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Performance Charts for Multistage Rocket BoostersCharts 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.
Document ID
20020060129
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
MacKay, John S.
(NASA Lewis Research Center Cleveland, OH United States)
Weber, Richard J.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1961
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
E-799
NASA-TN-D-582
Report Number: E-799
Report Number: NASA-TN-D-582
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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