Liquid rocket pressure regulators, relief valves, hurst disks, and explosive valves, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8080, Liquid rocket pressure regulators, relief valves, hurst disks, and explosive valves, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA (Washington, DC, United States), March,1973, pp. 123, Format(s): PDF 7268k

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The development of and operational programs for effective use in design are presented for liquid rocket pressure regulators, relief valves, check valves, burst disks, and explosive valves. A view of the total design problem is presented, and design elements are identified which are involved in successful design. Current technology pertaining to these elements is also described. Design criteria are presented which state what rule or standard must be imposed on each essential design element to assure successful design. These criteria serve as a checklist of rules for a project manager to use in guiding a design or in assessing its adequacy. Recommended practices are included which state how to satisfy each of the criteria.

Keywords:	propulsion systems, equipment specifications, pressure regulators, relief valves, actuators, explosive devices, flow regulators, intake systems, liquid propellant rocket engines, rocket engine design
Accession Number:	74N10724
Subjects:	Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:	145
Deposited On:	23 May 2002