Parametric study of vehicle size for direct-flight manned lunar mission; main parameter is take-off thrust which is influenced by many factors; close choice exists in second stage where conventional and high-energy propellants are compared; size of final stage is governed by method of approach to earth's surface.
Rocket for manned lunar exploration
IRE -- Trans Space Electronics Telemetry
IRE -- Transactions on Space Electronics and Telemetery ; SET-5 , n 4
1959
8 pages
Aufsatz (Zeitschrift)
Englisch
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