3.1 kg

87
USUSat Assem bly View s Structures D eployable Antennas Gim bal Antennas Battery Box C om m SolarC ells ADCS D eployable Boom s External Assem bly U SU Sat-ASSEM B-01 Internal Assem bly U SU Sat-ASSEM B-02 Structure Assem bly U SU Sat-STR U C T-01 Top Panel U SU Sat-STR U C T-02 Bottom Panel U SU Sat-STR U C T-03 Side Panel #1 U SU Sat-STR U C T-04 N adirExternal Panel U SU Sat-STR U C T-05 Side Panel #2 U SU Sat-STR U C T-06 Side Panel #3 U SU Sat-STR U C T-07 Side Panel #4 U SU Sat-STR U C T-08 Side Panel #5 U SU Sat-STR U C T-09 Side Panel #6 U SU Sat-STR U C T-10 Alum inum H oneycom b Panel U SU Sat-STR U C T-10 D eployable Assem bly U SU Sat-D EPLO Y-01 D elrin Post U SU Sat-D EPLO Y-02 Tensioner U SU Sat-D EPLO Y-03 Pin Puller U SU Sat-D EPLO Y-04 Antenna R ibbons U SU Sat-D EPLO Y-05 Pin PullerBracket U SU Sat-D EPLO Y-06 D elrin W asher U SU Sat-D EPLO Y-07 G im bal Assem bly U SU Sat-G IM BAL-01 C overPlate C 2 U SU Sat-G IM BAL-02 C overPlate C 1 U SU Sat-G IM BAL-03 C overPlate B U SU Sat-G IM BAL-04 C overPlate A1 USUSat-G IM BAL-05 C overPlate A2 U SU Sat-G IM BAL-06 G im bal Spacer U SU Sat-G IM BAL-07 G im bal Lock M echanism U SU Sat-G IM BAL-08 G im bal M agnetSpindle U SU Sat-G IM BAL-09 G im bal M ain Support#1 U SU Sat-G IM BAL-10 G im bal M ain Support#2 U SU Sat-G IM BAL-11 R eaction W heel R od U SU Sat-G IM BAL-12 G im bal R eaction W heel USUSat-G IM BAL-13 G im bal Arm C over U SU Sat-G IM BAL-14 G im bal W orm R od 1 U SU Sat-G IM BAL-15 G im bal W orm R od 2 U SU Sat-G IM BAL-16 G im bal W orm R od 3 U SU Sat-G IM BAL-17 D C Probe Patch U SU Sat-AN TEN N -01 D ow nlink Patch U SU Sat-AN TEN N -02 G PS Patch U SU Sat-AN TEN N -03 C rosslink M onopole U SU Sat-AN TEN N -04 Figure Included Figure N otIncluded Figure From O therSource C EE Enclosure Assem bly U SU Sat-ASSEM B-02 Battery Box Assem bly U SU Sat-BATT-01 Battery Box FrontR etainer U SU Sat-BATT-02 Battery Box R earR etainer U SU Sat-BATT-03 Battery Box G asket U SU Sat-BATT-04 Battery Box Fram e U SU Sat-BATT-05 Battery Box C over U SU Sat-BATT-06 Crosslink Chassis U SU Sat-XLIN K-01 T/R Sw itch and Isolator U SU Sat-XLIN K-02 R eceiverBox U SU Sat-R EC VER -01 R eceiverBox C over U SU Sat-R EC VER -02 Beacon Box U SU Sat-BEAC O N -01 R eceiverBox C over U SU Sat-BEAC O N -02 Transm itter U SU Sat-TR AN S-01 Link M atcher U SU Sat-TR AN S-02 C rosslink G PS Pream p U SU Sat-XLIN K-03 C rosslink SBand Pream p U SU Sat-XLIN K-04 SolarArray #1 & #2 U SU Sat-SO LAR C -01 SolarArray #3 U SU Sat-SO LAR C -02 SolarArray #4 U SU Sat-SO LAR C -03 SolarArray #5 U SU Sat-SO LAR C -04 SolarArray #6 -#10 U SU Sat-SO LAR C -05 SolarEpoxy Array #1 & #2 U SU Sat-SO LAR C -06 SolarEpoxy Array #3 U SU Sat-SO LAR C -07 SolarEpoxy Array #4 U SU Sat-SO LAR C -08 SolarEpoxy Array #5 U SU Sat-SO LAR C -09 SolarEpoxy Array #6 -#10 U SU Sat-SO LAR C -10 Kapton Sheets #1 & #2 U SU Sat-SO LAR C -11 Kapton Sheet#3 U SU Sat-SO LAR C -12 Kapton Sheet#4 U SU Sat-SO LAR C -13 Kapton Sheet#5 U SU Sat-SO LAR C -14 Kapton Sheet#6 U SU Sat-SO LAR C -15 G yro Assem bly U SU Sat-AD C S-01 G yros U SU Sat-AD C S-02 G yro M ounting R ing U SU Sat-AD C S-03 G yro M ounting Fram e U SU Sat-AD C S-04 C am era Assem bly U SU Sat-AD C S-05 C am era AdaptorR ing U SU Sat-AD C S-06 C am era Lens R etainer U SU Sat-AD C S-07 Science Boom USUSat-BO O M -01 M agnetom eterBoom USUSat-BO O M -02 D elrin R earM ount USUSat-BO O M -03 M agnetom eterM ount USUSat-BO O M -04 Science Boom M ount USUSat-BO O M -05 M agnetom eterTube USUSat-BO O M -06 Science Antenna Tube USUSat-BO O M -07 D elrin G uide USUSat-BO O M -08 M otorM ount USUSat-BO O M -09 Science O uterTube USUSat-BO O M -10 N on C onductive Tube USUSat-BO O M -11 Lead Screw USUSat-BO O M -12 W orm G earSleeve USUSat-BO O M -13

