High temperature refractory member with radiation emissive overc

Electrical generator or motor structure – Dynamoelectric – Conducting fluid

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H02K 4410

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active

049280279

ABSTRACT:
A radiation type heat dissipator for use in a plasma engine is formed of a refractory metal layer upon which there is deposited a radiation emissive coating made of a high emissivity material such as zirconium diboride. The radiation emissive coating has a surface emissivity coefficient substantially greater than the emissivility coefficient of the refractory metal and thereby enhances the optical radiating efficiency of the heat dissipator.

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W. Deininger et al.; AIAA-86-1510; Development of an Arcjet Nuclear Electric Propulsion System for a 1993 Flight Demonstration (p. 5); Jun. 1986, AIAA/ASME/SAE/ASEE 22nd Joint Propulsion Conference.
D. Q. King et al.; AIAA-87-1020; Design and Operation of a 100 KW Subscale MPD Engine (p. 2); May 1987; AIAA/DGLR/JSASS International Electric Propulsion Conference.

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