Engineering study to determine feasible methods of simulating planetary albedo and radiation effects upon the thermal balance of spacecraft Final report

Environmental simulation from 0.01 to 100 solar constants

Spisz, E. W.
Jack, J. R.

January 1972

The design and development of two solar radiation simulators with an intensity variation ranging fro...

Improvements of a Thermal Method for the Determination of Solar Absorptance and Thermal Emittance of Spacecraft Coatings

B. Biering
D. Hagelschuer

January 2015

For the determination of the solar absorptance αs and ε the thermal emittance optical methods are pr...

Empirical determination of radiation interchange factors Final report

Bobco, R. P.
Rogers, J. E.

December 1968

Techniques for measuring radiant interchange factors relative to spacecraft thermal desig

Computer program determines thermal environment and temperature history of lunar orbiting space vehicles

Mitchell, K. L.
Head, D. E.

August 1967

Program computes the thermal environment of a spacecraft in a lunar orbit. The quantities determined...

The thermal environment of the terrestrial planets, supplement 5

Schocken, K.

April 1965

Thermal environment of terrestrial planets - Venus, Earth, Moon, Mars, and interplanetary spac

Study of environmental effects upon particulate radiation induced absorption bands in spacecraft thermal control coating pigments Final report, 22 May 1967 - 27 Jan. 1969

January 1969

Environmental effects of charged particle and simulated solar electromagnetic radiation on optical p...

Radiant heating simulation First phase report, 23 Sep. - 10 Nov. 1964

Pugmire, T. K.

November 1964

Spectral radiance measurement of oxygen, nitrogen, xenon, and argon for simulation of radiant heatin...

Planetary entry experiments

Craig, Roger A.

July 1994

The final report summarizes the results from three research areas: (1) window design for the radiome...

Development of thermal-vacuum testing techniques for spacecraft at high solar intensities Interim technical summary report

December 1966

Test procedure development for high-intensity thermal testing of solar probe spacecraf

A computer program for calculating external thermal-radiation heat loads and temperatures of spacecraft orbiting the planets or the moon

Finch, H. L.
Sommerville, D.
Vogt, R.
Bland, D.

December 1968

Computer program for computation of thermal radiation heat loads and temperatures of spacecraft orbi...

Systems design study of the Pioneer Venus spacecraft. Appendices to volume 1, section 7 (part 2 of 3)

July 1973

The procedures for predicting the aeroheating environment of Venus entry probes are outlined. After ...

Ground Plane and Near-Surface Thermal Analysis for NASA's Constellation Program

Amundsen, Ruth M.
Leahy, Frank F.
Gasbarre, Joseph F.
Scola, Salvatore
Sharp, John R.

August 2008

Most spacecraft thermal analysis tools assume that the spacecraft is in orbit around a planet and ar...

An introduction to spacecraft thermal control

Hirasawa, P. S.
Schultz, H. D.
Shuldiner, I.
Nevelli, B. A.
Wellman, H. B.
Guard, F. L.

August 1965

External and internal passive and active methods for spacecraft thermal control - material insulatio...

Development of space-stable thermal-control coatings Triannual report, 1 Jan. - 30 Apr. 1970

Zerlaut, G. A.
Gilligan, J. E.

July 1970

Development and performance of solar wind simulation facility for studying thermal-control coating

Development of thermal radiative surface coatings for nasa-lewis space simulation chamber final report, 29 jun. - 30 may 1965

Baldrige, J. H.

January 1965

Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...

Environmental simulation from 0.01 to 100 solar constants

Spisz, E. W.
Jack, J. R.

January 1972

The design and development of two solar radiation simulators with an intensity variation ranging fro...

Improvements of a Thermal Method for the Determination of Solar Absorptance and Thermal Emittance of Spacecraft Coatings

B. Biering
D. Hagelschuer

January 2015

For the determination of the solar absorptance αs and ε the thermal emittance optical methods are pr...