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USUsat-STRUCT-01. 1 of 1. 1. I O N - F Utah State University - University of Washington - Virginia Tech. Aluminum 6061-T651. 0.010” 0.005”. 0.5 O. External Structure Assembly. Ashby, B. 01/03/01. None Required. SSE, Etc. DD/MM/YY. Irridite Class 3 per MIL-C-5541. USUsat-STRUCT-01. - PowerPoint PPT Presentation

TRANSCRIPT

Page 1: 3.1 kg

USUSat

Assembly Views

Structures

Deployable Antennas

Gimbal

Antennas

Battery Box

Comm

Solar Cells

ADCS

Deployable Booms

External AssemblyUSUSat-ASSEMB-01

Internal AssemblyUSUSat-ASSEMB-02

Structure AssemblyUSUSat-STRUCT-01

Top PanelUSUSat-STRUCT-02

Bottom PanelUSUSat-STRUCT-03

Side Panel #1USUSat-STRUCT-04

Nadir External PanelUSUSat-STRUCT-05

Side Panel #2USUSat-STRUCT-06

Side Panel #3USUSat-STRUCT-07

Side Panel #4USUSat-STRUCT-08

Side Panel #5USUSat-STRUCT-09

Side Panel #6USUSat-STRUCT-10

Aluminum Honeycomb PanelUSUSat-STRUCT-10

Deployable AssemblyUSUSat-DEPLOY-01

Delrin PostUSUSat-DEPLOY-02

TensionerUSUSat-DEPLOY-03

Pin PullerUSUSat-DEPLOY-04

Antenna RibbonsUSUSat-DEPLOY-05

Pin Puller BracketUSUSat-DEPLOY-06

Delrin WasherUSUSat-DEPLOY-07

Gimbal AssemblyUSUSat-GIMBAL-01

Cover Plate C2USUSat-GIMBAL-02

Cover Plate C1USUSat-GIMBAL-03

Cover Plate BUSUSat-GIMBAL-04

Cover Plate A1USUSat-GIMBAL-05

Cover Plate A2USUSat-GIMBAL-06

Gimbal SpacerUSUSat-GIMBAL-07

Gimbal Lock MechanismUSUSat-GIMBAL-08

Gimbal Magnet SpindleUSUSat-GIMBAL-09

Gimbal Main Support #1USUSat-GIMBAL-10

Gimbal Main Support #2USUSat-GIMBAL-11

Reaction Wheel RodUSUSat-GIMBAL-12

Gimbal Reaction WheelUSUSat-GIMBAL-13

Gimbal Arm CoverUSUSat-GIMBAL-14

Gimbal Worm Rod 1USUSat-GIMBAL-15

Gimbal Worm Rod 2USUSat-GIMBAL-16

Gimbal Worm Rod 3USUSat-GIMBAL-17

DC Probe PatchUSUSat-ANTENN-01

Downlink PatchUSUSat-ANTENN-02

GPS PatchUSUSat-ANTENN-03

Crosslink MonopoleUSUSat-ANTENN-04

Figure Included

Figure Not Included

Figure From Other Source

CEE Enclosure AssemblyUSUSat-ASSEMB-02

Battery Box AssemblyUSUSat-BATT-01

Battery Box Front RetainerUSUSat-BATT-02

Battery Box Rear RetainerUSUSat-BATT-03

Battery Box GasketUSUSat-BATT-04

Battery Box FrameUSUSat-BATT-05

Battery Box CoverUSUSat-BATT-06

Crosslink ChassisUSUSat-XLINK-01

T/R Switch and IsolatorUSUSat-XLINK-02

Receiver BoxUSUSat-RECVER-01

Receiver Box CoverUSUSat-RECVER-02

