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Integrated Aerodynamic Tests of the Space Shuttle Vehicle during Solid Rocket Booster Separation at Mach 4.5 (IA193)

机译:在4.5马赫(Ia193)固体火箭助推器分离期间航天飞机车辆的综合空气动力学试验

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Static force and moment tests were conducted in the VKF Tunnel A using the captive trajectory system to simulate solid rocket booster (SRB) separation maneuvers from the space shuttle orbiter/external tank at Mach 4.5. Phase I test objectives were to determine proximity interference aerodynamics of the SRBs with the booster motors active. The Phase II effort developed an expanded aerodynamic data base, up to longitudinal separation distances of 1700 in., with a single SRB and no motor modeling. Limited testing was accomplished at Mach 4.0 to determine Mach number effect. These tests are identified by NASA as IA193. (Author)

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