Empirical determination of radiation interchange factors Final report

Bobco, R. P.
Rogers, J. E.

December 1968

Techniques for measuring radiant interchange factors relative to spacecraft thermal desig

Computer program determines thermal environment and temperature history of lunar orbiting space vehicles

Mitchell, K. L.
Head, D. E.

August 1967

Program computes the thermal environment of a spacecraft in a lunar orbit. The quantities determined...

The thermal environment of the terrestrial planets, supplement 5

Schocken, K.

April 1965

Thermal environment of terrestrial planets - Venus, Earth, Moon, Mars, and interplanetary spac

Study of environmental effects upon particulate radiation induced absorption bands in spacecraft thermal control coating pigments Final report, 22 May 1967 - 27 Jan. 1969

January 1969

Environmental effects of charged particle and simulated solar electromagnetic radiation on optical p...

Radiant heating simulation First phase report, 23 Sep. - 10 Nov. 1964

Pugmire, T. K.

November 1964

Spectral radiance measurement of oxygen, nitrogen, xenon, and argon for simulation of radiant heatin...

Planetary entry experiments

Craig, Roger A.

July 1994

The final report summarizes the results from three research areas: (1) window design for the radiome...

Development of thermal-vacuum testing techniques for spacecraft at high solar intensities Interim technical summary report

December 1966

Test procedure development for high-intensity thermal testing of solar probe spacecraf

A computer program for calculating external thermal-radiation heat loads and temperatures of spacecraft orbiting the planets or the moon

Finch, H. L.
Sommerville, D.
Vogt, R.
Bland, D.

December 1968

Computer program for computation of thermal radiation heat loads and temperatures of spacecraft orbi...

Systems design study of the Pioneer Venus spacecraft. Appendices to volume 1, section 7 (part 2 of 3)

July 1973

The procedures for predicting the aeroheating environment of Venus entry probes are outlined. After ...

Ground Plane and Near-Surface Thermal Analysis for NASA's Constellation Program

Amundsen, Ruth M.
Leahy, Frank F.
Gasbarre, Joseph F.
Scola, Salvatore
Sharp, John R.

August 2008

Most spacecraft thermal analysis tools assume that the spacecraft is in orbit around a planet and ar...

An introduction to spacecraft thermal control

Hirasawa, P. S.
Schultz, H. D.
Shuldiner, I.
Nevelli, B. A.
Wellman, H. B.
Guard, F. L.

August 1965

External and internal passive and active methods for spacecraft thermal control - material insulatio...

Development of space-stable thermal-control coatings Triannual report, 1 Jan. - 30 Apr. 1970

Zerlaut, G. A.
Gilligan, J. E.

July 1970

Development and performance of solar wind simulation facility for studying thermal-control coating

Development of thermal radiative surface coatings for nasa-lewis space simulation chamber final report, 29 jun. - 30 may 1965

Baldrige, J. H.

January 1965

Testing polymeric coatings for use in space simulation chamber - resistance to abrasion, acids, ther...

Environmental simulation from 0.01 to 100 solar constants

Spisz, E. W.
Jack, J. R.

January 1972

The design and development of two solar radiation simulators with an intensity variation ranging fro...

Improvements of a Thermal Method for the Determination of Solar Absorptance and Thermal Emittance of Spacecraft Coatings

B. Biering
D. Hagelschuer

January 2015

For the determination of the solar absorptance αs and ε the thermal emittance optical methods are pr...

Empirical determination of radiation interchange factors Final report

Bobco, R. P.
Rogers, J. E.

December 1968

Techniques for measuring radiant interchange factors relative to spacecraft thermal desig

Engineering study to determine feasible methods of simulating planetary albedo and radiation effects upon the thermal balance of spacecraft Final report

Abstract

Extracted data

Engineering study to determine feasible methods of simulating planetary albedo and radiation effects upon the thermal balance of spacecraft Final report

Abstract

Extracted data

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