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Artifact: Relief Valve, Liquid Hydrogen Fuel Tank, Saturn IB Second Stage and Saturn V Third Stage (S-IVB)

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Identifier: A20120054
Artifact Category: Rocket Propulsion Systems
Period of Employment: November 9 1967 to July 15 1975
Manufacturer: W.O. Leonard Inc.
NASA Contract Number: NAS7-101
Spacecraft/Launch Systems: Saturn I/IB,Saturn V

Aluminum, Stainless Steel, Teflon

Dimensions: 8.75 x 8.25 x 5.5 (Inches)
Weight: 5.6 (Pounds)
Flight Vehicle System or Component: Propellant Venting
Program: Apollo
Flown Status: Unflown

A Saturn V Third Stage (S-IVB) Fuel Tank Relief Valve utilized in conjunction with the Liquid Hydrogen (LH2) Cryogenic storage tank and propellant distribution system; manufactured by subcontractor W.O. Leonard Inc (Pasadena, California) un behalf of Douglas Aircraft Company (Prime S-IVB) for NASA contract NAS7-101. This component was part of the vent and relief system capable of relieving all excess pressure accumulated from over-pressurization or fuel boil-off during fill and flight operation.

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