This paper describes potential heat rejection design concepts for Brayton power conversion systems. Brayton conversion systems are currently under study by NASA for Nuclear Electric Propulsion (NEP) and surface power applications. The Brayton Heat Rejection Subsystem (HRS) must dissipate waste heat generated by the power conversion system due to inefficiencies in the thermal-to-electric conversion process. Sodium potassium (NaK) and H2O are two coolant working fluids that have been investigated in the design of a pumped loop and heat pipe space HRS. In general NaK systems are high temperature (300 to 1000 K) low pressure systems, and H2O systems are low temperature (300 to 600 K) high pressure systems. NaK is an alkali metal with health and...
The purpose of this research was to model and analyze a nuclear heated multi-turbine power conversio...
The purpose of this research was to model and analyze a nuclear heated multi-turbine power conversio...
The major power conversion concepts considered for the Megawatt Class Nuclear Space Power System (MC...
This paper describes potential heat rejection design concepts for Brayton power conversion systems. ...
Preliminary design for vapor and conduction fin radiators for Brayton cycle space powerplan
A low-temperature radiator has been designed to reject 17.62 kW of thermal power from an isotope Bra...
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
A preliminary design of the heat exchanger and duct assembly (HXDA) for a 60 kwe, closed loop, Brayt...
Thermal performance analysis of solar Brayton heat receiver in transferring heat to working gas of B...
Titanium-water heat pipes are being evaluated for use in the heat rejection system for space fission...
The feasibility of using Brayton power systems for nuclear electric spacecraft was investigated. The...
Comparison of Brayton and Rankine cycle magnetogasdynamic space power generation systems for use wit...
Design description and performance test results from identical Brayton heat exchange unit
Gas-to-liquid heat exchangers, for liquid cooled Brayton cycle space power plant, with finned tubin
NASA has been supporting design studies and technology development that could provide power to an ou...
The purpose of this research was to model and analyze a nuclear heated multi-turbine power conversio...
The purpose of this research was to model and analyze a nuclear heated multi-turbine power conversio...
The major power conversion concepts considered for the Megawatt Class Nuclear Space Power System (MC...
This paper describes potential heat rejection design concepts for Brayton power conversion systems. ...
Preliminary design for vapor and conduction fin radiators for Brayton cycle space powerplan
A low-temperature radiator has been designed to reject 17.62 kW of thermal power from an isotope Bra...
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
A preliminary design of the heat exchanger and duct assembly (HXDA) for a 60 kwe, closed loop, Brayt...
Thermal performance analysis of solar Brayton heat receiver in transferring heat to working gas of B...
Titanium-water heat pipes are being evaluated for use in the heat rejection system for space fission...
The feasibility of using Brayton power systems for nuclear electric spacecraft was investigated. The...
Comparison of Brayton and Rankine cycle magnetogasdynamic space power generation systems for use wit...
Design description and performance test results from identical Brayton heat exchange unit
Gas-to-liquid heat exchangers, for liquid cooled Brayton cycle space power plant, with finned tubin
NASA has been supporting design studies and technology development that could provide power to an ou...
The purpose of this research was to model and analyze a nuclear heated multi-turbine power conversio...
The purpose of this research was to model and analyze a nuclear heated multi-turbine power conversio...
The major power conversion concepts considered for the Megawatt Class Nuclear Space Power System (MC...