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.Prepared at Lewis Research Center.Cover title.Bibliography: p. 21-22.Data from the first tests of the 2- to 15-kilowatt space power system in a vacuum chamber were compared with pred...
Performance characteristics of 14.3 kVA modified Lundell alternator for 1200 Hz Brayton cycle space ...
An analysis was conducted to determine the best nuclear-turboelectric space powerplant to meet the r...
The design theory and performance of a breadboard of the proposed Mini-Brayton electrical control sy...
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 ...
This paper presents experimental test results from operation of a 2 kWe Brayton power conversion uni...
Description and performance of electrical subsystem and components for Brayton power syste
The electrical subsystem of the 2- to 15-kW Brayton power conversion system consists of the auxiliar...
The first U.S. power module on International Space Station (ISS) was activated in December 2000. Com...
Performance tests on Brayton cycle direct current power supply circuit for automatic contro
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ac...
Performance test of homopolar inductor alternator for Brayton cycle space power syste
Electric tests on Brayton rotating unit alternator, voltage regulator, and speed contro
Test results of an experimental investigation to measure Brayton engine performance while operating ...
Single shaft turbine compressor-alternator test for performance of voltage regulator and electronic ...
Performance characteristics of 14.3 kVA modified Lundell alternator for 1200 Hz Brayton cycle space ...
An analysis was conducted to determine the best nuclear-turboelectric space powerplant to meet the r...
The design theory and performance of a breadboard of the proposed Mini-Brayton electrical control sy...
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 ...
This paper presents experimental test results from operation of a 2 kWe Brayton power conversion uni...
Description and performance of electrical subsystem and components for Brayton power syste
The electrical subsystem of the 2- to 15-kW Brayton power conversion system consists of the auxiliar...
The first U.S. power module on International Space Station (ISS) was activated in December 2000. Com...
Performance tests on Brayton cycle direct current power supply circuit for automatic contro
Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14).Mode of ac...
Performance test of homopolar inductor alternator for Brayton cycle space power syste
Electric tests on Brayton rotating unit alternator, voltage regulator, and speed contro
Test results of an experimental investigation to measure Brayton engine performance while operating ...
Single shaft turbine compressor-alternator test for performance of voltage regulator and electronic ...
Performance characteristics of 14.3 kVA modified Lundell alternator for 1200 Hz Brayton cycle space ...
An analysis was conducted to determine the best nuclear-turboelectric space powerplant to meet the r...
The design theory and performance of a breadboard of the proposed Mini-Brayton electrical control sy...