REG NASA-LLIS-0883--2000 Lessons Learned Facility Chilled Water for Thermal Conditioning Unit (TCU).pdf
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1、Best Practices Entry: Best Practice Info:a71 Committee Approval Date: 2000-04-24a71 Center Point of Contact: KSCa71 Submitted by: Wilson HarkinsSubject: Facility Chilled Water for Thermal Conditioning Unit (TCU) Practice: Use of the Facility Chilled Water (FCW) System to provide the heat exchange me
2、dium for the hypergolic propellant Thermal Conditioning Units (TCU).Programs that Certify Usage: This practice has been used on the Space Shuttle Program and the KSC Hypergolic Propellant Loading System.Center to Contact for Information: KSCImplementation Method: This Lesson Learned is based on Main
3、tainability Technique number OPS-15 from NASA Technical Memorandum 4628, Recommended Techniques for Effective Maintainability.Incorporating this technique eliminates the need and cost of a separate cooling system to be designed, installed and maintained at each propellant storage area. Maintainabili
4、ty and reliability of the TCU is greatly enhanced since the individual cooling systems have been removed in lieu of connections to the existing Facility Chilled Water (FCW) System.While at the launch pad the Space Shuttle Orbital Maneuvering System (OMS) and Reaction Control System (RCS) propellant
5、tanks are filled with hypergolic propellant; Monomethylhydrazine (MMH) and Nitrogen Tetroxide (N2O4). The OMS/RCS is used for altitude and attitude changes required by Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-the Shuttle during orbital flight.
6、 Loading of the tanks takes place about two weeks prior to launch. A temperature requirement is imposed on the propellant for loading to assure proper operation of the Ground Support Equipment (GSE) and to assure proper weight measurement of the loaded propellant. The temperature requirement is met
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