Development of thermal protection system of the MUSES-C/DASH reentry capsule

Acta Astronautica

Volumn 51, Issue 1-9, 2002, Pages 63-72

  Yamada, Tetsuya ^a   Inatani, Yoshifumi ^a   Honda, Masahisa ^b   Hirai, Ken'ich ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b IHI CORPORATION   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ABLATION; AERODYNAMIC HEATING; HEAT TRANSFER; ORBITS; PYROLYSIS; SPACE FLIGHT; SPACECRAFT; THERMOCOUPLES;

ASTEROIDS; INTERPLANETARY TRANSFER ORBITS; SPACE MISSIONS; THERMAL PROTECTION SYSTEMS;

SPACE RESEARCH;

EID: 10644241752     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(02)00054-1     Document Type: Conference Paper

References (14)

1. MUSES-C Mission Plan, MUSES-C Working group, ISAS, March. 2000.
2. DASH Mission Plan, DASH Working group, ISAS,September, 2000.
3. R. W. Detra, N. H. Kemp, F. R. Riddel, Jet Propulsion, vol. 27; Dec. 1957.
4. M. E. Tauber & K. Sutton , J. Spacecraft, vol. 28, no. 1, pp.40-42, 1991.
5. K. Suzuki, et. al., 21st ISTS 98-d-02, 1998.
6. K. Fujita,"SPRADIAN-Structured Package of Radiation Analysis", ISAS report no. 669, Sept. 1997.
7. Komurasaki, K. & Candler, G.V., "Laminar to Turbulent Transition Prediction around the MUSES-C Reentry Capsule, AIAA 98-2941,June 1998.
8. T. Yamada, Y. Inoue, et. al., Proc. symposium on dynamics of astronautics, ISAS, 1997.
9. T. Yamada, "Effect of Internal Pyrolysis Gas Pressure on the the Ablator Performance", 22nd International Sympo. Space Technology and Science, Morioka, Japan, 1999.
10. Shimada, T., Hirai, K.,"Mathematical Modeling of Ablation Analysis Code taking account of Pyrolysis Gas and Incoming Airflow", IA contractor report, 691(A)-M-10-183,1999.
11. Hirai, K., Niikura, K., Nogi, S. & Shimada, T., "Numerical Simulations of Charring Ablation for the Heat Shields on Super-orbital Reentry Capsule", ISTS 98 d-08, 21st International symposium on Space Technology and Science, Japan, 1998
12. Tetsuya Yamada, Yoshifumi Inatani, "ISAS High Enthalpy Flow Facility for Thermal Protection Material Tests", IEPC-99-233, 26th IEPC, Kitakyushu, Japan, Oct. 17-21, 1999.
13. Suzuki, K., Kubota, H., Fujita, K. & Abe, T., "Chemical Nonequilibrium Ablation Analysis of MUSES-C Super-orbital reentry Capsule", AIAA 97-2481, June, 1997
14. Ohtsu, H., Suzuki, K., Fujita, K. & Abe, T.,"Effect of Ablative Gas on the Radiative Environment around the MUSES-C Reentry Capsule"' AIAA 99-3463, June, 1999