Objectives: Measure Pressure: a) Confirm spacecraft aerodynamics. b) Independently measure attitude. c) Determine density profile. d) Determine wind component. Measure Temperature: a) Verify heating levels on spacecraft surface. b) Determine recession amount and rate. c) Validate material response at Mars conditions. The better we understand the Mars entry environment, the better we can design the next spacecraft.
Entry Descent and Landing Workshop Proceedings
AAS/AIAA Spaceflight Mechanics Meeting ; 2013 ; Kauai, HI, United States
2013-02-12
Miscellaneous
No indication
English
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