Marshall Technical Reports Server

Large-Scale Liquid Hydrogen Testing of Variable Density Multilayer Insulation With a Foam Substrate

NASA/TM-211089, Martin, J.J and Hastings, L., Large-Scale Liquid Hydrogen Testing of Variable Density Multilayer Insulation With a Foam Substrate , George C. Marshall Space Flight Center Marshall Space Flight Center, Alabama 35812, National Aeronautics and Space Administration Washington, DC 20546-0001, Prepared by Vehicle and Systems Development Department,Space Transportation Directorate, June 2001, pp. 88, Format(s): PDF 212079k

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The multipurpose hydrogen test bed (MHTB), with an 18-m3 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 MLI 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 robust, 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/m2. The orbit hold tests resulted in heat leaks of 0.085 and 0.22 W/m2 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
Keywords:orbital cryogenic fluid management, cryogenic storage, cryogenic insulation, multilayer insulation
Subjects:Chemistry and Materials: Composite Materials: Composite Materials
ID Code:567
Deposited On:01 August 2002