Data from the first tests of the 2- to 15-kilowatt space power system in a vacuum chamber were compared with predictions of both a pretest analysis and a modified version of that analysis. The pretest analysis predicted test results with differences of no more than 9 percent of the largest measured value for each quantity. The modified analysis correlated measurements. Differences in conversion efficiency and power output were no greater than plus or minus 2.5 percent. This modified analysis was used to project space performance maps for the current test system
Thermal performance analysis of solar Brayton heat receiver in transferring heat to working gas of B...
Performance characteristics of 14.3 kVA modified Lundell alternator for 1200 Hz Brayton cycle space ...
A space-type laminar flow radiator was designed and integrated with a 2- to 15-kilowatt Brayton elec...
Data from the first tests of the 2- to 15-kilowatt space power system in a vacuum chamber were compa...
Component and system performance tests of Brayton cycle power conversion system in 2 to 15 kW sub e ...
The electrical subsystem of the 2- to 15-kW Brayton power conversion system consists of the auxiliar...
Description and performance of electrical subsystem and components for Brayton power syste
Test results of an experimental investigation to measure Brayton engine performance while operating ...
Performance tests on Brayton cycle direct current power supply circuit for automatic contro
Electric tests on Brayton rotating unit alternator, voltage regulator, and speed contro
Performance test of homopolar inductor alternator for Brayton cycle space power syste
Performance of turbine-compressor-alternator Brayton cycle unit for space electric power generatio
Experimental performance of 2-15 kilowatt Brayton power system using mixture of helium and xeno
The methods which have been used by the NASA Lewis Research Center for predicting Brayton Cycle comp...
This paper provides an analytical evaluation on the operation and performance of a dual Brayton comm...
Thermal performance analysis of solar Brayton heat receiver in transferring heat to working gas of B...
Performance characteristics of 14.3 kVA modified Lundell alternator for 1200 Hz Brayton cycle space ...
A space-type laminar flow radiator was designed and integrated with a 2- to 15-kilowatt Brayton elec...
Data from the first tests of the 2- to 15-kilowatt space power system in a vacuum chamber were compa...
Component and system performance tests of Brayton cycle power conversion system in 2 to 15 kW sub e ...
The electrical subsystem of the 2- to 15-kW Brayton power conversion system consists of the auxiliar...
Description and performance of electrical subsystem and components for Brayton power syste
Test results of an experimental investigation to measure Brayton engine performance while operating ...
Performance tests on Brayton cycle direct current power supply circuit for automatic contro
Electric tests on Brayton rotating unit alternator, voltage regulator, and speed contro
Performance test of homopolar inductor alternator for Brayton cycle space power syste
Performance of turbine-compressor-alternator Brayton cycle unit for space electric power generatio
Experimental performance of 2-15 kilowatt Brayton power system using mixture of helium and xeno
The methods which have been used by the NASA Lewis Research Center for predicting Brayton Cycle comp...
This paper provides an analytical evaluation on the operation and performance of a dual Brayton comm...
Thermal performance analysis of solar Brayton heat receiver in transferring heat to working gas of B...
Performance characteristics of 14.3 kVA modified Lundell alternator for 1200 Hz Brayton cycle space ...
A space-type laminar flow radiator was designed and integrated with a 2- to 15-kilowatt Brayton elec...