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Spatially Resolved Species Measurements in a GO2/GH2 Propellant RocketThe objective of the current work is to develop an non-intrusive technique to experimentally determine the major species and temperature field in the combustion chamber of a uni-element rocket for a GO2/GH2 propellant combination.
Document ID
19960029256
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Foust, M. J. (Pennsylvania State Univ. University Park, PA United States)
Ni, T. (Pennsylvania State Univ. University Park, PA United States)
Santoro, R. J. (Pennsylvania State Univ. University Park, PA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Publication Information
Publication: Thirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology
Subject Category
Inorganic And Physical Chemistry
Accession Number
96N29752
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19960029254Collected WorksThirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology19960029254Collected WorksThirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology
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