Theory indicates that certain combinations of propellants have greater propulsive capability than either propellant alone; optimum performance results from suitably programmed variation of propellant proportions throughout burning; results applicable to first stage of rocket presented.
Optimum proportioning of two propellants to obtain maximum burnt velocity
ARS -- J
ARS Journal ; 29 , n 8
1959
3 pages
Aufsatz (Zeitschrift)
Englisch
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