Liquid rocket engine turbines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8110, Liquid rocket engine turbines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), January,1974, pp. 158, Format(s): PDF 8105k

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Criteria for the design and development of turbines for rocket engines to meet specific performance, and installation requirements are summarized. The total design problem, and design elements are identified, and the current technology pertaining to these elements is described. Recommended practices for achieving a successful design are included.

Keywords:	propulsion systems, liquid propellant rocket engines, rocket engine design, turborocket engines, engine parts, performance prediction, space shuttles, technology assessment
CASI Document ID Number:	74N34245
Subjects:	Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:	160
Deposited On:	23 May 2002