Feasibility study of two- or three-stage horizontal takeoff launch vehicle assuming orbit delivery of one ton load with 3300 fps velocity reserve to space laboratory orbiting at 200 mi; analysis includes concept of two recoverable vehicles and discusses configuration, separation, return, and propulsion; design assumes use of conventional airports.
French concept for aerospace transporter
SAE -- Space Technology Conf
Proceedings of the Space Technology Conference ; 1967 Reusable
1967
10 pages
Conference paper
English
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A French Concept for an Aerospace Transporter
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