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Large-Scale Liquid Hydrogen Testing of Variable Density Multilayer Insulation with a Foam SubstrateThe multipurpose hydrogen test bed (MHTB), with an 18-cu m liquid hydrogen tank, was used to evaluate a combination foam/multilayer combination insulation (MLI) concept. The foam element (Isofoam SS-1171) insulates during ground hold/ascent flight, and allowed a dry nitrogen purge as opposed to the more complex/heavy helium purge subsystem normally required. The 45-layer MLI was designed for an on-orbit storage period of 45 days. Unique WI features include a variable layer density, larger but fewer double-aluminized Mylar perforations for ascent to orbit venting, and a commercially established roll-wrap installation process that reduced assembly man-hours and resulted in a roust, virtually seamless MLI. Insulation performance was measured during three test series. The spray-on foam insulation (SOFI) successfully prevented purge gas liquefaction within the MLI and resulted in the expected ground hold heat leak of 63 W/sq m. The orbit hold tests resulted in heat leaks of 0.085 and 0.22 W/sq m with warm boundary temperatures of 164 and 305 K, respectively. Compared to the best previously measured performance with a traditional MLI system, a 41-percent heat leak reduction with 25 fewer MLI layers was achieved. The MHTB MLI heat leak is half that calculated for a constant layer density MLI.
Document ID
20010063699
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Martin, J. J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Hastings, L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2001
Subject Category
Composite Materials
Report/Patent Number
M-1020
NASA/TM-2001-211089
NAS 1.15:211089
Report Number: M-1020
Report Number: NASA/TM-2001-211089
Report Number: NAS 1.15:211089
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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