Experimentally determined heat transfer data obtained on JP-4 and RFNA fuels under conditions simulating those occurring during thrust chamber operation; heat flux and temperature distribution within walls of tubular chamber cooled with JP-4 and within walls of drilled passage thrust chamber cooled with RFNA are obtained.
Analysis of regenerative cooling in rocket thrust chambers
Jet Propulsion
Jet Propulsion ; 28 , n 2
1958
7 pages
Article (Journal)
English
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Regenerative Cooling for Liquid Propellant Rocket Thrust Chambers
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