Evaluation by Rocket Combustor of C/C Composite Cooled Structure Using Metallic Cooling Tubes

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES SPACE TECHNOLOGY JAPAN ◽

10.2322/tstj.7.pc_61 ◽

2009 ◽

Vol 7 (ists26) ◽

pp. Pc_61-Pc_66

Author(s):

Masao TAKEGOSHI ◽

Fumiei ONO ◽

Shuichi UEDA ◽

Toshihito SAITO ◽

Osamu HAYASAKA

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