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NAL-735
Part of SB-735 Family
Japanese test vehicle. Single stage vehicle.

Status: Active. First Launch: 2002-07-14. Last Launch: 2005-10-09. Number: 2 . Gross mass: 4,700 kg (10,300 lb). Height: 10.00 m (32.00 ft). Diameter: 0.74 m (2.42 ft). Apogee: 18 km (11 mi).



Family: test vehicle. Country: Japan. Launch Sites: Woomera, Woomera LA1. Stages: NAL-735 engine. Agency: ISAS.

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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