Thermal conductivity of oriented fibrous carbon insulation from 300 to 1300$sup 0$K in nitrogen and argon at one atmosphere

Journal Article · Mon Apr 01 04:00:00 EDT 1974 · Nucl. Technol., v. 22, no. 1, pp. 94-107

OSTI ID:4329921

Godfrey, T G; McElroy, D L; Ardary, Z L

The thermal conductivity, lambda , of three samples of oriented fibrous carbon insulation of possible interest to fusion reactors was measured from 300 to 1300 deg K in a radial heat-flow apparatus. Samples of 0.18 g/cm/sup 3/ density were prepared by a vacuum filtration process from carbon fibers and powdered phenolic resin and were characterized after carbonization. The lambda of these low-density composites depended on both the heat treatment temperature and the fiber orientation. For samples heat treated at 1575 deg K, the room- temperature lambda perpendicular to the planes of fibers was ~0.5 mW/(cm deg K) and was three times as high in the direction parallel to the planes. At 1000 deg K, the lambda in both directions had doubled, primarily because of the positive d lambda /dT of the amorphous carbon fibers. Material heat treated at 2775 deg K had a significantly higher room-temperature lambda and a negative d lambda /dT, indicating that a slight degree of ordering or graphitization had occurred in the fibers during heat treatment. At high temperatures, the lambda of all three samples increased markedly because of radiative heat transport. (11 figures, 3 tables) (auth)

• Research Organization: Oak Ridge National Lab., TN
• NSA Number: NSA-29-030175
• OSTI ID: 4329921
• Journal Information: Nucl. Technol., v. 22, no. 1, pp. 94-107, Journal Name: Nucl. Technol., v. 22, no. 1, pp. 94-107; ISSN NUTYB
• Country of Publication: Country unknown/Code not available
• Language: English

Related Subjects

*CARBON-- THERMAL CONDUCTIVITY
*COMPOSITE MATERIALS-- THERMAL CONDUCTIVITY
FILAMENTS
HEAT TREATMENTS
HIGH TEMPERATURE
MEDIUM TEMPERATURE
N50330* --Metals
Ceramics
& Other Materials--Plastics & Other Materials--Properties
Structure & Phase Studies
ORIENTATION
TEMPERATURE DEPENDENCE
THERMAL INSULATION
VERY HIGH TEMPERATURE