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Propellant potential of vaporized metals in temperature-limited rocket systems.Light metallic elements in association with hydrogen as carrier fluid for rocket propulsion
Document ID
19650028903
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Glassman, I.
Mellor, A. M.
Sawyer, R. F.
Date Acquired
August 2, 2013
Publication Date
November 1, 1964
Subject Category
Propellants
Accession Number
65A11607
Funding Number(s)
CONTRACT_GRANT: AF 49/638/-1268
CONTRACT_GRANT: NSG-641
Distribution Limits
Public
Copyright
Other
Keywords
PROPELLANT
ELECTROTHERMAL ENGINE
METAL VAPOR

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