SB-735 (original) (raw)

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SB-735

Part of S-310

Japanese sounding rocket.

Status: Retired 1994.

Subtopics

ST-735 Japanese test vehicle. Two stage vehicle consisting of 1 x ST-735 + 1 x ST-735 stage 2

NAL-735 Japanese test vehicle. Single stage vehicle.

Country: Japan. Agency: ISAS. Bibliography: 2.

1984 January 17 - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K?. LV Family: SB-735. Launch Vehicle: ST-735.

SRB Sep test - . Nation: Japan. Agency: ISAS. Apogee: 50 km (31 mi).

1994 September 16 - . 04:00 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K?. LV Family: SB-735. Launch Vehicle: ST-735.

FIH test - . Nation: Japan. Agency: ISAS. Apogee: 118 km (73 mi).

2002 July 14 - . 01:34 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA1. LV Family: SB-735. Launch Vehicle: NAL-735. FAILURE: Failure.

National Experimental Supersonic Transport NEXST-1 test - . Nation: Japan. Agency: NAL. Apogee: 0 km (0 mi). The intention was that an 11.5-m-long, one tenth scale model of the aircraft would be propelled by the NAL-735 solid rocket booster to Mach 2 at 18 km altitude. Instead the vehicle lost stability and crashed near the launch point..

2005 October 9 - . 21:36 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA1. LV Family: SB-735. Launch Vehicle: NAL-735.

NEXST-1 F2 - . Nation: Japan. Agency: NAL. Apogee: 20 km (12 mi).

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