Relatively simple and straightforward method of determining this trade off and some typical trade off values are given; method is general with respect to vehicle performance or design criteria and is illustrated for case where multistage vehicle's inert parts weights and propellant volumes are fixed and given vehicle burnout velocity is to be maintained.
Trade-off between propellant specific impulse and density
Aerospace Eng
Aerospace Engineering ; 20 , n 11
1961
Aufsatz (Zeitschrift)
Englisch
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