Tasks accomplished during the HTTA Program study period included: (1) performance of a literature review to provide system guidelines; (2) development of analytical procedures needed to predict system performance; (3) design and analysis of the HTTA pressurization system considering (a) future utilization of results in the design of a spacecraft maneuvering system propellant package, (b) ease of control and operation, (c) system safety, and (d) hardware cost; and (4) making conclusions and recommendations for systems design
The H2-O2 space shuttle auxiliary power unit (APU) program is a NASA-Lewis effort aimed at hardware ...
This paper studies concepts for the Hydrogen On-Orbit Storage and Supply Experiment (HOSS). HOSS is ...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Technical analyses and computer programs in support of optimization of liquid hydrogen thermal prote...
Vehicle-scale analysis of fluorine-hydrogen main tank injection pressurization syste
Technology for long life, high performing, gaseous hydrogen-gaseous oxygen rocket engines suitable f...
High-energy cryogenic propellant is an essential element in future space exploration programs. There...
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
Results are presented from more than 1500 hours of testing on a liquid hydrogen thermal conditioning...
Data tables for optimal thermal protection of liquid hydrogen storage in nuclear interplanetary spac...
A high pressure thruster effort was conducted with the major objective of demonstrating a duct cooli...
An analytical and experimental effort was completed to evaluate a baffle type thermal conditioner fo...
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
The analysis on the feasibility for using metal hydrides in the thermal protection system of cryogen...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
The H2-O2 space shuttle auxiliary power unit (APU) program is a NASA-Lewis effort aimed at hardware ...
This paper studies concepts for the Hydrogen On-Orbit Storage and Supply Experiment (HOSS). HOSS is ...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Technical analyses and computer programs in support of optimization of liquid hydrogen thermal prote...
Vehicle-scale analysis of fluorine-hydrogen main tank injection pressurization syste
Technology for long life, high performing, gaseous hydrogen-gaseous oxygen rocket engines suitable f...
High-energy cryogenic propellant is an essential element in future space exploration programs. There...
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
Results are presented from more than 1500 hours of testing on a liquid hydrogen thermal conditioning...
Data tables for optimal thermal protection of liquid hydrogen storage in nuclear interplanetary spac...
A high pressure thruster effort was conducted with the major objective of demonstrating a duct cooli...
An analytical and experimental effort was completed to evaluate a baffle type thermal conditioner fo...
The auxiliary power unit (APU) for the space shuttle is required to provide hydraulic and electrical...
The analysis on the feasibility for using metal hydrides in the thermal protection system of cryogen...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
The H2-O2 space shuttle auxiliary power unit (APU) program is a NASA-Lewis effort aimed at hardware ...
This paper studies concepts for the Hydrogen On-Orbit Storage and Supply Experiment (HOSS). HOSS is ...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan