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Design, Development,and Testing of Umbillical System Mechanisms for the X-33 Advanced Technology DemonstratorThe X-33 Advanced Technology Demonstrator is an un-piloted, vertical take-off, horizontal landing spacecraft. The purpose of the X-33 program is to demonstrate technologies that will dramatically lower the cost of access to space. The rocket-powered X-33 will reach an altitude of up to 100 km and speeds between Mach 13 and 15. Fifteen flight tests are planned, beginning in 2000. Some of the key technologies demonstrated will be the linear aerospike engine, improved thermal protection systems, composite fuel tanks and reduced operational timelines. The X-33 vehicle umbilical connections provide monitoring, power, cooling, purge, and fueling capability during horizontal processing and vertical launch operations. Two "rise-ofF' umbilicals for the X-33 have been developed, tested, and installed. The X-33 umbilical systems mechanisms incorporate several unique design features to simplify horizontal operations and provide reliable disconnect during launch.
Document ID
20000024930
Acquisition Source
Kennedy Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Littlefield, Alan C.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Melton, Gregory S.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 1999
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS1.15:208562
NASA/TM-1999-208562
Report Number: NAS1.15:208562
Report Number: NASA/TM-1999-208562
Meeting Information
Meeting: Aerospace Mechanisms
Location: Greenbelt, MD
Country: United States
Start Date: May 10, 2000
End Date: May 12, 2000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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