Design and vehicle integration of a Pu-238 Brayton power system for MORL.
Plutonium 238 radioisotope Brayton cycle power system design and vehicle integration
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Plutonium 238 radioisotope Brayton cycle power system design and vehicle integration
Heat rejection radiator mass influence on space nuclear power system, discussing Brayton cycle, thermoelectric and Rankine cycle systems
Brayton cycle space powerplant vapor chamber and conduction fin radiators compared for size and weight, noting working fluids
Alternator and voltage and frequency controls for space Brayton cycle energy conversion system designed for and tested at 1200 Hz
Design details and static test data on gas bearing simulator for Brayton cycle radial flow turbocompressor
Performance of gas bearing Brayton cycle turboalternator
Performance of turbine-compressor-alternator Brayton cycle unit for space electric power generation
Operational test and evaluation of Brayton cycle electric generator
Nuclear Brayton cycle heat exchanger and duct assembly
Motor-starting characteristics of modified Lundell alternator for single shaft, Brayton cycle, space power system
Performance of axial flow compressor for Brayton cycle electrical power generating system with argon
Analog computer simulation of design parameter effects on stability of direct acting gas pressure regulator based on Brayton cycle space power generator
Component and system performance tests of Brayton cycle power conversion system in 2 to 15 kW sub e range
Post test analysis of closed Brayton cycle space electric power conversion system for space
Preliminary test results of heat transfer/thermal storage tube design for solar Brayton cycle power system under simulated orbital conditions
Design and characteristics of radial inflow turbine stage for use as an alternative to stage of Brayton cycle turbo-alternator compressor unit
Performance tests of two identical Brayton cycle heat exchanger units consisting of recuperator, heat sink exchanger and ducting in combination with turbine
Brayton cycle 2-15 kW power system for space application and potential gains from component improvements, discussing current status