Encyclopedia Astronautica
TT-210


Japanese sounding rocket. Single stage vehicle.

Status: Retired 1976.
Gross mass: 200 kg (440 lb).
Height: 6.00 m (19.60 ft).
Diameter: 0.21 m (0.68 ft).
Apogee: 100 km (60 mi).
First Launch: 1975.08.17.
Last Launch: 1976.09.24.
Number: 3 .

More... - Chronology...


Associated Countries
See also
  • S Series of Japanese single-stage sounding rockets designed for low-cost observations of the ionosphere. More...

Associated Manufacturers and Agencies
  • NASDA Japanese agency overseeing development of rockets, spacecraft, and rocket engines. National Space Development Agency, Japan. More...

Associated Launch Sites
  • Tanegashima Japan's main launch site for he larger N and H launch vehicles. In use for sounding rockets from 1967 and orbital launches from 1975. As of 2007 over 140 major launches had been made from the site. More...

Associated Stages

TT-210 Chronology


1975 August 17 - . 06:00 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima T. LV Family: S. Launch Vehicle: TT-210. LV Configuration: TT-210 TT-210-1F.
  • Test mission - . Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi).

1976 January 27 - . 06:00 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima T. LV Family: S. Launch Vehicle: TT-210. LV Configuration: TT-210 TT-210-2F.
  • Test mission - . Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi).

1976 September 24 - . 01:30 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima T. LV Family: S. Launch Vehicle: TT-210. LV Configuration: TT-210 TT-210-3F.
  • Test mission - . Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi).

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