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Dynamic performance of Surveyor throttleable engine when propellants contain dissolved helium.Surveyor throttleable liquid propellant rocket engine for operation on propellants saturated with dissolved liquid gas
Document ID
19670048105
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Breshears, R. R.
Mccafferty, J.
Mcdermott, C. E.
Date Acquired
August 3, 2013
Publication Date
May 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-949
Report Number: AIAA PAPER 66-949
Accession Number
67A26834
Distribution Limits
Public
Copyright
Other
Keywords
SURVEYOR PROJECT
PROPELLANT TRANSFER
SPACECRAFT CONTROL
LIQUID PROPELLANT ROCKET ENGINE
HELIUM

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