Study of 3-stage composite, earth satellite launching system; first stage provides power for takeoff, initial climb and acceleration to second stage ramjet starting velocity; 2 trajectories of second stage (recoverable, ramjet powered lifting vehicle) are computed on IBM 650 computer; third stage is rocket which takes its payload to orbital conditions; report is devoted mainly to performance of second stage; ramjet performance analysis and performance scaling factor.
Air-breathing satellite booster
Can Aeronautical J
Canadian Aeronautical Journal ; 7 , n 6
1961
7 pages
Article (Journal)
English
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Engineering Index Backfile | 1962
Design aspects of air breathing booster
Engineering Index Backfile | 1960
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Engineering Index Backfile | 1960
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SAE Technical Papers | 1960
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