A study of thread-reinforced polyurethane foam and glass fabric liner, serving as internally bonded insulation for space shuttle LH2 tanks, is reported. Emphasis was placed on an insulation system capable of reentry and multiple reuse in the shuttle environment. The optimized manufacturing parameters associated with each element of the composite are established and the results, showing successful completion of subscale system evaluation tests using the shuttle flight environmental requirements, are given
The Space Shuttle External Tank (ET) contains the liquid H2 fuel and liquid oxygen oxidizer and supp...
The Aerospace industry has a long history of using low density polyurethane and polyurethane-modifie...
Lightweight polyurethane foam assembled in panels is effective spacer material for construction of s...
A study of internal insulation materials and fabrication processes for space shuttle LH2 tanks is re...
The paper presents the project plan to demonstrate, by March 1997, the reusability of an integrated ...
Thermal Protection Systems (TPS) of NASA's Space Shuttle External Tank include polyurethane and poly...
A concept for a fail-safe thermal protection system was developed. From screening tests, approximate...
Four commercially available polyisocyanurate polyurethane spray-foam insulation formulations are use...
The selection and quantification of four foams using a more environmentally friendly HCFC-141b blowi...
Design studies involving weight and cost were carried out for several structural concepts applicable...
Cryogenic propellant tank insulations or liquid oxygen/liquid hydrogen low-thrust 2224N (500 lbf) pr...
Advancements in high temperature materials by NASA have led to the development of polyimide foam sys...
Summary of work accomplished on design of insulation and manufacture of tooling for fabrication and ...
Self evacuating multilayer insulation panel systems for liquid hydrogen space tankag
Three reusable insulation systems concepts were developed for use with cryogenic tanks of earth-base...
The Space Shuttle External Tank (ET) contains the liquid H2 fuel and liquid oxygen oxidizer and supp...
The Aerospace industry has a long history of using low density polyurethane and polyurethane-modifie...
Lightweight polyurethane foam assembled in panels is effective spacer material for construction of s...
A study of internal insulation materials and fabrication processes for space shuttle LH2 tanks is re...
The paper presents the project plan to demonstrate, by March 1997, the reusability of an integrated ...
Thermal Protection Systems (TPS) of NASA's Space Shuttle External Tank include polyurethane and poly...
A concept for a fail-safe thermal protection system was developed. From screening tests, approximate...
Four commercially available polyisocyanurate polyurethane spray-foam insulation formulations are use...
The selection and quantification of four foams using a more environmentally friendly HCFC-141b blowi...
Design studies involving weight and cost were carried out for several structural concepts applicable...
Cryogenic propellant tank insulations or liquid oxygen/liquid hydrogen low-thrust 2224N (500 lbf) pr...
Advancements in high temperature materials by NASA have led to the development of polyimide foam sys...
Summary of work accomplished on design of insulation and manufacture of tooling for fabrication and ...
Self evacuating multilayer insulation panel systems for liquid hydrogen space tankag
Three reusable insulation systems concepts were developed for use with cryogenic tanks of earth-base...
The Space Shuttle External Tank (ET) contains the liquid H2 fuel and liquid oxygen oxidizer and supp...
The Aerospace industry has a long history of using low density polyurethane and polyurethane-modifie...
Lightweight polyurethane foam assembled in panels is effective spacer material for construction of s...