1 |
Harvard Thermal, 1999, TAS User's Manual, ver.4.0
|
2 |
Hottel, H. C. and Sarofim, A. F., 1967, Radiative Transfer, McGraw-Hill
|
3 |
Gilmore, D. G., 1994, Satellite Thermal Control Handbook, The Aerospace Corporation Press.El Segundo, California
|
4 |
Han, C. Y., Kim, J. S., and Rhee, S. W., 2003, 'Thermal Design for Satellite Propulsion System by Thermal Analysis,' Transaction of the KSME(B), Vol. 27, No. 1, pp. 117-124
과학기술학회마을
DOI
|
5 |
Kim, J. S., Han, C. Y., You, J. H., Choi, Y. J. , Sohn, T. J., and Choi, J. C., 11. 11. 2000, 'Preliminary Design of KOMPSAT-2 Propulsion Subsystem,' Proceedings of the KSAS Fall Annual Meeting 2000, pp. 630-633
|
6 |
KARI, Sep. 12, 1996, 'Korea Multi-Purpose Satellite Propulsion Subsystem Critical Design Audit Data Package,' KOMPSAT PS CDA, KARI-95-T01
|
7 |
Kim, M. Y., and Baek, S. W., 1996, 'Thermal Radiation Model for Rocket Plume Base Heating Using the Finite-Volume Method,' Transaction of the KSME(B), Vol. 20, No. 11, pp. 3598-3606
과학기술학회마을
|
8 |
Kim, J.S., Choi, H.S. and Han, C.Y., 11. 11. 2000, 'On-orbit Performance Analysis of KOMPSAT-1 Propulsion Subsystem,' Proceedings of the KSAS Fall Annual Meeting 2000, pp. 634-637
|
9 |
Analytix Corporation, 1996, AC/SINDA User's Manual
|
10 |
Gebhart, B., 1971, Heat Transfer, McGraw-Hill
|
11 |
Analytix Corporation, 1996, AC/TRASYS User's Manual
|