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Manned spacecraft center's experience with vacuum-ignition phenomena in bipropellant reaction control engines.
Vacuum-ignition phenomena in Apollo rocket engine when oriented in upward-firing attitude
Document ID
19670055248
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chaffee, N. H.
Wiltz, J. A.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-514
Report Number: AIAA PAPER 67-514
Accession Number
67A33977
Distribution Limits
Public
Copyright
Other
Keywords
ROCKET FIRING
APOLLO PROJECT
ENGINE TESTING
VACUUM EFFECT
ROCKET ENGINE
IGNITION
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