Sunflower turboalternator csu i-3a. 4329-hour-test summary report
Sunflower combined shaft unit Rankine cycle turboalternator
RANKINE CYCLE↗
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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.
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Operation of a haynes alloy no. 25 forced circulation loop to study the effects of hydrogen in a simulated sunflower system
Haynes alloy forced circulation mercury loop for studying hydrogen effects in working fluid of Rankine cycle Sunflower solar power system
SUNFLOWER POWER SYSTEM↗
Experimental investigation of mercury condensing pressure drops
Mercury vapor condensation in Rankine cycle power plant from pressure drops - thermodynamics
POWER PLANT↗
Analysis of low-temperature direct-condensing vapor-chamber fin and conducting fin radiators
Analysis of flat, direct-condensing finned-tube space radiator with vapor chamber, and central fin tube geometries for low temperature Rankine space power electric generating system
RANKINE CYCLE↗
Survey of electric power plants for space applications
Fuel and solar cells, chemical batteries, Rankine and Brayton cycle power plants, thermoelectric generators, and thermionic converters for space power applications
SPACECRAFT POWER SUPPLY↗
Mathematical model with experimental verification for the dynamic behavior of a single-tube condenser
Mathematical model derived from condensation of working fluid in Rankine power cycle to predict behavior of single-tube condenser
CONDENSER↗
Comparison of calculated and measured characteristics of horizontal multitube heat exchanger with steam condensing inside tubes
Comparison of calculated and measured characteristics of horizontal multitube heat exchanger in Rankine cycle turbogenerator studies
TURBOGENERATOR↗
SNAP-8 electrical generating system development program Semiannual progress report, 1 Jul. - 31 Dec. 1965
Turboelectric, nuclear, space power conversion system using mercury Rankine cycle - SNAP 8
RANKINE CYCLE↗
Cavitation damage investigations in mixed-flow liquid metal pumps.
Cavitation damage in high-temperature liquid metal pumps for Rankine cycle space power plants studied in water model
LIQUID METAL↗
Liquid MHD power conversion
Nonrotating Rankine cycle for liquid metal magnetohydrodynamic power conversion
POWER CONVERSION↗
Critique of session on corrosion by boiling alkali metals
Boiling alkali metal corrosion research for Rankine cycle and thermionic power conversion systems
RANKINE CYCLE↗
Lithium-boiling potassium test loop
Initial operations of lithium-boiling potassium Rankine cycle test loop, and operating characteristics
LOOP↗
Effects of liquid and vapor cesium on structural materials
Literature survey on corrosive effects of liquid and vapor cesium on structural materials, and compatibility of cesium as working fluid for Rankine cycle space power plant
POWER PLANT↗
Magnetohydrodynamic power systems.
Liquid-metal and plasma MHD systems for power generation in space environments, noting Rankine and Brayton cycles
SPACE ENVIRONMENT↗
Man-rating of reactor power systems for lunar- base missions.
Integrated thermoelectric SNAP-8 Rankine power system for manned lunar base missions, studying man-system interactions effect on design criteria
SNAP-8↗
Lunar power systems.
Lunar electric power systems transported by Saturn V noting Brayton cycle, Rankine cycle, solar cells and thermoelectric systems
ELECTRIC ENERGY↗
Space Station thermal management system development status and plans
The manned Space Station, as currently designed, contains a baseline thermal management system (TMS) which uses components and subsystems never before employed in manned spacecraft. The basis for the technology used in the TMS design is the result of a long-term TMS Technology Development Plan which was initiated in 1979. Rankin and Marshall (1983) have discussed the history and progress of that plan from its beginnings to early 1983. The present paper is concerned with the status of activities conducted at the NASA Lyndon B. Johnson Space Center (JSC) under this plan since 1983, taking into account also a summary of activities planned for the next several years.
Rankin, J. G.↗
EFFECTS OF EXHAUST NOZZLE RECOMBINATION ON HYPERSONIC RAMJET PERFORMANCE. I - EXPERIMENTAL INVESTIGATION OF RECOMBINATION IN EXHAUST NOZZLES
Temperature measurements in supersonic nozzles for hydrogen-air and methane-air combustion products at stagnation temperatures up to 5400 degrees rankine and pressures up to 4.5 atmospheres
NOZZLE FLOW↗