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Mars polar lander thruster cold start validation testingTesting conducted verified that the thruster could indeed be fired with catalyst bed temperatures.
Document ID
20210002225
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/13015
Authors
Fischer, T. L.
Frei, T. E.
Weiss, J. M.
Date Acquired
July 8, 2001
Publication Date
July 8, 2001
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
propulsion
thruster
hydrazine
engines
testing
cold
start
Mars
Polar
Lander
descent
engine

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