The report describes experimental studies on attitude control thrusters for satellites and space probes performed within a BMBW-supported research activity at the DFVLR in Trauen. The investigated thrusters develop a vacuum thrust of 1 to 10 N. The components of the gaseous propellant system hydrogen/oxygen are injected through a coaxial injector element. Subject of these investigations is the examination of simple methods solving thermodynamic and reaction kinetic problems by varying the injector conditions in the coaxial injector element considering minimum thruster dimensions and optimum cooling. (Author)
Untersuchungen an Zweistoff-Kleinsttriebwerken fuer Bahnkorrektur und Lageregelung (Investigation of Two-Component Propellant Thrusters for Orbit Correction and Attitude Control)
1972
7 pages
Report
Keine Angabe
Englisch
Untersuchungen an Zweistoff-Kleinsttriebwerken fuer Bahnkorrektur und Lageregelung
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