CrUCiS"

.. Menkent,•

•• •• • Ri9il,

-20 -20

• •

-20 -10 0 10 20

X, nd

• (f) 5 min prior to entry (g.e.t. =191:45:32.2>-

Figure 19.- Continued.

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20

138

SEQ iil!i SSI s" ~., !l" i7Q ih itO iU lil' iU US S••

•X ' I 7 2Z • " -, 2.) -ZO -. ,2 0 i ..Y a • -.. !i -2 • -s " HI -2 2 0 ·7

SEQ 61D 617 621 ., .. ... 1 ,.. ~ , ..s "I 'ss "0 ,73 ..,X -'II Z, • -16 " 20 13 -21 -I 11 -. •y i -10

_.J -10 -13 -" 2 -7 -&2 -. "Ii

SEQ •• 0 700 717 ", 7Z .. 71' 7113 hi JSl 7U 7S1 7s. 77Q

X -'3 -I" I II -2 a Q -2) 1 .8 23 .. -, •y .3 -, -16 -I' ·16 -I. -20 ..,, .. ZO .,. -20 -22 "2~

SEQ 79i IU)

X -22 -,.Y -21 _l ..

,R

E= 3706 n. mi.

V. = 35325 fps Field of view = 100 0

I

20

Page 143: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

2020

• 139·

SEQ 5l1l~ S•• S·. .." S71t su SU i .. ." .IQ ·17 'a. "II .,..'11.)X ,. 22 8 I' 2,) 12 0 Ii 11 -Ii 20 • -.6 11 ItY • 2 1J Ii 0 Ii II • 0 lJ -,) • 11 -I -.

SEQ ••s 6r,1 US "0 673 ... 690 700 7U. 7a' 7; .. 7.U 7 .. .1 ,... 7lilX • J -'1 -I .0 -Ii • -2J -... • " _2 0 0 -2J I• Y .3 9 I -,. 0 -7 .) -I -, ., _7 -10 -& I -.. -la'SEQ 753 757 7•• 77Q 781 719 7'0 7U 79 Ii 7 9 7 ~O2 In,) ',)6 ,,.1 .,. ..X -:, 22 If .. It IS S 12 S -21 • • -,7 & ,) -IY -&g -IJ -Ilf eli _17 -18 -&7 ·Ii -... -II -1 9 .,. -2,) .2,) -2"

RE=3557 n. mi. hE=132 stat. mi.V. =36055 fps

Field of view =1000 V. =24 583 mphII

• •Arcturu~ """

10 10

• •

••/Alphecca

Menkent~Beta Crucis~

-<-c

, .~

s::::0 • 0• ~

~

•0->- • •

•• •Ri~il,

• • .-10

Antares~ -10•• Atria~r- Rasalhague

•••

• ,•-20 • -20

-20 -10 0 10 20

X, nd

• (h) 1 min prior to entry (g.e.t. =191:49:32.2).

Figure 19. - Continued.

Page 144: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

1:40'I

•SEQ ,/

ill. la'i i6' C;7" 589 it.l it5 ,.. '1 7 Ul '''1 '''J 6411X ! I 22 1, 23 12 a 5 11 20 • 11 19 UY I' • • II 10 U 12 1 0 , 2 e2 Q

SEQ "I ,Its "0 ,.,3 ." "0 7g0 71 7 71' 72 .. 7.16 74aX ·21 ·1 10 _5 , .21 ·11t 0 0 ·2 0 gy 12 S 0 3 -2 • 2 .,1 -,1 -,1 ·5 .'

SEQ Ill" lSI 751 757 75' 770 711 11' no 793 795 797 '02 •X -'1 I ·7 21 II ·5 1.. i 1 1 5 -20 • • /

Y 0 "7 .., _10 -, .. &0 "12 -1,1 .. 1.1 .11t "10 .... ·11t

SEQ lu3 aJ, 11111 a.... 'u .71 9J,1X -I' 1 ,1 _1 U 1 II ,Y ·12 -I' -I' -I' -~Z .. 2.1 -Zit

RE =3508 n. mi. hE =76 stat. mi.

V. =36309 fps Field of view =1000 V. = 24 756 mphI I

2020

10 • 10 •/AIPhecca •/Menkent,

'0(/Beta Cru~is~

•• •

-0 -<t:0 0

..• • •..Ri?il,

~

>- c-

• •• •Antares,

• ••

-10rRaSalhagUe • Atria,

-10•

• ,• "•

-20 • • •• -20

Nunki,Peacock•

-20 -10 0 10 20

X, nd •(j) Entry interface (g.e.L =191:50:32.2>­

Figure 19.- Concluded.

Page 145: ~PR - NASA · msc internal note no. 69-fm-107 project apollo views from the spacecraft during apollo 10 (mission f) may 18, 1969 launch date by alfred n. lunde

••r

••

REFERENCES

1. Lunde, Alfred N.: Views From the Spacecraft During Apollo 10(Mission F). MSC IN 69-FM-74, March 21, 1969.

2. Rogers, JQseph E.; and Burton, John K.: Apollo 8 Reentry CrewCharts. MSC memo 68-FM23-216, December 12, 1968.

3. OMAB; LMAB; and LAB: The Spacecraft Operational Trajectory forApollo'lO (Mission F), Volume II. MSC IN 69-FM-97,