TR-1
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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