Thermal insulation requirements of vehicles exposed for extended periods to solar space environment and heat flow paths pertaining to bipropellant liquid propulsion systems; comparison of several high energy propellant combinations is made in terms of payload capability in mission; results show that systems considered can sustain coast periods up to 15,000 hr (2 yr) without significant change in payload magnitudes.
High energy propellant comparisons for space missions
ARS J
ARS Journal ; 31 , n 5 ; p 609-613
1961
5 pages
Aufsatz (Zeitschrift)
Englisch
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