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PROGRAM UPDATEMarch 2012
History
FY05 FY06 FY07 FY08 FY09 FY10 FY11
Orion Contract Awarded
Pad Abort 1 Flight Test Vehicle Built
Launch Abort Motor Test
Orion Water Landing Recovery Training
Heat ShieldPrototype Developed
Orion Crew Exploration Vehicle ConceptDeveloped
ParachuteTests
LAS Attitude Control Motor Test
Orion namedMulti-Purpose Crew Vehicle
May 2011
Phase I: Design Trades Phase II: Spacecraft Development MPCV
Pad
Abort 1 Stacking
Pad Abort 1Flight Test
SuccessMay 2010
First Orion Environmental Testing
Source: NASA
3
Launch Abort System and Crew ModuleAcoustic and Vibration Tests
3Image Credit: Lockheed Martin
Lockheed Martin Reverberant Acoustic Laboratory – Denver, Colorado- Full-Scale Spacecraft Testing- Simulates Launch Acoustic Forces & Vibrations - Validates Structural Integrity of the Spacecraft
4
Vibration Tests in VTF
4Image Credit: Lockheed Martin
Exploration Flight Test 1
5
Upper Stage 1st Engine Start
Upper Stage 1st Engine Cut-OffUpper Stage
2nd Engine Start
Upper Stage 2nd Engine Cut-Off
Boost Stage 1
Upper Stage Burn
Coast
EFT-1 Overview• 2 Revolutions • Low Inclination• High Apogee• High Energy Entry
Recovery
CM/Upper Stage
Separation
Upper Stage Disposal Burn
CM Translation
BurnLV/Upper
Stage Sep
LAS Jettison
SM Fairing
Sep
CM Translation Burn
Source: NASA
Lunar flyby
Plymouth Rock: Humans explore asteroid 2008 EA9 and others
Explore the Moon’s far side from Earth-Moon L2 point
SLS test flight
Asteroid survey Asteroid scout
Deimos Scout
Stepping StonesA series of exploration missions building incrementally towards America’s long- term goal of exploring Mars.
A human mission to the moons of Mars will require capabilities such as heavy-lift launch ,
Red Rocks: exploreMars from Deimos
Deimos photo courtesy of NASA-JPL, University of Arizona
Notional mission concepts: Lockheed Martin
Image Credit: Lockheed Martin
For more information:
7
www.lockheedmartin.com/orion
Presentation content courtesy of NASA