DUAL MODE CHEMICAL ROCKET ENGINE, AND DUAL MODE PROPULSION SYSTEM COMPRISING THE ROCKET ENGINE

The invention relates generally to dual mode bipropellant chemical rocket propulsion systems to be used in aerospace applications for 1) orbit raising, orbit manoeuvres and maintenance, attitude control and deorbiting of spacecraft, and/or 2) propellant settling, attitude and roll control of missile...

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Bibliographic Details
Main Authors BERGMAN, Göran, ANFLO, Kjell
Format Patent
LanguageEnglish
French
German
Published 01.01.2020
Subjects
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