Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane
Title | Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane PDF eBook |
Author | National Aeronautics and Space Adm Nasa |
Publisher | Independently Published |
Pages | 26 |
Release | 2018-09-06 |
Genre | Science |
ISBN | 9781719976404 |
The feasibility of safely separating the space shuttle orbiter (140A/B) from the top of a large carrier vehicle (the C-5 airplane) at subsonic speeds was investigated. The longitudinal equations of motion for both vehicles were numerically integrated using a digital computer program which incorporates experimentally derived interference aerodynamic data to analyze the separation maneuver for various initial conditions. Separation of the space shuttle orbiter from a carrier vehicle was feasible for a range of dynamic-pressure and flight-path-angle conditions. By using an autopilot, the vehicle attitudes were held constant which ensured separation. Carrier-vehicle engine thrust, landing gear, and spoilers provide some flexibility in the separation maneuver. Wilhite, A. W. Langley Research Center NASA-TM-X-3492, L-11074 RTOP 506-26-10-08
Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane
Title | Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane PDF eBook |
Author | Alan W. Wilbite |
Publisher | |
Pages | 28 |
Release | 1977 |
Genre | Piggyback aircraft |
ISBN |
Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane
Title | Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane PDF eBook |
Author | Alan W. Wilhite |
Publisher | |
Pages | |
Release | 1977 |
Genre | |
ISBN |
The feasibility of safely separating the space shuttle orbiter (140A/B) from the top of a large carrier vehicle (the C-5 airplane) at subsonic speeds was investigated. The longitudinal equations of motion for both vehicles were numerically integrated using a digital computer program which incorporates experimentally derived interference aerodynamic data to analyze the separation maneuver for various initial conditions. Separation of the space shuttle orbiter from a carrier vehicle was feasible for a range of dynamic-pressure and flight-path-angle conditions. By using an autopilot, the vehicle attitudes were held constant which ensured separation. Carrier-vehicle engine thrust, landing gear, and spoilers provide some flexibility in the separation maneuver.
Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane
Title | Analysis of Separation of the Space Shuttle Orbiter from a Large Transport Airplane PDF eBook |
Author | Alan W. Wilbite |
Publisher | |
Pages | 28 |
Release | 1977 |
Genre | Piggyback aircraft |
ISBN |
NASA Technical Memorandum
Title | NASA Technical Memorandum PDF eBook |
Author | |
Publisher | |
Pages | 908 |
Release | 1977 |
Genre | Aeronautics |
ISBN |
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 994 |
Release | |
Genre | Aeronautics |
ISBN |
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 1294 |
Release | 1984 |
Genre | Aeronautics |
ISBN |