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Test vehicle. Year: 1988. Family: Other Suborbital Vehicles. Country: Japan. Single stage vehicle consisting of 1 x TR-1 Manufacturer: Nissan. Launches: 10. First Launch Date: 1988-09-05. Last Launch Date: 1998-11-18. Launch data is: continuing. Apogee: 80 km (49 mi). Liftoff Thrust: 608.000 kN (136,683 lbf). Total Mass: 11,800 kg (26,000 lb). Core Diameter: 1.13 m (3.70 ft). Total Length: 14.30 m (46.90 ft). Model: TR-1. Family: Other Suborbital Vehicles. Country: Japan. Single stage vehicle consisting of 1 x TR-1 Apogee: 80 km (49 mi). Liftoff Thrust: 608.000 kN (136,683 lbf). Total Mass: 11,800 kg (26,000 lb). Core Diameter: 1.13 m (3.70 ft). Total Length: 14.30 m (46.90 ft). Model: TR-1A. Family: Other Suborbital Vehicles. Country: Japan. Single stage vehicle consisting of 1 x TR-1A Apogee: 270 km (160 mi). Liftoff Thrust: 608.000 kN (136,683 lbf). Total Mass: 10,300 kg (22,700 lb). Core Diameter: 1.13 m (3.70 ft). Total Length: 13.40 m (43.90 ft). TR-1 Chronology 1988 September 5 - 23:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. LV Configuration: TR-1 TR-1-1. - H-II 1/4 Scale model test flight Nation: Japan. Agency: NASDA. Apogee: 80 km (49 mi). References: 1904.
1989 January 26 - 23:00 GMT - Launch Site: Tanegashima. Launch Complex: T. 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). References: 1904.
1989 August 19 - 23:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. LV Configuration: TR-1 TR-1-3. - H-II 1/4 Scale model test flight Nation: Japan. Agency: NASDA. Apogee: 80 km (49 mi). References: 1904.
1991 September 15 - 23:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. Model: TR-1A. LV Configuration: TR-1A TR-1A-1. - Microgravity mission Nation: Japan. Agency: NASDA. Apogee: 270 km (160 mi). References: 1904.
1992 August 19 - 23:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. Model: TR-1A. LV Configuration: TR-1A TR-1A-2. - Microgravity mission Nation: Japan. Agency: NASDA. Apogee: 290 km (180 mi). References: 1904.
1993 September 16 - 23:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. Model: TR-1A. LV Configuration: TR-1A TR-1A-3. - Microgravity mission Nation: Japan. Agency: NASDA. Apogee: 264 km (164 mi). References: 1904.
1995 August 24 - 22:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. Model: TR-1A. LV Configuration: TR-1A TR-1A-4. - Microgravity mission Nation: Japan. Agency: NASDA. Apogee: 270 km (160 mi). References: 1904.
1996 September 24 - 22:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. Model: TR-1A. LV Configuration: TR-1A TR-1A-5. - Microgravity mission Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi). References: 1904.
1997 September 25 - 00:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. Model: TR-1A. LV Configuration: TR-1A TR-1A-6. - Microgravity mission Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi). References: 1904.
1998 November 18 - 23:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: TR-1. Model: TR-1A. LV Configuration: TR-1A TR-1A-7. - Microgravity mission Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi). References: 1904.
Bibliography and Further Reading - McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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