Concept of Saturn V derivative launch vehicle systems, their performance capabilities, and their ability to perform orbital and high-energy missions at minimum total program cost; these derivative configurations have payload capability range extending from that of Saturn IB to postulated manned planetary vehicle requirements which might include placing larger nuclear modules/ stages in rendezvous compatible orbits about earth; vehicle and facilities design commonality and impact are summarized.
Saturn V derivatives
SAE -- Proc
Proceedings of Space Technology Conference ; 1968 Launching
1968
15 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
SAE Technical Papers | 1968
|NTRS | 1968
|Saturn OUTLOOK, Saturn AURA, Saturn PREVUE
Online Contents | 2006
2007 Saturn Sky - Saturn Aura Concept
Kraftfahrwesen | 2005
|Engineering Index Backfile | 1945