Weight savings advantage of catalyzed hydrogen rocket propellant, discussing specific impulse and tankage volume
Possible weight saving from catalysis of recombination in hydrogen rockets.
1968-01-01
Miscellaneous
No indication
English
NASA includes foreign rockets as possible launchers
Online Contents | 2004
Cost and weight optimization for multistage rockets
AIAA | 1965
|Optimum Stage Weight Distribution of Multistage Rockets
AIAA | 1973
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