Aeromaneuvering Orbit Transfer Vehicles for the space transport systemAlternatives to all-propulsive manned Orbit Transfer Vehicles (OTV) are presented that utilize aeromaneuvering in combination with propulsive maneuvering. A summary of the results of feasibility and concept definition studies is induced along with a discussion of the advantages and disadvantages of aeromaneuvering as compared with all-propulsive vehicles. Manned aeromaneuvering OTV concepts are described, including the Aeromaneuvering Orbit-to-Orbit Shuttle (AMOOS) for future orbital transportation and the Aeromaneuvering Recovery System (AMRS) for emergency recovery of crewmen from high-altitude orbits. Data are provided regarding aeromaneuvering OTV configurations, performance, systems, tradeoffs, mission applications, and major design parameters, such as dynamic pressure, heating rates, and guidance.
Document ID
19760063105
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hethcoat, J. P. (NASA Marshall Space Flight Center Huntsville, Ala., United States)
White, J. (Lockheed Missiles and Space Co., Inc. Huntsville, Ala., United States)