High altitude launch platform payload launching apparatus and me

Aeronautics and astronautics – Composite aircraft

Patent

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244 63, 244158R, 244172, B64G 114

Patent

active

052956423

ABSTRACT:
A high altitude launch platform, used to launch a payload into earth orbit, is part of a payload launch system having a payload launching rocket carried by the high altitude launch platform. A first amount of fuel, substantially less than the capacity of the fuel tanks, is provided to the launch platform while the launch platform is on the ground. The launch platform is flown to a first altitude and the fuel tanks are provided with a second amount of fuel while the high altitude launch platform is at the first altitude. The addition of the second amount of fuel is sufficient to allow the payload to be launched into orbit.

REFERENCES:
patent: 1703488 (1929-02-01), Junkers
patent: 3369771 (1968-02-01), Walley et al.
patent: 4650139 (1987-03-01), Taylor et al.
patent: 4834324 (1989-05-01), Criswell
patent: 5129602 (1992-07-01), Leonard
EPO 0264030, Apr. 1988, Hardy et al.
Salkeld, "Single-Stage Shuttles for Ground Launch and Air Launch", Astronautics Aeronautics, Mar. 1974 pp. 52-64.
Peebles, "Air Launched Shuttle Concepts" Brit. Interplanetary Soc., Apr. 1983, vol. 36 No. 4 pp. 153-155.

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