Failure analysis was conducted on a heat pipe from a Stirling Engine test rig which was designed to operate at 1073 K. Premature failure had occurred due to localized overheating at the leading edge of the evaporator fin. It was found that a crack had allowed air to enter the fin and react with the sodium coolant. The origin of the crack was found to be located at the inner surface of the Inconel 600 fin where severe intergranular corrosion had taken place
In a Stirling Radioisotope Power System (RPS), heat must be continuously removed from the General Pu...
In support of the U.S. Department of Energy's Stirling Engine Highway Vehicle Systems program, the N...
The heater head tubes of current prototype automotive Stirling engines are fabricated from alloy N-1...
NASA Lewis Research Center has been managing Stirling engine development programs for over a decade....
The Heat Pipe Stirling Engine (HP-1000), a free-piston Stirling engine incorporating three heat exch...
Life issues relating to a sodium heat pipe heat transport system are described. The heat pipe system...
Experiments on Stirling engines of the 50 KW class were conducted to clarify the characteristics of ...
This final report presents the conceptual design of a liquid fueled external heating system (EHS) an...
Failure of Stirling Space Power Demonstrator Engine (SPDE) regenerator screens was investigated. Aft...
The work done by Thermacore, Inc., Lancaster, Pennsylvania, for the Phase 1, 1992 SBIR National Aero...
High-temperature heat pipes are being evaluated for use in energy conversion applications such as fu...
Seven commercial alloys were evaluated in Stirling simulator materials rigs. Five iron base alloys (...
NASA has identified the Stirling power converter as a prime candidate for the next generation power ...
The conceptual design of a free-piston Stirling Space Engine (SSE) intended for space power applicat...
The principal objective of this Phase 2 SBIR program was to develop and demonstrate a practically in...
In a Stirling Radioisotope Power System (RPS), heat must be continuously removed from the General Pu...
In support of the U.S. Department of Energy's Stirling Engine Highway Vehicle Systems program, the N...
The heater head tubes of current prototype automotive Stirling engines are fabricated from alloy N-1...
NASA Lewis Research Center has been managing Stirling engine development programs for over a decade....
The Heat Pipe Stirling Engine (HP-1000), a free-piston Stirling engine incorporating three heat exch...
Life issues relating to a sodium heat pipe heat transport system are described. The heat pipe system...
Experiments on Stirling engines of the 50 KW class were conducted to clarify the characteristics of ...
This final report presents the conceptual design of a liquid fueled external heating system (EHS) an...
Failure of Stirling Space Power Demonstrator Engine (SPDE) regenerator screens was investigated. Aft...
The work done by Thermacore, Inc., Lancaster, Pennsylvania, for the Phase 1, 1992 SBIR National Aero...
High-temperature heat pipes are being evaluated for use in energy conversion applications such as fu...
Seven commercial alloys were evaluated in Stirling simulator materials rigs. Five iron base alloys (...
NASA has identified the Stirling power converter as a prime candidate for the next generation power ...
The conceptual design of a free-piston Stirling Space Engine (SSE) intended for space power applicat...
The principal objective of this Phase 2 SBIR program was to develop and demonstrate a practically in...
In a Stirling Radioisotope Power System (RPS), heat must be continuously removed from the General Pu...
In support of the U.S. Department of Energy's Stirling Engine Highway Vehicle Systems program, the N...
The heater head tubes of current prototype automotive Stirling engines are fabricated from alloy N-1...