Optimum staging principles for determining relative weights of stages of solid propellant rocket vehicle are established and relative influence of specific impulse and propellant mass fraction of various stages on performance of optimized multistage system investigated.
Optimum staging of solid-propellant rocket vehicles
Astronautica Acta
Astronautica Acta ; 7 , n 2-3
1961
13 pages
Aufsatz (Zeitschrift)
Englisch
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