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Use of Heated Helium to Simulate Surface Pressure Fluctuations on the Launch Abort Vehicle During Abort Motor Firing
2011
17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference)
unpublished
The solid-rocket plumes from the Abort motor of the Multi-Purpose Crew Vehicle (MPCV, also know as Orion) were simulated using hot, high pressure, Helium gas to determine the surface pressure fluctuations on the vehicle in the event of an abort. About 80 different abort situations over a wide Mach number range, (0.3≤M≤1.2) and vehicle attitudes (±15º) were simulated inside the NASA Ames Unitary Plan, 11-Foot Transonic Wind Tunnel. For each abort case, typically two different Helium plume and
doi:10.2514/6.2011-2901
fatcat:4oe2o4nw4rgwxcseiwsjvfkdr4