Add to ORKGAnalytical and experimental studies conducted at the NASA Langley Research Center for investigating integrated cryogenic propellant tank systems for a Reusable Launch Vehicle are described. The cryogenic tanks are investigated as an integrated tank system. An integrated tank system includes the tank wall, cryogenic insulation, Thermal Protection System (TPS) attachment sub-structure, and TPS. Analysis codes are used to size the thicknesses of cryogenic insulation and TPS insulation for thermal loads, and to predict tank buckling strengths at various ring frame spacings. The unique test facilities developed for the testing of cryogenic tank components are described. Testing at cryogenic and high-temperatures verifies the integrity of materia...
To test structural components of reusable launch vehicles the DLR-Institute of Structural Mechanics ...
Returning and reusing a launch vehicle stage after it has fulfilled its primary ascent mission signi...
The initial objective was to study the use of superplastically formed corrugated hat section stringe...
Analytical and experimental studies conducted at the NASA Langley Research Center for investigating ...
To advance reusable space transportation vehicles with cryogenic tanks for future space missions, a ...
Reusable launch vehicle stages encounter large heat fluxes during their mission, especially during r...
Future reusable launch and re-entry vehicles are characterised by complex structures undergoing seve...
An important step in developing a cost-effective, reusable, launch vehicle is the development of dur...
An important step in developing a cost-effective, reusable, launch vehicle is the development of dur...
A cryogenic pressure-box test machine has been designed and is being developed to test full-scale re...
An interface design between structure, cryogenic insulation and thermal protection system (TPS) is d...
Reusable launchers experience a large range of thermal extremes, reaching from the cryogenic tempera...
Reusable launch vehicle stages face intense heat fluxes, particularly during reentry. Thermal protec...
This viewgraph presentation provides an overview of thermal-mechanical cyclic tests conducted on a c...
Within FESTIP Structures Technology De-vel-opment work concentrated on cryogenic tank structures as ...
To test structural components of reusable launch vehicles the DLR-Institute of Structural Mechanics ...
Returning and reusing a launch vehicle stage after it has fulfilled its primary ascent mission signi...
The initial objective was to study the use of superplastically formed corrugated hat section stringe...
Analytical and experimental studies conducted at the NASA Langley Research Center for investigating ...
To advance reusable space transportation vehicles with cryogenic tanks for future space missions, a ...
Reusable launch vehicle stages encounter large heat fluxes during their mission, especially during r...
Future reusable launch and re-entry vehicles are characterised by complex structures undergoing seve...
An important step in developing a cost-effective, reusable, launch vehicle is the development of dur...
An important step in developing a cost-effective, reusable, launch vehicle is the development of dur...
A cryogenic pressure-box test machine has been designed and is being developed to test full-scale re...
An interface design between structure, cryogenic insulation and thermal protection system (TPS) is d...
Reusable launchers experience a large range of thermal extremes, reaching from the cryogenic tempera...
Reusable launch vehicle stages face intense heat fluxes, particularly during reentry. Thermal protec...
This viewgraph presentation provides an overview of thermal-mechanical cyclic tests conducted on a c...
Within FESTIP Structures Technology De-vel-opment work concentrated on cryogenic tank structures as ...
To test structural components of reusable launch vehicles the DLR-Institute of Structural Mechanics ...
Returning and reusing a launch vehicle stage after it has fulfilled its primary ascent mission signi...
The initial objective was to study the use of superplastically formed corrugated hat section stringe...