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Technology considerations for main engine specific impulseCombustion, cooling, nozzle design, and specific impulse prediction for space shuttle main engine
Document ID
19700030311
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kors, D. L. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Publication Information
Publication: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 4 JUL. 1970
Subject Category
Propulsion Systems
Accession Number
70N39627
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitleCollected Works19700030310Collected WorksSpace Transportation System Technology Symposium: Propulsion - Volume 419700030310Collected WorksSpace Transportation System Technology Symposium: Propulsion - Volume 4N70-39626 22-31Collected Works
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