Cryogenic thermal insulation Patent
Development of thermal insulation material for insulating liquid hydrogen tanks in spacecraft
Middleton, R. L.↗
Engineering topics
Publications and source records attributed to Schell, J. T..
Development of thermal insulation material for insulating liquid hydrogen tanks in spacecraft
Dual seal insulation, consisting of an inner layer of sealed-cell Mylar honeycomb core and an outer helium purge channel of fiber glass reinforced phenolic honeycomb core, is used as a thin, lightweight insulation for external surfaces of cryogenic-propellant tanks.
Accelerated compression set properties of elastomeric materials for space vehicle gasket use at high temperatures
Comparative analysis of two commercial instruments used for measuring hardness of elastomers
Lightweight external insulation system for liquid hydrogen stages of Saturn V vehicle