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Supplemental multilayer insulation research facilityThe Supplemental Multilayer Insulation Research Facility (SMIRF) provides a small scale test bed for conducting cryogenic experiments in a vacuum environment. The facility vacuum system is capable of simulating a Space Shuttle launch pressure profile as well as providing a steady space vacuum environment of 1.3 x 10(exp -4) Newton/sq meter (1 x 10(exp -6) torr). Warm side boundary temperatures can be maintained constant between 111 K (200 R) and 361 K (650 R) using a temperature controlled shroud. The shroud can also simulate a typical lunar day-night temperature profile. The test hardware consists of a cryogenic calorimeter supported by the lid of the vacuum chamber. A 0.45 cu meter (120 gallon) vacuum jacketed storage/supply tank is available for conditioning the cryogen prior to use in the calorimeter. The facility was initially designed to evaluate the thermal performance of insulation systems for long-term storage in space. The facility has recently been used to evaluate the performance of various new insulation systems for LH2 and LN2 ground storage dewars.
Document ID
19950024174
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dempsey, P. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Stochl, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1995
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:106991
E-9766
NASA-TM-106991
Report Number: NAS 1.15:106991
Report Number: E-9766
Report Number: NASA-TM-106991
Meeting Information
Meeting: Centennial Conferences
Country: US
Start Date: July 17, 1995
End Date: July 21, 1995
Accession Number
95N30595
Funding Number(s)
PROJECT: RTOP 243-30-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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