Beacon BoxUSUSat-BEACON-01

Receiver Box CoverUSUSat-BEACON-02

TransmitterUSUSat-TRANS-01

Link MatcherUSUSat-TRANS-02

Crosslink GPS PreampUSUSat-XLINK-03

Crosslink SBand PreampUSUSat-XLINK-04

Solar Array #1 & #2USUSat-SOLARC-01

Solar Array #3USUSat-SOLARC-02

Solar Array #4USUSat-SOLARC-03

Solar Array #5USUSat-SOLARC-04

Solar Array #6 - #10USUSat-SOLARC-05

Solar Epoxy Array #1 & #2USUSat-SOLARC-06

Solar Epoxy Array #3USUSat-SOLARC-07

Solar Epoxy Array #4USUSat-SOLARC-08

Solar Epoxy Array #5USUSat-SOLARC-09

Solar Epoxy Array #6 - #10USUSat-SOLARC-10

Kapton Sheets #1 & #2USUSat-SOLARC-11

Kapton Sheet #3USUSat-SOLARC-12

Kapton Sheet #4USUSat-SOLARC-13

Kapton Sheet #5USUSat-SOLARC-14

Kapton Sheet #6USUSat-SOLARC-15

Gyro AssemblyUSUSat-ADCS-01

GyrosUSUSat-ADCS-02

Gyro Mounting RingUSUSat-ADCS-03

Gyro Mounting FrameUSUSat-ADCS-04

Camera AssemblyUSUSat-ADCS-05

Camera Adaptor RingUSUSat-ADCS-06

Camera Lens RetainerUSUSat-ADCS-07

Science BoomUSUSat-BOOM-01

Magnetometer BoomUSUSat-BOOM-02

Delrin Rear MountUSUSat-BOOM-03

Magnetometer MountUSUSat-BOOM-04

Science Boom MountUSUSat-BOOM-05

Magnetometer TubeUSUSat-BOOM-06

Science Antenna TubeUSUSat-BOOM-07

Delrin GuideUSUSat-BOOM-08

Motor MountUSUSat-BOOM-09

Science Outer TubeUSUSat-BOOM-10

Non Conductive TubeUSUSat-BOOM-11

Lead ScrewUSUSat-BOOM-12

Worm Gear SleeveUSUSat-BOOM-13

Page 2: 3.1 kg

3.1 kg

Ashby, B.

SSE, Etc.

01/03/01

DD/MM/YY

0.010”0.005” 0.5 O

External Structure Assembly

USUsat-STRUCT-01

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-01

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 3: 3.1 kg

0.586 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Top Isogrid Panel

USUsat-STRUCT-02-A

1 of 2

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-02

-A1

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 4: 3.1 kg

0.586 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Top Isogrid Panel Hole Pattern

USUsat-STRUCT-02-B

2 of 2

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-02

-B2

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 5: 3.1 kg

0.583 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Bottom Isogrid Panel

USUsat-STRUCT-03-A

1 of 2

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-03

-A1

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 6: 3.1 kg

0.583 kg

Ashby, B.

