Flexible, Lightweight Vacuum Shell for Load-Responsive Multilayer Insulation for High Thermal Performance

TBMG-20696

10/01/2014

Abstract
Content

Better thermal insulation is needed to insulate cryogenic propellants used by NASA for launch vehicles, spacecraft, and orbiting fuel depots. In particular, cryotank insulation during in-air pre-launch and launch ascent stages currently uses spray-on foam insulation (SOFI), which is extremely problematic.

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Citation
"Flexible, Lightweight Vacuum Shell for Load-Responsive Multilayer Insulation for High Thermal Performance," Mobility Engineering, October 1, 2014.
Additional Details
Publisher
Published
Oct 1, 2014
Product Code
TBMG-20696
Content Type
Magazine Article
Language
English