Experimental investigation of reactor-loop transients during startup of a simulated SNAP-8 system
Primary loop transients during startup of Rankine cycle space power system in SNAP 8 simulator
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Primary loop transients during startup of Rankine cycle space power system in SNAP 8 simulator
Analytical method for predicting performance of centrifugal pumps during pressurized startup
Analog computer simulation of single shaft Brayton cycle system dynamics, including startup and shutdown transients
Cold flow startup test on nuclear rocket engine using radial turbopump
Computerized simulation of SNAP-8 to evaluate condensing-pressure control method during system startup
Experimental investigation of reactor loop transients during SNAP 8 power conversion system startup
Startup testing of SNAP 8 power conversion system
Neutron kinetics of fast, hot, critical assembly in startup mode
Optimal startup control of jacketed tubular reactor with first order reversible exothermic reaction, presenting distributed maximum principle for diffusional parameter system
Visual observation of high temperature profiles during startup in lithium heat pipe
Inventory control of mercury condensing pressure during SNAP 8 startup
Deadband condenser inlet pressure control method for SNAP 8 startup
SNAP 8 reactor startup tests using reactor and heat radiator simulators and evaluation of temperature transients
Analysis of nuclear light bulb startup and engine dynamics including transient responses to perturbations at full power operating level
Reassessment of Cotter model startup in Li heat pipe, modifying model by moving sonic point to end of hot zone and including wall friction and condensation
Liquid hydrazine catalytic reactor startup characteristics as function of catalyst adsorbed gas condition and temperature by high speed motion picture observation
Startup testing of SNAP 8 power conversion system coupled with nuclear reactor simulator
Cold performance tests and startup tests were conducted on the Brayton-cycle inverter, motor-driven pump, dc supply, speed control with parasitic load resistor and the Brayton control system. These tests were performed with the components in a vacuum and mounted on coldplates. A temperature range of ?25 to -50 C was used for the tests. No failures occurred, and component performance gave no indication that there would be any problem with the safe operation of the Brayton power generating system.