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Independent Orbiter assessment: analysis of the electrical power generation/power reactant storage and distribution subsystem
U.S. Government
Paperback. Books LLC, Reference Series 2011-10-03.
ISBN 9781234359041
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Förlagets beskrivning
Original publisher: Houston, Tex. : McDonnell Douglas Astronautics Company, Houston Division ; [Washington, DC : National Aeronautics and Space Administration, 1986] OCLC Number: (OCoLC)69936927 Subject: Space shuttles. Excerpt: ... * The Oxygen ( 02 ) tanks flown on a mission can number from 2 to 5. The 02 reactant is stored in the tank at an initial temperature of-300 degrees F. Each tank contains heaters labeled AI, A2, B1 and B2, with one heater assembly consisting of A1 and B1 and the other containing A2 and B2. The tanks also consist of a temperature sensor for each heater assembly, fluid temperature sensor, quantity sensor, pressure sensor, heater controller pressure sensor, relief valve and port, fill QD and cap, and vent QD and cap. In a five tank configuration, the B heater in tanks 4 and 5 are not operational. Reference Figure 7. * There is an 02 Relief Valve / Filter Package for each 02 tank. All ORVFP's have a filter, plus the ones for tanks 1 and 2 contain a manifold relief valve, while those for tanks 3 and 4 contain a check valve. Reference Figure 8. There are 2 02 Valve Modules. Both OVM's contain a, check valve ( one for tank l, one for tank 2 ), a manifold shutoff valve and its position indicator, a manifold pressure sensor, and an ECLSS system supply valve and its position sensor * HVM 1 contains one fuel cell reactant supply valve and its position sensor, while HVM 2 contains two of each. HVM 1 contains a GSE valve and GSE fill T-O QD. HVM 2 contains a horizontal drain QD and cap. Reference Figure 9.. The 02 and H2 lines, components, and fittings made up a separate category outside of the six major divisions
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Independent Orbiter assessment: analysis of the electrical power generation/power reactant storage and distribution subsystem
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