Add to ORKGWall temperatures and heat transfer coefficients for solid-vapor mixtures of para hydrogen and nitro...
Optimized pressurization system for Apollo-type service module using cryogenic propellant
Low temperature elongation of polymide films for nonmetallic-tank liners for liquid hydroge
Composite multilayer insulation system of double goldized, Nylar radiation shield
Self evacuating multilayer insulation panel systems for liquid hydrogen space tankag
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Fabrication and demonstration of high performance multilayer cryogenic insulation applied to Torus t...
Thermal performance of self evacuated multilayer radiation shield insulation of lightweight prefabri...
External and internal passive and active methods for spacecraft thermal control - material insulatio...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
The currently stated exploration plan for NASA includes the possibilities ranging from short (severa...
Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...
Thermal insulation materials and techniques for high temperature and cryogenic environments - techno...
Heat transfer, altitude performance, and combustion efficiency evaluated in study of space storable ...
Design and fabrication of shadow shield system for thermal protection of liquid hydrogen propellant ...
Wall temperatures and heat transfer coefficients for solid-vapor mixtures of para hydrogen and nitro...
Optimized pressurization system for Apollo-type service module using cryogenic propellant
Low temperature elongation of polymide films for nonmetallic-tank liners for liquid hydroge
Composite multilayer insulation system of double goldized, Nylar radiation shield
Self evacuating multilayer insulation panel systems for liquid hydrogen space tankag
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Fabrication and demonstration of high performance multilayer cryogenic insulation applied to Torus t...
Thermal performance of self evacuated multilayer radiation shield insulation of lightweight prefabri...
External and internal passive and active methods for spacecraft thermal control - material insulatio...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
The currently stated exploration plan for NASA includes the possibilities ranging from short (severa...
Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...
Thermal insulation materials and techniques for high temperature and cryogenic environments - techno...
Heat transfer, altitude performance, and combustion efficiency evaluated in study of space storable ...
Design and fabrication of shadow shield system for thermal protection of liquid hydrogen propellant ...
Wall temperatures and heat transfer coefficients for solid-vapor mixtures of para hydrogen and nitro...
Optimized pressurization system for Apollo-type service module using cryogenic propellant
Low temperature elongation of polymide films for nonmetallic-tank liners for liquid hydroge