A preliminary study of a system for controlling rockets during combustions was studied in large rockets with low acceleration. A control system utilizing auxiliary engines for rocket orientation is analyzed. It is concluded that a free gyroscope with sensors in three dimensions, and four servomotors are required for actuating four auxiliary rocket engines.
Facility Studies of Propulsion Systems for Velocities on the Order of 8 Km/Sec with Loads of 50 Kgs, and Rocket Control and Guidance Systems, Volume 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
1971
34 pages
Report
Keine Angabe
Englisch
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