5 . . . 4 . . . 3 . . . 2 . . . 1 . . . space launch system...flight of space launch system. among...
TRANSCRIPT
SPACE LAUNCH SYSTEM
National Aeronautics and Space Administration
www.nasa.gov/sls
5 . . . 4 . . . 3 . . . 2 . . . 1 . . .
SLS at Critical Design Review
Todd MaySpace Launch System Program
https://ntrs.nasa.gov/search.jsp?R=20150019522 2020-06-29T23:15:08+00:00Z
www.nasa.gov/sls
www.nasa.gov/sls
RS-25 Engines
Core StageCore Stage
SLS Block 2 CargoSLS Block 1B Crew SLS Block 1B Cargo
Interstage
Advanced
Boosters
Solid
Rocket
Boosters
Exploration
Upper Stage
SLS Block 1
Orion
Launch
Abort
System
Launch Vehicle
Stage Adapter
Interim Cryogenic
Propulsion Stage
Exploration
Upper Stage
Cargo FairingCargo Fairing
Interstage
Universal
Stage Adapter
Solid
Rocket
Boosters
Core Stage
SLS Evolution Overview
8796_NSC Presentation_.3
www.nasa.gov/sls
SLS Block 1B & Mission Element Concepts Under Study
Mission concepts
with Universal Stage Adaptor
Co
re S
tag
e / B
oo
ster
sE
xplo
rati
on
Up
per
Sta
ge
Mis
sio
n E
lem
ents
Mission concepts
with 8m and 10m fairings
total mission volume = ~
Orion with
short-duration
hab module
30’ tall x 27.6’ dia
400m3
5m fairing w/robotic
lunar lander & short-
duration hab module
600m3
Science
Missions
400m3
ARM Mission
400m3
8m fairing with large
aperture telescope
1200m3
10m fairing w/notional
Mars payload
1800m38796_NSC Presentation_.4
www.nasa.gov/sls
• Thirteen small-sat secondary
payloads of 6U volume/mass (14 kg
payload mass) will fly on the first
flight of Space Launch System.
Among the potential payloads are these three
candidates identified by NASA’s Advanced
Exploration Systems:
– BioSentinel: Study radiation-induced DNA
damage of live organisms in cislunar
space; correlate with measurements on
ISS and Earth.
– Lunar Flashlight: Locate ice deposits in the
moon’ permanently shadowed craters
– Near Earth Asteroid (NEA) Scout:
Flyby/rendezvous and characterize one
NEA that is a candidate for a human
mission.
Secondary Payload Capability
8796_NSC Presentation_.5
www.nasa.gov/sls
STATE OF THE ROCKET
8796_NSC Presentation_.6
www.nasa.gov/sls8796_NSC Presentation_.9
www.nasa.gov/sls8796_NSC Presentation_.10
www.nasa.gov/sls8796_NSC Presentation_.11
www.nasa.gov/sls8796_NSC Presentation_.12
www.nasa.gov/sls8796_NSC Presentation_.13
www.nasa.gov/sls8796_NSC Presentation_.14
www.nasa.gov/slsNASA ProvidedBoeing Provided
CRD (0/3)
FC (3/3)
CCSE (1/2)TAC (4/4) DACU (3/3) CLSS (1/1)
ANTENNAS (4/4)
RINU (1/1)
Cables
Coldplates (23/23) &
Envir Cntrl
Physical Structure Elect &
Ground
Power
PBOB (2/2) Lab Monitor & Control
Boeing/NASA Provided
MDAU (2/2)CTC (0/2)
OFI XMTR (1/1)
PDCU (0/2)
UBOB (2/2)
CBOB (3/3)
CCU (0/1)
EGSE
ARTEMIS/MAE
STRO
HW/SW
RDAU (1/2)
CAPUC (4/4)
DBOB (23/23)
www.nasa.gov/sls8796_NSC Presentation_.16
www.nasa.gov/sls8796_NSC Presentation_.17
www.nasa.gov/sls8135_SLS_Ambassador_11
The Adventure Begins NOW.
Join Us on The Journey!
8786 Adv. Rocketry Workshop.18