Lewis, B..

01/03/01

02/03/01

0.010”0.005” 0.5 O

Bottom Isogrid Panel Hole Pattern

USUsat-STRUCT-03-B

2 of 2

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-03

-B2

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 7: 3.1 kg

.089 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Side Panel #1

USUsat-STRUCT-04

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-04

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 8: 3.1 kg

0.163 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Nadir External Panel

USUsat-STRUCT-05-A

1 of 2

None Required

None Required

US

Us

at-ST

RU

CT

-05

-A1

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Delrin

Non Critical

FRACTURE CLASSIFICATION

Page 9: 3.1 kg

0.163 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Nadir External Panel Hole Pattern

USUsat-STRUCT-05-B

2 of 2

None Required

None Required

US

Us

at-ST

RU

CT

-05

-B2

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Delrin

Non Critical

FRACTURE CLASSIFICATION

Page 10: 3.1 kg

0.149 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Side Panel #2

USUsat-STRUCT-06

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-06

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non Critical

FRACTURE CLASSIFICATION

Page 11: 3.1 kg

0.149 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Side Panel #3

USUsat-STRUCT-07

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-07

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 12: 3.1 kg

0.148 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Side Panel #4

USUsat-STRUCT-08

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-08

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non FC or FC

FRACTURE CLASSIFICATION

Page 13: 3.1 kg

0.148 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Side Panel #5

USUsat-STRUCT-09

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-09

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non Critical

FRACTURE CLASSIFICATION

Page 14: 3.1 kg

0.150 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Side Panel #6

USUsat-STRUCT-10

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-10

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T651

Non Critical

FRACTURE CLASSIFICATION

Page 15: 3.1 kg

0.190 kg

Ashby, B.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Aluminum Honeycomb Panel

USUsat-STRUCT-11

1 of 1

None Required

Irridite Class 3 per MIL-C-5541

US

Us

at-ST

RU

CT

-11

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 2024T3 Skins, 5052-0015-3.4 core

Non Critical

FRACTURE CLASSIFICATION

Page 16: 3.1 kg

Lewis, B. 02/03/01

0.010”0.005” 0.5 O

Assembly View of Deployable Antennas

USUSat-DEPLOY-01

1 of 1

None Required

TBD

US

US

at-DE

PL

OY

-01

1 o

f 11

MATERIAL:

Multiple

Non FC or FC

FRACTURE CLASSIFICATION

Page 17: 3.1 kg

TBD kg

Suisse, B.

Lewis, B.

10/02/01

20/02/01

0.010”0.005” 0.5 O

Delrin Post

USUSat-DEPLOY-02

1 of 1

None Required

TBD

US

US

at-DE

PL

OY

-02

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Delrin

Non-Critical

FRACTURE CLASSIFICATION

Page 18: 3.1 kg

x.xxx kg

Holemans, W.

Lewis, B.

05/02/01

10/02/01

0.010”0.005” 0.5 O

PSC Tensioner

USUSat-DEPLOY-03

1 of 1

None Required

TBD

US

US

at-DE

PL

OY

-03

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Material Here

Non Critical

FRACTURE CLASSIFICATION

Page 19: 3.1 kg

x.xxx kg

Starsys

SSE, Etc.

05/01/01

10/01/01

0.010”0.005” 0.5 O

Starsys EP-5025 Pin Puller

USUSat-DEPLOY-04

1 of 1

None Required

TBD

US

US

at-DE

PL

OY

-04

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Multiple

Non Critical

FRACTURE CLASSIFICATION

Page 20: 3.1 kg

Lewis, B. 02/03/01

0.010”0.005” 0.5 O

USUSat-DEPLOY-05

1 of 1

US

US

at-DE

PL

OY

-05

1 o

f 11

Copper Beryllium Tape

Non Critical

FRACTURE CLASSIFICATION

Page 21: 3.1 kg

TBD kg

Harrison, R.

Lewis, B.

