Laboratory and flight test program to evaluate the space stability of highly specular reflective surfaces.

Author:

MARSHALL K. N.1,DOUGLAS N. J.1,POLLARD H. E.1,ROLLING R. E.1

Affiliation:

1. Lockheed Palo Alto Research Laboratory, Palo Alto, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Effects of Combined Electron-Ultraviolet Irradiation on on Thermal Control Coatings in Vacuo at 77°K;Thermal Design Principles of Spacecraft and Entry Bodies;1969-01-01

2. ROLE OF FLIGHT EXPERIMENTS IN THE STUDY OF THERMAL-CONTROL COATINGS FOR SPACECRAFT;Thermophysics of Spacecraft and Planetary Bodies;1967

3. Role of Flight Experiments in the Study of Thermal-Control Coatings for Spacecraft;Thermophysics of Spacecraft and Planetary Bodies: Radiation Properties of Solids and the Electromagnetic Radiation Environment in Space;1967-01-01

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