Total Hemispherical Emittance of Polyimide Films for Space Use in the Temperature Range from 173 to 700 K

International Journal of Thermophysics

Volumn 23, Issue 1, 2002, Pages 319-331

  Fukuzawa, K ^a   Ohnishi, A ^b   Nagasaka, Y ^a  

^a KEIO UNIVERSITY   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

Mercury orbiter mission; Optical constants; Polyimide film; Steady state calorimetric method; Thermal control materials; Total hemispherical emittance

Indexed keywords

ALUMINUM; CALORIMETRY; COATING TECHNIQUES; DATA REDUCTION; DEPOSITION; LIGHT EMISSION; MULTILAYERS; PLANETS; POLYIMIDES; SPACECRAFT;

MERCURY ORBITER EMISSIONS; OPTICAL CONSTANTS; POLYIMIDE FILMS; STEADY-STATE CALORIMETRIC METHOD; THERMAL CONTROL MATERIALS; TOTAL HEMISPHERICAL EMITTANCE;

PLASTIC FILMS;

EID: 1942454208     PISSN: 0195928X     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1013933917245     Document Type: Article

References (10)

1. H. Saito, H. Yamakawa, Y. Kobayashi, and T. Mukai, IAF-98-Q.2.04 (1998).
2. R. Grard, G. Scoon, and M. Coradini, ESA J. 18:197 (1994).
3. M. M. Finckenor and D. Dooling, NASA/TP-1999-209263 (1999).
4. A. Ohnishi and R. Sato, Trans. IEE Japan 116-A(2):136 (1996) (in Japanese).
5. H. Inoue, H. Okamoto, and Y. Hiraoka, Int. J. Radiat. Appl. Instrum. Part C 29:283 (1987).
6. H. Yamane, Polyimides: Characterization and Application: Proc. Second Int. Conf. Polyimides (UMI, Ann Arbor, MI, 1989), pp. 86-105.
7. A. Ohnishi, T. Hayashi, and H. Nagano, Proc. 4th Japan Symp. Thermophys. Prop., Vol. 1 (1983) (in Japanese).
8. R. Horikoshi, Y. Nagasaka, and A. Ohnishi, Int. J. Thermophys. 19:547 (1998).
9. R. Siegel and J. R. Howell, Thermal Radiation Heat Transfer, 3rd ed. (Taylor and Francis, Washington, DC, 1992), pp. 11-91.
10. American Institute of Physics Handbook, 3rd ed. (McGraw-Hill, New York, 1972), pp. 6-124.