10/02/01

20/02/01

0.010”0.005” 0.5 O

Pin Puller Bracket

USUSat-DEPLOY-06

1 of 1

None Required

TBD

US

US

at-DE

PL

OY

-06

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 22: 3.1 kg

Harrison, R.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Delrin Washer

USUSat-DEPLOY-07

1 of 1

None Required

TBD

US

US

at-DE

PL

OY

-07

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Delrin

Non Critical

FRACTURE CLASSIFICATION

Page 23: 3.1 kg

Lewis, B. 02/03/01

Gimbal Assembly Drawings

USUSat-GIMBAL-01

1 of 1

US

US

at-GIM

BA

L-01

1 o

f 11

Multiple

Page 24: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Cover Plate C2

USUSat-GIMBAL-02

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-02

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 25: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Cover Plate C1

USUSat-GIMBAL-03

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-03

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 26: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Cover Plate B

USUSat-GIMBAL-04

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-04

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 27: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Cover Plate A1

USUSat-GIMBAL-05

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-05

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 28: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Cover Plate A2

USUSat-GIMBAL-06

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-06

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 29: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Spacer

USUSat-GIMBAL-07

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-07

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 30: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Locking Mechanism

USUSat-GIMBAL-08

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-08

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 31: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Magnet Spindle

USUSat-GIMBAL-09-A

1 of 2

None Required

TBD

US

US

at-GIM

BA

L-09

-A1

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 32: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Magnet Spindle

USUSat-GIMBAL-09-B

2 of 2

None Required

TBD

US

US

at-GIM

BA

L-09

-B2

of 2

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 33: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Main Support #1

USUSat-GIMBAL-10

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-10

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 34: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Main Support #2

USUSat-GIMBAL-11

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-11

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 35: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Reaction Wheel Rod

USUSat-GIMBAL-12

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-12

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 36: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Reaction Wheel

USUSat-GIMBAL-13

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-13

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 37: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Arm Cover

USUSat-GIMBAL-14

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-14

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 38: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Worm Rod 1

USUSat-GIMBAL-15

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-15

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 39: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Worm Rod 2

USUSat-GIMBAL-16

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-16

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 40: 3.1 kg

TBD kg

Florin, D. 10/12/00

0.010”0.005” 0.5 O

Gimbal Worm Rod 3

USUSat-GIMBAL-17

1 of 1

None Required

TBD

US

US

at-GIM

BA

L-17

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Aluminum 6061-T6

Non-Critical

FRACTURE CLASSIFICATION

Page 41: 3.1 kg

TBD kg

Gettamaneni, K.

Lewis, B.

25/01/01

20/02/01

0.010”0.005” 0.5 O

USUSat DC Probe Patch

USUSat-ANTENN-01

1 of 1

None Required

TBD

US

US

at-AN

TE

NN

-011

of 1

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Multiple

Non-Critical

FRACTURE CLASSIFICATION

Page 42: 3.1 kg

TBD kg

Gettamaneni, K.

Lewis, B.

