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Title: DETERMINATION OF THE EMISSIVITY OF MATERIALS. Quarterly Progress Report, July 1-September 30, 1962

Technical Report ·
OSTI ID:4750306

Work was continued in support of NASA space power systems. An aluminum phosphate-bonded mixture of nickel-chrome spinel and silicon dioxide completed 8650 hr of endurance testing on a SNAP-8 fimed-tube radiator segment. Flame- sprayed coatings of titania on SNAP-8 and Sunflower I sections completed 7810 hr and 7760 hr, respectively. A fourth rig containing a SNAP-8 section with an aluminum phosphate-bonded mixture of silicon carbide and silicon dioxide completed 6530 hr of testing. Emittance measurements were made on ten materials and on the substrate material, niobium-1% zirconium alloy. The ten materials tested included zirconium silicate, magnesium aluminate, chromic oxide, ceric oxide, titania, barium titanate, calcium titanate, strontium titanate, irontitanum-aluminum oxide, and iron-titanium oxide. Measurement of both total hemispherical and spectral normal emittances were made for all materials except ceric oxide and iron titanium oxide. Two different bonding methods were used for chromic oxide and calcium titanate and three different methods were used for zirconium silicate. One zirconium silicate coating was bonded to type 310 stainless steel rather than niobium-1% zirconium to determine the influence on coating emittance of the type substrate used. Specimens of zirconium silicate and irontitanium oxide were endurance tested. (auth)

Research Organization:
Pratt and Whitney Aircraft Div., United Aircraft Corp., Hartford, Conn.
DOE Contract Number:
NASW-104
NSA Number:
NSA-17-006675
OSTI ID:
4750306
Report Number(s):
PWA-2128
Resource Relation:
Other Information: Orig. Receipt Date: 31-DEC-63
Country of Publication:
United States
Language:
English