Japanese test vehicle. Single stage vehicle.
Success Rate: 100.00%. Launch data is: complete.
Status: Retired 1998.
Gross mass: 11,800 kg (26,000 lb).
Height: 14.30 m (46.90 ft).
Diameter: 1.13 m (3.70 ft).
Thrust: 608.00 kN (136,683 lbf).
Apogee: 80 km (49 mi).
First Launch: 1988.09.05.
Last Launch: 1989.08.19.
Number: 3 .
More... - Chronology...
Associated Countries
See also
Associated Manufacturers and Agencies
-
Nissan Japanese manufacturer of rocket engines and rockets. Nissan, Japan. More...
Bibliography
-
McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
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
-
TR-1-1 Solid rocket stage. 608.00 kN (136,684 lbf) thrust. Mass 10,800 kg (23,810 lb). More...
TR-1 Chronology
1988 September 5 - .
23:00 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
TR-1.
Launch Vehicle:
TR-1.
LV Configuration: TR-1 TR-1-1.
- H-II 1/4 Scale model test flight - .
Nation: Japan. Agency: NASDA. Apogee: 85 km (52 mi).
1989 January 26 - .
23:00 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
TR-1.
Launch Vehicle:
TR-1.
LV Configuration: TR-1 TR-1-2.
- H-II 1/4 Scale model test flight - .
Nation: Japan. Agency: NASDA. Apogee: 80 km (49 mi).
1989 August 19 - .
23:00 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
TR-1.
Launch Vehicle:
TR-1.
LV Configuration: TR-1 TR-1-3.
- H-II 1/4 Scale model test flight - .
Nation: Japan. Agency: NASDA. Apogee: 85 km (52 mi).
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