25/01/01

20/02/01

0.010”0.005” 0.5 O

USUSat Downlink Patch

USUSat-ANTENN-02

1 of 1

None Required

TBD

US

US

at-AN

TE

NN

-021

of 1

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Multiple

Non-Critical

FRACTURE CLASSIFICATION

Page 43: 3.1 kg

USUSat-BATT-02-A

US

US

at-BA

TT

-02-A

1 o

f 21

Page 44: 3.1 kg

USUSat-BATT-02-B

US

US

at-BA

TT

-02-B

2 o

f 21

Page 45: 3.1 kg

USUSat-BATT-03-A

US

US

at-BA

TT

-03-A

1 o

f 21

Page 46: 3.1 kg

USUSat-BATT-03-B

US

US

at-BA

TT

-03-B

2 o

f 21

Page 47: 3.1 kg

USUSat-BATT-04-A

US

US

at-BA

TT

-04-A

1 o

f 21

Page 48: 3.1 kg

USUSat-BATT-04-B

US

US

at-BA

TT

-04-B

2 o

f 21

Page 49: 3.1 kg

USUSat-BATT-05-A

US

US

at-BA

TT

-05-A

1 o

f 61

Page 50: 3.1 kg

USUSat-BATT-05-B

US

US

at-BA

TT

-05-B

2 o

f 61

Page 51: 3.1 kg

USUSat-BATT-05-C

US

US

at-BA

TT

-05-C

3 o

f 61

Page 52: 3.1 kg

USUSat-BATT-05-D

US

US

at-BA

TT

-05-D

4 o

f 61

Page 53: 3.1 kg

USUSat-BATT-05-E

US

US

at-BA

TT

-05-E

5 o

f 61

Page 54: 3.1 kg

USUSat-BATT-05-F

US

US

at-BA

TT

-05-F

6 o

f 61

Page 55: 3.1 kg

USUSat-BATT-06-A

US

US

at-BA

TT

-06-A

1 o

f 21

Page 56: 3.1 kg

USUSat-BATT-06-B

US

US

at-BA

TT

-06-B

2 o

f 21

Page 57: 3.1 kg

x.xxx kg

JHU APL

Sean Findlay

11/04/00

01/18/01

0.010”0.005” 0.5 O

Crosslink and GPS Chassis

USUSat-XLINK-1

1 of 1

None Required

TBD

US

US

at-XL

INK

-01

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Multiple

Non Critical

FRACTURE CLASSIFICATION

Side View

Top View

Page 58: 3.1 kg

x.xxx kg

0.010”0.005” 0.5 O

CNS T/R switch and isolator

USUSat-XLINK-02

1 of 1

None Required

TBD

US

US

at-XL

INK

-02

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Multiple

Non Critical

FRACTURE CLASSIFICATION

1.0

1.0

0.5

CNS transmit/receive switch

CNS isolator

Page 59: 3.1 kg

Lewis, B. 02/03/01

0.010”0.005” 0.5 O

Solar Arrays #1 & #2

USUSat-SOLARC-01

1 of 1

US

US

at-SO

LA

RC

-011

of 1

1

Multiple

FRACTURE CLASSIFICATION

Page 60: 3.1 kg

Lewis, B. 02/03/01

0.010”0.005” 0.5 O

Solar Array #3

USUSat-SOLARC-02

1 of 1

US

US

at-SO

LA

RC

-021

of 1

1

MATERIAL:

Multiple

FRACTURE CLASSIFICATION

Page 61: 3.1 kg

Lewis, B. 02/03/01

Solar Array #4

USUSat-SOLARC-03

1 of 1

US

US

at-SO

LA

RC

-031

of 1

1

MATERIAL:

Multiple

Page 62: 3.1 kg

Lewis, B. 02/03/01

Solar Array #5

USUSat-SOLARC-04

1 of 1

US

US

at-SO

LA

RC

-041

of 1

1

MATERIAL:

Multiple

Page 63: 3.1 kg

Lewis, B. 02/03/01

Solar Array #6 - #10

USUSat-SOLARC-05

1 of 1

US

US

at-SO

LA

RC

-051

of 1

1

MATERIAL:

Multiple

Page 64: 3.1 kg

Lewis, B. 02/03/01

Solar Epoxy Arrays #1 & #2

USUSat-SOLARC-046

1 of 1

US

US

at-SO

LA

RC

-061

of 1

1

MATERIAL:

Multiple

Page 65: 3.1 kg

Lewis, B. 02/03/01

Solar Epoxy Array #3

USUSat-SOLARC-047

1 of 1

US

US

at-SO

LA

RC

-071

of 1

1

MATERIAL:

Multiple

Page 66: 3.1 kg

Lewis, B. 02/03/01

Solar Epoxy Array #4

USUSat-SOLARC-08

1 of 1

US

US

at-SO

LA

RC

-081

of 1

1

MATERIAL:

Multiple

Page 67: 3.1 kg

Lewis, B. 02/03/01

Solar Epoxy Array #5

USUSat-SOLARC-09

1 of 1

US

US

at-SO

LA

RC

-091

of 1

1

MATERIAL:

Multiple

Page 68: 3.1 kg

Lewis, B. 02/03/01

Solar Epoxy Arrays #6 - #10

USUSat-SOLARC-010

1 of 1

US

US

at-SO

LA

RC

-101

of 1

1

MATERIAL:

Multiple

Page 69: 3.1 kg

Lewis, B. 02/03/01

Kapton Sheets #1 & #2

USUSat-SOLARC-11

1 of 1

US

US

at-SO

LA

RC

-111

of 1

1

MATERIAL:

