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- W966256265 abstract "Charts relating the stage propellant fractions are given for two-and three-stage rockets launching payloads into nominal low-altitude circular orbits about the earth. A simple method is described for extending these data to higher orbit or escape missions. Various combinations of stages using RP - liquid-oxygen and hydrogen - liquid-oxygen propellants are considered. However, the results can be generalized with little error to any other propellant combination.Charts relating the stage propellant fractions are given for two-and three-stage rockets launching payloads into nominal low-altitude circular orbits about the earth. A simple method is described for extending these data to higher orbit or escape missions. Various combinations of stages using RP - liquid-oxygen and hydrogen - liquid-oxygen propellants are considered. However, the results can be generalized with little error to any other propellant combination." @default.
- W966256265 created "2016-06-24" @default.
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- W966256265 date "1961-01-01" @default.
- W966256265 modified "2023-09-27" @default.
- W966256265 title "Performance Charts for Multistage Rocket Boosters" @default.
- W966256265 hasPublicationYear "1961" @default.
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