Preliminary results from a round-robin study of ultraviolet degradation of spacecraft thermal-control coating
Effect of ultraviolet radiation on spacecraft low solar absorptance white coatings
ULTRAVIOLET RADIATION↗
Engineering topics
Neel, C. B.
Publications and source records attributed to Neel, C. B..
Albedo and earth radiation deduced from emissivity sensors on the first orbiting solar observatory
Albedo and earth radiation data obtained from orbiting solar observatory emissivity sensors
TERRESTRIAL RADIATION↗
Reference black body is compact, convenient to use
To replace the classical hollow sphere, a compact reference black body has been constructed from stacked razor blades. Treated with a deposit of black oxide on the surfaces or notches between the upper edges of the blades, the device is useful over a wide range of incident angles.
Dimeff, J.↗
Experimental development of a technique for the correlation of flight- and ground-based studies of the ultraviolet degradation of polymer films
Ultraviolet degradation of polymer films
ULTRAVIOLET RADIATION↗
Research on the stability of thermal-control coatings for spacecraft.
Flight test of long term stability of temperature control coatings for spacecraft surfaces
PROTECTIVE COATING↗
Preliminary results from a round-robin study of ultraviolet degradation of spacecraft thermal-control coatings
Ultraviolet degradation of spacecraft thermal- control coatings in simulated space environment
ULTRAVIOLET RADIATION↗
Measurement of thermal-radiation character- istics of temperature-control surfaces during flight in space
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Neel, C. B.↗
AN ANALOG STUDY OF THE INFLUENCE OF INTERNAL MODIFICATIONS TO A WING LEADING EDGE ON ITS TRANSIENT TEMPERATURE RISE DURING HIGHSPEED FLIGHT
Aerodynamic heating of sweptback wing leading edge
SWEPTBACK WING↗
A heated-wire liquid-water-content instrument and results of initial flight tests in icing conditions
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Neel, C. B.↗
A Procedure for the Design of Air-Heated Ice-Prevention Systems
A procedure proposed for use in the design of air-heated systems for the continuous prevention of ice formation on airplane components is set forth. Required heat-transfer and air-pressure-loss equations are presented, and methods of selecting appropriate meteorological conditions for flight over specified geographical areas and for the calculation of water-drop-impingement characteristics are suggested. In order to facilitate the design, a simple electrical analogue was devised which solves the complex heat-transfer relationships existing in the thermal-system analysis. The analogue is described and an illustration of its application to design is given.
Neel, C. B.↗