Paper discusses analyses conducted on realistic orbital launch booster vehicles utilizing cryogenic propellants; effect on design of cryogenic stages of propellant performance, orbital storage period, and space environment is described, as is influence of design variations upon propellant loss rate in orbit of realistic orbital launch boosters; thermal analysis from boost and transition through orbital conditions is presented.
Orbital storage of cryogenic propellants for rendezvous missions
SAE -- Paper
SAE Meeting ; 1962 Boosters
1962
14 pages
Aufsatz (Konferenz)
Englisch
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Orbital Storage of Cryogenic Propellants for Rendezvous Missions
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