Pressurizing test of CFRP model tank in cryogenic temperature

10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2001, Pages

  Morimoto, T ^a   Shimoda, T ^a   Morino, Y ^a   Hayashi, Y ^b   Yokozeki, T ^c   Ishikawa, T ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Tokyo Business Service Co Ltd   (Japan)

^c UNIVERSITY OF TOKYO   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894292522     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Robinson, Composite Cryogenic Propellant Tank Development, AIAA-94-1375-CP
2. st International Symposium on Space Technology and Science, 98-o-l-4V, Omiya, May 1998
3. Yoshiki Morino, Takashi Ishikawa, Takahira Aoki, Hisashi Kumazawa, and Youichi Hayasi, CFRP Material Characterization Testing for the RLV Cryogenic Propellant TANK, AIAA-99-1297
4. Makoto Yoshida, Takayuki Sudo, Masataka Nosaka, Tomohiko Goto, and Masayuki Yamashita, Evaluation of CFRP Tank Element Pressurized up to 2 MPa with Liquid Hydrogen, Proceedings of the Annual Meeting and the First Symposium on Propulsion System for Reusable Launch Vehicles, pp. 195-200, Sendai, March 1998
5. Takayuki Shimoda, Yoshiki Morino, Tetsuya Morimoto, and Takashi Ishikawa, Study on Application of CFRP to Cryogenic Tank forReusable Launch Vehicle, Proceedings of the Annual Meeting and the First Symposium on Propulsion System for Reusable Launch. Vehicles, pp. 89-94, Sendai, March 1998
6. Yoshiki Morino, Takayuki Shimoda, Tetsuya Morimoto, Takashi Ishikawa, and Takahira Aoki, Feasibility Study of the Cryogenic Composite Tnak for Reusable Launch Vehicles, IAF-99-I.3.06
7. th Aircraft Symposium, pp. 541-544, Tokyo, November 1999
8. nd international Symposium on Space Technology and Science, ISTS 2000-g-22, Morioka, May 2000
9. Takayuki Shimoda, Yoshiki Morino, and Tetsuya Morimoto, "Feasibility Study of CFRP Application to the Cryogenic Propellant Tank of Reusable Launch Vehicle, ISTS 2000-c-ll, Morioka, May 2000
10. Stefania Canton, Gandolfo Di Vita, Giovanni Totaro, Yoshiki Morino, and Tetsuya Morimoto, "Applicability of Filament Winding Method to Fabricate Cryogenic Composite Tanks for Liquid Propulsion, IAF-00-S.3.08