Item Details

Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber With Development of an Optimized Design [microform]

Mary E. Wadel
Format
Book; Government Document; Microform
Published
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1998].
Language
English
Series
NASA/TM
NASA Technical Memorandum
SuDoc Number
NAS 1.15:206313
Description
viii, 69 leaves : ill.
Notes
"January 1998."
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche : negative.
Series Statement
NASA/TM ; 1998-206313
NASA technical memorandum 206313
Technical Details
  • Access in Virgo Classic

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    a| Rocket engines x| Combustion.
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