Simplified equations of motion are used to calculate the dimensions of a rocket propulsion system capable of velocities of 8 km/sec with payloads of 50 kgs. The optimum mass of the rocket for the propulsion system is computed.
Facility Studies of Propulsion Systems for Velocities on the Order of 8 Km/Sec with Loads to 50 Kgs, and Rocket Control and Guidance Systems, Volume 1 . Estudio de Factibilidad Sobre Sistema de Propulsion Para Alcanzar Velocidades Del Orden de 8 Km/Sec Con Cargas Utiles de 50 Kgs Y Sobre Sistemas de Control Y Guiado Para Cohetes, Tomo 1
1971
22 pages
Report
No indication
English
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