Various components incorporated in system are divided into propellants, pressurization and expulsions system, engines and control; most types of propellants, available for attitude control systems and aspects of various pressurization schemes and their relation to overall-system are presented; highest efficiency in attitude control can only be realized by use of small rocket engines with either pulse, continuous or controlled thrust.
Chemical rocket engines and propulsion systems for attitude control and stabilization of space vehicles
Chemische Raketentriebwerke Fuer Lageregelungssysteme von Raumfahrzeugen
Raketentechnik u Raumfahrtforschung ; 6 , n 4
1962
10 pages
Article (Journal)
German
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