Performance is presented in graphical form suited for systems designer interested in visualizing relationships between motor propellant fraction, size of total propulsion system in relation to payload, and burnout velocity; derivation of coefficients that allow direct comparison of relative importance of characteristics of each stage.
Ideal performance of multistage rockets
ARS -- J
ARS Journal ; 30 , n 6
1960
6 pages
Aufsatz (Zeitschrift)
Englisch
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