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- W2320159098 abstract "The Power Transfer Unit (PTU) described here becomes part of the US space shuttle Orbiter equipment, as a component of the Station/Shuttle Power Transfer System (SSPTS) and supports operation in conjunction with the International Space Station (ISS). Two of these units are installed on an existing midbody avionics shelf underneath the payload bay liner. Each PTU consists of two 120V to 32V, 2000 watt converters, and one 1800 watt 28 to 124V converter module. When docked, the 120V/32V modules operate using power supplied from the ISS power system to conserve the Orbiter’s cryogenic fuel (O2/H2) by supporting the Orbiter electrical system. The 28/124V module operates from Orbiter power to supply ISS quality power to the payload bay, supporting various ISS equipments that need active power while in transit." @default.
- W2320159098 created "2016-06-24" @default.
- W2320159098 creator A5077628019 @default.
- W2320159098 date "2005-06-19" @default.
- W2320159098 modified "2023-10-14" @default.
- W2320159098 title "A Power Converter for Manned Spacecraft from COTS Components" @default.
- W2320159098 doi "https://doi.org/10.2514/6.2005-5689" @default.
- W2320159098 hasPublicationYear "2005" @default.
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