Liquid rocket metal tanks and tank components, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8088, Wagner, W. A., Liquid rocket metal tanks and tank components, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), May,1974, pp. 165, Format(s): PDF 16716k

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Significant guidelines are presented for the successful design of aerospace tanks and tank components, such as expulsion devices, standpipes, and baffles. The state of the art is reviewed, and the design criteria are presented along with recommended practices. Design monographs are listed.

Keywords:	spacecraft propulsion and power, propellant tanks, space storage, construction materials, payloads, spacecraft design, systems engineering, tank geometry
CASI Document ID Number:	75N13022
Subjects:	Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:	156
Deposited On:	23 May 2002