Cryogenic Flow Testing
Two-Phase Flowmeter Development
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The Cryogenics Test Lab is used to develop new cryogenic technologies and test cryogenic equipment for use in propellant loading systems. Recent activities include two-phase flowmeter development, superinsulation testing, and cryogenic valve qualification. The lab is located at the NASA Development Testing Laboratory (M7-581).
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Two-Phase Flowmeter Development |
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CRYOGENIC TRANSFER SYSTEM MECHANICAL DESIGN HANDBOOK
by Frank S. Howard, NASA Kennedy Space Center
The purpose of this handbook is to provide a source of information on mechanical engineering experience gained from the design, installation, and operation of Kennedy Space Center cryogenic transfer systems from site activation for launch of the Saturn IB to the activation of Space Shuttle.
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Disclaimer of Endorsement: Reference herein to any specific commercial products, process, or service by trade name, trademark, manufacturer, or otherwise, does not constitute or imply its endorsement, recommendation, or favoring by the United States Government. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government, and shall not be used for advertising or product endorsement purposes.
Disclaimer of Liability: With respect to this multimedia document, neither the United States Government nor any of their employees, makes any warranty, express or implied, including the warranties of merchantability and fitness for a particular purpose, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights.
Last Revised: May 1, 1997
A service of NASA / Kennedy Space Center Engineering Development Directorate, Mechanical GSE Division, Roger Hall, Chief (roger.hall-1@ksc.nasa.gov)