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Semi-reactive stratoplane /1932/
High altitude, high speed aircraft design parameters - thrust, combustion, and dynamics
Document ID
19650027287
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
August 2, 2013
Publication Date
November 1, 1965
Subject Category
Aircraft
Accession Number
65N36888
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THRUST
DYNAMICS
COMBUSTION
AIRCRAFT DESIGN
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