Radiative heating analysis around the MUSES-C reentry capsule at a superorbital speed

Radiative heating analysis around the MUSES-C reentry capsule at a superorbital speed

Author(s):

Otsu, Hirotaka ( University of Tokyo )
Suzuki, Kojiro ( University of Tokyo )
Fujita, Kazuhisa ( The Institute of Space and Astronautical Science, Japan )
Abe, Takashi ( The Institute of Space and Astronautical Science, Japan )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME Joint Thermophysics and Heat Transfer Conference

Ser. no.:

1998

Pub. Year:

1998

No.:

98-2447

Paper no.:

98-2447

Page(from):

1

Page(to):

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050862
Series ID:	PA00000169
Conf. info. (Name):	AIAA/ASME Joint Thermophysics and Heat Transfer Conference
Conf. info. (Number):	7th
Conf. info. (Venue):	Albuquerque, NM
Conf. info. (Date):	1998.06.15-1998.16.18
Note for article:	7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, June 15-18, 1998/Albuquerque, NM

Similar Items:

1 Technical Paper Effect of Ablative Gas on the Radiative Environment around the MUSES-C Reentry Capsule Otsu, Hirotaka, Suzuki, Kojiro, Fujita, Kazuhisa, Abe, Takashi American Institute of Aeronautics and Astronautics	7 Technical Paper Assessment of the Thermochemical Model for a Super-Orbital Reentry Flow. Otsu, H., Sasoh, A., Fujita, K., Abe, T. American Institute of Aeronautics and Astronautics
2 Technical Paper Effect of ablative gas on the radiative environment around the MUSES-C reentry capsule Otsu, Hirotaka, Suzuki, Kojiro, Fujita, Kazuhisa, Abe, Takashi American Institute of Aeronautics and Astronautics	8 Technical Paper Research on the heatshield for MUSES-C earth reentry Park, Chul, Abe, Takashi, Inatani, Yoshifumi American Institute of Aeronautics and Astronautics
3 Technical Paper Effect of Models for Transport Properties on the Hypersonic Reentry Heating Environment Otsu,Hirotaka, Kanai,Norihiko, Fujita,Kazuhisa, Abe,Takashi American Institute of Aeronautics and Astronautics	9 Technical Paper Parachute system of MUSES-C reentry capsule Hinada, Motoki, Hiraki, Koju, Ishii, Nobuaki, Inatani, Yoshifumi, Nakajima, Takashi, Honda, Masahisa American Institute of Aeronautics and Astronautics
4 Technical Paper Chemical nonequilibrium ablation analysis of MUSES-C Super-orbital reentry capsule Suzuki, K., Kubota, H., Fujita, K., Abe, T. American Institute of Aeronautics and Astronautics	10 Technical Paper Reentry Heating Mitigation by Utilizing the Hall Effect Otsu, H., Matsushita, K., Detlev, K., Abe, T., Funaki, I. American Institute of Aeronautics and Astronautics
5 Technical Paper Air radiation analysis of a superorbital reentry vehicle Fujita, K., Abe, T., Suzuki, K. American Institute of Aeronautics and Astronautics	11 Technical Paper Laminar-to-turbulent transition prediction around the MUSES-C reentry capsule Komurasaki, K., Candler, G.V. American Institute of Aeronautics and Astronautics
6 Technical Paper Rarefied gas effects on the magnetic flow control system for aerobraking flight of the reentry vehicle Otsu, Hirotaka, Katsurayama, Hiroshi, Abe, Takashi, Konigorski, Detlev American Institute of Aeronautics and Astronautics	12 Technical Paper Reentry Environment Advanced Diagnostics (READ) Flight Experiment on USERS Reentry Vehicle Abe,T., Fujita,K., Otsu,H., Hama,K., Shingu,S., Ichizono,K. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12