Kapton

Page 70: 3.1 kg

Lewis, B. 02/03/01

Kapton Sheet #3

USUSat-SOLARC-012

1 of 1

US

US

at-SO

LA

RC

-121

of 1

1

Kapton

Page 71: 3.1 kg

Lewis, B. 02/03/01

Kapton Sheet #4

USUSat-SOLARC-13

1 of 1

US

US

at-SO

LA

RC

-131

of 1

1

Kapton

Page 72: 3.1 kg

Lewis, B. 02/03/01

Kapton Sheet #5

USUSat-SOLARC-14

1 of 1

US

US

at-SO

LA

RC

-141

of 1

1

Kapton

Page 73: 3.1 kg

Lewis, B. 02/03/01

Kapton Sheet #6

USUSat-SOLARC-15

1 of 1

US

US

at-SO

LA

RC

-151

of 1

1

Kapton

Page 74: 3.1 kg
Page 75: 3.1 kg
Page 76: 3.1 kg

Lewis, B. 02/03/01

Delrin Rear Mount

USUSat-BOOM-003

1 of 1

US

US

at-BO

OM

-00

31

of 1

1

Delrin

Page 77: 3.1 kg

Lewis, B. 02/03/01

Magnetometer Mount

USUSat-BOOM-004

1 of 1

US

US

at-BO

OM

-00

41

of 1

1

Delrin

Page 78: 3.1 kg

Lewis, B. 02/03/01

Science Boom Mount

USUSat-BOOM-005

1 of 1

US

US

at-BO

OM

-00

51

of 1

1

Delrin

Page 79: 3.1 kg

Lewis, B. 02/03/01

Magnetometer Tube

USUSat-BOOM-006

1 of 1

US

US

at-BO

OM

-00

61

of 1

1

Al 6061-T6

Page 80: 3.1 kg

Lewis, B. 02/03/01

Science Antenna Tube

USUSat-BOOM-007

1 of 1

US

US

at-BO

OM

-00

71

of 1

1

Al6061-T6

Page 81: 3.1 kg

Lewis, B. 02/03/01

Delrin Guide

USUSat-BOOM-0048

1 of 1

US

US

at-BO

OM

-00

81

of 1

1

Delrin

Page 82: 3.1 kg

Lewis, B. 02/03/01

Motor Mount

USUSat-BOOM-009

1 of 1

US

US

at-BO

OM

-00

91

of 1

1

Delrin

Page 83: 3.1 kg

Lewis, B. 02/03/01

Science Outer Tube

USUSat-BOOM-010

1 of 1

US

US

at-BO

OM

-01

01

of 1

1

Al 60610-T6

Page 84: 3.1 kg

Lewis, B. 02/03/01

Non-Conductive Tube

USUSat-BOOM-011

1 of 1

US

US

at-BO

OM

-01

11

of 1

1

Delrin

Page 85: 3.1 kg

Lewis, B. 02/03/01

Lead Screw

USUSat-BOOM-012

1 of 1

US

US

at-BO

OM

-01

21

of 1

1

Stainless Steel

Gettamaneni, K. 01/03/01

0.010”0.005” 0.5 O

None Required

TBD

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Page 86: 3.1 kg

Gettamaneni, K.

Lewis, B.

01/03/01

02/03/01

0.010”0.005” 0.5 O

Worm Gear Sleeve

USUSat-BOOM-013

1 of 1

None Required

TBD

US

US

at-BO

OM

-01

31

of 1

1

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Al 6061-T6

Non Critical

FRACTURE CLASSIFICATION

Page 87: 3.1 kg

TBD kg

Gettamaneni, K.

Lewis, B.

25/01/01

20/02/01

0.010”0.005” 0.5 O

Plasma Impedance Probe Patch (THIS IS FOR UW & VT ONLY, OUR SCIENCE BOOM DOES THIS FOR US)

NA

1 of 1

None Required

TBD

NA

1 o

f 11

I O N - FUtah State University - University of Washington - Virginia Tech.

MATERIAL:

Multiple

Non-Critical

FRACTURE CLASSIFICATION