Rocket control during acceleration, after launch to the first stage was studied. Systems in use were analyzed, and auxiliary propulsion was chosen for the investigation. It is concluded that the selected system requires the use of a gyroscope, free in three geometries, with primary sensory elements, and four activating servomotors for four auxiliary rocket engines.
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 2 . 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, Tomo 2
1972
34 pages
Report
Keine Angabe
Englisch
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