When the technology associated with zero loss storage and transfer is implemented, NASA can reduce the LH2 losses and procurement costs by up to 30 compared to historical Shuttle numbers. This return on investment is based on the mission manifest and commodity use. LH2 densification can provide improved launch vehicle ascent performance by minimizing the size of the LH2 tanks or storing more mass of propellant in the given tank volume
A concept for improving the performance of propulsion systems in expendable and single-stage-to-orbi...
Using densified liquid hydrogen as a cryogenic propellant for launch vehicle applications can reduce...
Cryogenic propellants such as liquid hydrogen (LH2) and liquid oxygen (LO2) are a part of NASA's fut...
NASA has used liquefied hydrogen (LH2) on a large scale since the beginning of the space program as ...
AbstractNASA operations for handling cryogens in ground support equipment have not changed substanti...
AbstractNASA operations for handling cryogens in ground support equipment have not changed substanti...
GODU-LH2 system has successfully met all test objectives at the 33%, 67%, and 100% tank fill level. ...
The Ground Operations Demonstration Unit for Liquid Hydrogen (GODU-LH2) has been developed at NASA K...
Recent demonstration of advanced liquid hydrogen storage techniques using Integrated Refrigeration a...
Described herein is a comprehensive projecta large-scale test of an integrated refrigeration and sto...
NASA has completed a series of tests at the Kennedy Space Center to demonstrate the capability of us...
Integrated Ground Operations Demonstration Units (IGODU) project developed to mature, integrate and ...
Recent demonstration of advanced liquid hydrogen storage techniques using Integrated Refrigeration a...
NASA Kennedy Space Center (KSC) researchers have been working on enhanced and modernized cryogenic l...
Propellant densification is cooling the propellant below the normal boiling point; Densified propell...
A concept for improving the performance of propulsion systems in expendable and single-stage-to-orbi...
Using densified liquid hydrogen as a cryogenic propellant for launch vehicle applications can reduce...
Cryogenic propellants such as liquid hydrogen (LH2) and liquid oxygen (LO2) are a part of NASA's fut...
NASA has used liquefied hydrogen (LH2) on a large scale since the beginning of the space program as ...
AbstractNASA operations for handling cryogens in ground support equipment have not changed substanti...
AbstractNASA operations for handling cryogens in ground support equipment have not changed substanti...
GODU-LH2 system has successfully met all test objectives at the 33%, 67%, and 100% tank fill level. ...
The Ground Operations Demonstration Unit for Liquid Hydrogen (GODU-LH2) has been developed at NASA K...
Recent demonstration of advanced liquid hydrogen storage techniques using Integrated Refrigeration a...
Described herein is a comprehensive projecta large-scale test of an integrated refrigeration and sto...
NASA has completed a series of tests at the Kennedy Space Center to demonstrate the capability of us...
Integrated Ground Operations Demonstration Units (IGODU) project developed to mature, integrate and ...
Recent demonstration of advanced liquid hydrogen storage techniques using Integrated Refrigeration a...
NASA Kennedy Space Center (KSC) researchers have been working on enhanced and modernized cryogenic l...
Propellant densification is cooling the propellant below the normal boiling point; Densified propell...
A concept for improving the performance of propulsion systems in expendable and single-stage-to-orbi...
Using densified liquid hydrogen as a cryogenic propellant for launch vehicle applications can reduce...
Cryogenic propellants such as liquid hydrogen (LH2) and liquid oxygen (LO2) are a part of NASA's fut...