SIMULATION OF LAUNCH ABORT SYSTEM (LAS) EXHAUST PLUMES WITH DOWNSTREAM SURFACES, PHASE 3: SHOCK NOISE EFFEC…

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Award details

Award ID: NNA08BA87P
Contractor
Awarding agency: National Aeronautics and Space Administration
Sub-agency / office: National Aeronautics and Space Administration
Award amount: $0
Period of performance: Jun 20, 2008 – Aug 31, 2008
NAICS: 541712 — Research and Development in the Physical, Engineering, and Life Sciences
PSC: PSC AR31
Place of performance: FL

SIMULATION OF LAUNCH ABORT SYSTEM (LAS) EXHAUST PLUMES WITH DOWNSTREAM SURFACES, PHASE 3: SHOCK NOISE EFFECTS AND HEATED HELIUM PLUME TESTS.

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