Basic principles and assumptions in calculating rocket combustion characteristics; outline of method commonly accepted for determining theoretical performance of rocket motors with different propellants; computed results for various propellant combinations are given and discussed. Based on Chapter IV of author's forthcoming book, "Rocket Propulsion Elements".
Thermochemistry of rocket propellants
Am Rocket Soc -- J
ARS Journal ; n 72
1947
8 pages
Article (Journal)
English
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