NASA NTRS · 19910036901
Reusable cryogenic foam insulation for advanced aerospace vehicles
Abstract
Future high-speed aircraft and aerospace vehicles using cryogenic propellants will require an advanced reusable insulation system for the propellant tank structure. This cryogenic insulation system must be lightweight, structurally and thermally efficient, and capable of multiple reuse without cracking or degraded performance. This paper presents recent progress in the development of a reusable cryogenic foam insulation system having a maximum service temperature of 400 F. The system consists of preshaped, precut blocks of rigid polymethacrylimide foam insulation, wrapped with a high-temperature Kapton and aluminum foil vapor barrier which is adhesively bonded to the propellant tank wall.
Keep this discovery
Explore connections, maps & timelines
Mcauliffe, Patrick S., Taylor, Allan H., Sparks, Larry L., Dube, William P.. 1991-01-01. Reusable cryogenic foam insulation for advanced aerospace vehicles. https://ntrs.nasa.gov/citations/19910036901
Cite the original work for its findings. Save a collection to share your selection of sources.