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Design of the Core Stage Inter-Tank Umbilical {CSITU) Compliance MechanismProject Goals: a) Design the compliance mechanism for the CSITU system to a 30% level -3D models completed in Pro/Engineer -Relevant design analysis b) Must meet all system requirements and establish basis for proceeding with detailed design. Tasks to be completed: A design that meets requirements for the 30% design review, 01/16/2013. Umbilical arms provide commodities to the launch vehicle prior to T-0. Commodities can range anywhere from hydraulics, pneumatics, cryogenic, electrical, ECS, etc ... Umbilicals commonly employ truss structures to deliver commodities to vehicle. Common configurations include: -Tilt-up -Swing Arm -Hose Drape -Drop Arm Umbilical arms will be mounted to Mobile Launch Platform. SLS currently has 9 T-0 umbilical arms. The compliance refers to the ability of the umbilical to adjust to minor changes in vehicle location. The compliance mechanism refers to the mechanism on the ground support equipment {GSE) that compensates for these changes. For the CSITU, these minor changes, or vehicle excursions, can be up to +4 in. Excursions refer to movements of the vehicle caused by wind loads and thermal expansion. It is ideal to have significant vertical compliance so a passive secondary release mechanism may be implemented.
Document ID
20130014287
Acquisition Source
Kennedy Space Center
Document Type
Presentation
Authors
Smith, Kurt R.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 27, 2013
Publication Date
May 3, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
KSC-2013-119
Report Number: KSC-2013-119
Meeting Information
Meeting: Kennedy Engineering Academy Accelerated Training Program Showcase
Location: Cocoa Beach , FL
Country: United States
Start Date: May 3, 2013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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