The parameters of a rocket capable of velocities of 8 km/sec are determined using simplified equations of motion. Based on the analysis of the variation of weight at launch as a function of the number of stages, four stages are determined to be the optimum number. The relation of the mass of the shell to the optimum propulsion for each stage is computed.
Feasibility Study of Propulsion Systems with Velocities on the Order of 8 Km/Second and Payloads of 50 Kilograms, and Control and Guidance Systems for Rockets, Part 1 . Estudio de Factibilidad Sobre Sistema de Propulsion Para Alcanzar Velocidades Del Orden de 8 Km/Seg Con Cargas Utiles de 50 Kgs Y Sobre Sistemas de Control Y Guiado Para Cohetes
1972
22 pages
Report
Keine Angabe
Englisch
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