A hydrazine gas generator system with catalytic gas generator was developed and its qualification for satellites was tested. An electrothermal gas generator was developed and tested. For the design of the gas generators EXOSAT demands were considered. Functional tests, environmental and life tests of the catalytic gas generator system show its suitability for attitude control of satellites and sondes.
Qualification of a Hydrazine Gas Generator System with Electrothermal/Catalytic Gas Generator
1984
35 pages
Report
Keine Angabe
Englisch
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