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Present techniques and problems in the determination of the base heating environment of propelled boost and space vehicles.Short duration technique for determining base heating of tail ends of multiengine rocket vehicle from exhaust jets
Document ID
19650031617
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dahm, W. K.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Propulsion Systems
Accession Number
65A14321
Distribution Limits
Public
Copyright
Other
Keywords
BASE HEATING
CONVECTIVE HEAT TRANSFER
ROCKET EXHAUST
SEPARATED FLOW

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