DocumentCode :
1737346
Title :
Search for the Japanese H-II Rocket Flight No. 8
Author :
Momma, Hiroyasu ; Watanabe, Masayuki ; Mitsuzawa, Kyohiko ; Danno, Kunioki ; Ida, Masahiko
Author_Institution :
Japan Marine Sci. & Technol. Center, Yokosuka, Japan
Volume :
2
fYear :
2000
fDate :
2000
Firstpage :
1115
Abstract :
In November 1999, the H-II Rocket Flight No. 8 was launched from Tanegashima Space Center. However, the first stage engine stopped suddenly in 4 minutes. Consequently, the engine dropped 380 nautical miles off Izu-Ogasawara Islands in 3000 m of water. The JAMSTEC was requested to search for the first stage engine in order to identify the cause of the failure. The search area was a box, 3.3 km in width and 26 km in length. First of all, the survey using 40 kHz side scan sonar on board the ROV Kaiko was carried out. After seven days of sonar survey, a probable contact was obtained. It was the engine section. However, the main engine was not discovered yet. Then, the JAMSTEC/Deep Tow sonar was deployed in the second cruise. On the second day, sonar contacts were obtained approximately 15 km southeast of the engine section. On December 24 in 1999, the main engine was discovered by the deep tow camera, In the third cruise, nozzle skirt of the main engine was discovered by the ROV Dolphin-3 K. Finally, the main engine was recovered approximately two months after the launch
Keywords :
oceanographic regions; oceanography; rockets; seafloor phenomena; space debris; water pollution; AD 1999 11; Izu-Ogasawara Islands; Japanese H-II Rocket Flight No. 8; North Pacific; Tanegashima Space Center; debris; engine; nozzle skirt; ocean; pollution; rocket; seafloor; search; Accidents; Combustion; Engines; Hydrogen; Remotely operated vehicles; Rockets; Satellites; Solids; Sonar; Space technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
OCEANS 2000 MTS/IEEE Conference and Exhibition
Conference_Location :
Providence, RI
Print_ISBN :
0-7803-6551-8
Type :
conf
DOI :
10.1109/OCEANS.2000.881752
Filename :
881752
Link To Document :
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