Liquid rocket engine fluid-cooled combustion chambers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8087, Liquid rocket engine fluid-cooled combustion chambers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), April,1972, pp. 120, Format(s): PDF 12865k

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A monograph on the design and development of fluid cooled combustion chambers for liquid propellant rocket engines is presented. The subjects discussed are (1) regenerative cooling, (2)transpiration cooling, (3) film cooling, (4) structural analysis, (5) chamber reinforcement, and (6) operational problems.

Keywords:	propulsion systems, combustion chambers, liquid propellant rocket engines, rocket engine design, cooling systems, equipment specifications, regenerative cooling, systems analysis
CASI Document ID Number:	73N31697
Subjects:	Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:	124
Deposited On:	23 May 2002