Performance of N/p silicon and cadmium sulfide solar cells as affected by hypervelocity particle impact
Simulated micrometeoroid impact effect on silicon and cadmium sulfide solar cell performances
Engineering topics
Publications and source records attributed to Jack, J. R..
Simulated micrometeoroid impact effect on silicon and cadmium sulfide solar cell performances
Solar absorptance and hemispherical emmitance of metals at space conditions determined with cyclic incident radiation technique
Solar absorptance, total hemispherical emittance and absorptance/emittance ratio for metals at cryogenic temperatures measured simultaneously with sinusoidally perturbed incident radiation
Thermal radiative and electrical properties of cadmium sulfide solar cell at low simulated solar intensities and temperatures
Cyclic incident radiation method for measuring thermal emittance and absorption properties of metals at cryogenic temperatures
Solar absorptance, emittance, and other properties of cadmium sulfide solar cell and five metals for use on spacecraft
Thermal radiation properties of various spacecraft metals and CdS solar cell over temperature range from simulated space environmental tests
Absorptance and emittance of metal surfaces determined via cyclic incident radiation, noting error computation and method accuracy parameters
Cyclic radiation technique has been developed for determining absorptance and emittance of metal surfaces. Using this technique both absorptance and emittance can be determined from one set of data, and variable and controlled temperature levels are possible.
Absorptance and emittance of metal surfaces determined via cyclic incident radiation, noting error computation and method accuracy parameters
High resistance cross flow heat exchangers for electrothermal rocket engines
Thrust coefficients of supersonic nozzles operating at low propellant flow rates
Performance of two types of resistance-heated hydrogen thrustors - tubular and wire-coil heat exchangers
Effects of regenerative and radiation cooling on thrustor performance for frozen flow
Feasibility of optimizing nozzle performance for orbital-launch nuclear rockets
Experimental results concerning the design of resistance-heated hydrogen thrustors, including performance considerations
Nasa program for electric propulsion - resistance- heated hydrogen thrustor
Performance of an electric propulsion system, using resistance heated hydrogen jets, varying heat exchanger temperature, propellant flow rate and input power