S-IVB Forward (inflight). Provides fuel tank vent, electrical, pneumatic, airconditioning, and preflight conditioning interfaces. Umbilical withdrawal by pneumatic disconnect in conjuction with pneumatic/hydralic redundant dual cylinder system. Secondary mechanical system. Arm also equipped with line handling device to protect ines during withdrawal. Retract time is 8.4 seconds (max).
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Copyright 1997-2005 by John
Duncan |