Efficiency estimates of turbine and compressor components of Brayton rotating unit during hot closed loop operatio
Design and characteristics of radial inflow turbine stage for use as an alternative to stage of Bray...
A system was designed to produce 2-10 kW net continuous electric power for at least 5 years. The tur...
The Brayton rotating unit (BRU), operating on a gas bearing system, has been designed, fabricated, a...
Performance of turbine-compressor-alternator Brayton cycle unit for space electric power generatio
Compressor performance was mapped during the Brayton cycle power system testing. The range of testin...
Electric tests on Brayton rotating unit alternator, voltage regulator, and speed contro
The Brayton rotating unit (BRU), operating on a gas bearing system, has been designed, fabricated, a...
The methods which have been used by the NASA Lewis Research Center for predicting Brayton Cycle comp...
The performance characteristics of the Brayton-rotating-unit's 4.97-inch radial turbine were investi...
This paper provides an analytical evaluation on the operation and performance of a dual Brayton comm...
Brayton cycle compressor research package for testing aerodynamic performance of Brayton cycle compr...
Performance of single stage, axial flow turbine designed for Brayton cycle space power syste
Cold performance characteristics of small radial inflow turbine designed for Brayton cycle power sys...
Design description and performance test results from identical Brayton heat exchange unit
Advanced aerodynamic design and specifications of high efficiency Brayton cycle compressor for monat...
Design and characteristics of radial inflow turbine stage for use as an alternative to stage of Bray...
A system was designed to produce 2-10 kW net continuous electric power for at least 5 years. The tur...
The Brayton rotating unit (BRU), operating on a gas bearing system, has been designed, fabricated, a...
Performance of turbine-compressor-alternator Brayton cycle unit for space electric power generatio
Compressor performance was mapped during the Brayton cycle power system testing. The range of testin...
Electric tests on Brayton rotating unit alternator, voltage regulator, and speed contro
The Brayton rotating unit (BRU), operating on a gas bearing system, has been designed, fabricated, a...
The methods which have been used by the NASA Lewis Research Center for predicting Brayton Cycle comp...
The performance characteristics of the Brayton-rotating-unit's 4.97-inch radial turbine were investi...
This paper provides an analytical evaluation on the operation and performance of a dual Brayton comm...
Brayton cycle compressor research package for testing aerodynamic performance of Brayton cycle compr...
Performance of single stage, axial flow turbine designed for Brayton cycle space power syste
Cold performance characteristics of small radial inflow turbine designed for Brayton cycle power sys...
Design description and performance test results from identical Brayton heat exchange unit
Advanced aerodynamic design and specifications of high efficiency Brayton cycle compressor for monat...
Design and characteristics of radial inflow turbine stage for use as an alternative to stage of Bray...
A system was designed to produce 2-10 kW net continuous electric power for at least 5 years. The tur...
The Brayton rotating unit (BRU), operating on a gas bearing system, has been designed, fabricated, a...