Development of rocket motor having thrust of six tons, to be used in high-energy upper stages; construction details and arrangement with special reference to turbopump-feed systems presently available; development requirements are outlined and possible further development of rocket engine is indicated.
Investigation of high-energy standard propulsion unit for ELDO-B launch vehicle
Untersuchungen zu einem hochenergetischen Einheitstriebwerk fuer die ELDO-B Traegerraketen
Raumfahrtforschung ; 9 , n 4
1965
7 pages
Aufsatz (Zeitschrift)
Deutsch
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NTIS | 1993
|British Library Online Contents | 1994
TIBKAT | 1993
|SLUB | 1993
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