Solar cell Patent
Development and characteristics of solar cells with phosphors in cover glass to improve response to solar ultraviolet radiation
Streed, E. R.↗
Engineering topics
Streed, E. R.
Publications and source records attributed to Streed, E. R..
A comparison of infrared-emittance measurements and measurement techniques.
IR directional and hemispherical emittance of spacecraft thermal control coatings, comparing values determined by various measurement techniques
Millard, J. P.↗
Passive thermal control by second-surface mirror.
Second surface mirror used as coating for spacecraft thermal control
Streed, E. R.↗
An experimental study of the combined space environmental effects on a zinc-oxide - Potassium-silicate coating.
High energy particle and electromagnetic space radiation effects on thermal control coating, noting spectral absorptance for various conditions
SPACE RADIATION↗
Low solar absorptance surfaces with controlled emittance - A second generation of thermal control coatings.
Low solar absorption surface coatings of aluminum, silver and silica with controlled emittance for spacecraft thermal control
PROTECTIVE COATING↗
A review of the status of spacecraft thermal control materials.
Thermal control materials for spacecraft, considering UV spectral distribution, radiation energy and flux, oxygen bleaching, etc
ENVIRONMENT SIMULATION↗
An experimental study of the combined space environmental effects on a zinc-oxide/ potassium-silicate coating.
High energy particle and electromagnetic space radiation effects on thermal control coating, noting spectral absorptance for various conditions
Streed, E. R.↗
Low solar absorptance surfaces with controlled emittance - A second generation of thermal control coatings.
Low solar absorption surface coatings of aluminum, silver and silica with controlled emittance for spacecraft thermal control
Greenberg, S. A.↗
Performance of multilayer insulation systems for the 300 deg to 800 deg K temperature range.
Multilayer insulation system materials and design data for use on spacecraft in temperature range from 300 to 800 degrees K
SPACECRAFT SHIELDING↗
Performance of multilayer insulation systems for the 300 deg to 800 deg k temperature range.
Multilayer insulation system materials and design data for use on spacecraft in temperature range from 300 to 800 degrees K
THERMAL INSULATION↗
The study of low solar absorptance coatings for a solar probe mission
Low solar radiation absorption coatings for solar probe mission
SOLAR PROBE↗
The influence of temperature on the stability of low solar absorptance and thermal coatings
Temperature effect on stability of low solar absorptance to infrared emittance ratio coatings in space environment
THERMOSTABILITY↗
Methods for experimental determination of the extra-terrestrial solar absorptance of spacecraft materials
Spectral diffuse reflectance and simulated solar absorptance measurements for determination of solar absorptance of spacecraft materials
SOLAR ABSORBER↗
ERRORS ASSOCIATED WITH HOHLRAUM RADIATION CHARACTERISTICS DETERMINATIONS
Errors in radiation measurements with a hohlraum reflectometer and infrared spectraphotometer
INFRARED SPECTRUM↗