Tanegashima T home
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Launch Complex: T.
Tanegashima. Latitude: 30.3772 deg. Longitude: 130.9631 deg. Used by: Lambda, MT-135, S, TR-1. First Launch: 1967-01-01. Last Launch: 1998-11-18. Number Launches: 93. Takesaki Launch Site

T Chronology

1967 - Launch Vehicle: S. NAL-16 NAL-16TR Test mission Agency: STA. Apogee: 45 km (27 mi).

1968 September 17 - 07:10 GMT - Launch Vehicle: S. SA-II SA-II A9 Test mission Agency: STA. Apogee: 20 km (12 mi).

1968 September 19 - 01:58 GMT - Launch Vehicle: Lambda. LS-C-D Test mission Agency: STA. Apogee: 100 km (60 mi).

1968 September 19 - 07:01 GMT - Launch Vehicle: S. NAL-16 NAL-16H F1 Test mission Agency: STA. Apogee: 100 km (60 mi).

1969 January 30 - 01:31 GMT - Launch Vehicle: S. NAL-16 NAL-16 31D Test mission Agency: STA. Apogee: 50 km (31 mi).

1969 February 1 - 01:40 GMT - Launch Vehicle: S. NAL-25 NAL-25 31 Test mission Agency: STA. Apogee: 50 km (31 mi).

1969 February 6 - 06:31 GMT - Launch Vehicle: Lambda. LS-C-1 Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1969 February 7 - 06:30 GMT - Launch Vehicle: S. S-C SC-3 Test mission Agency: STA. Apogee: 85 km (52 mi).

1969 February 8 - 01:30 GMT - Launch Vehicle: S. S-C SC-4 Test mission Agency: STA. Apogee: 85 km (52 mi).

1969 February 8 - 06:30 GMT - Launch Vehicle: S. S-C SC-1 Test mission Agency: STA. Apogee: 85 km (52 mi).

1969 September 9 - 06:30 GMT - Launch Vehicle: S. S-B SB-III F11 Test mission Agency: STA. Apogee: 75 km (46 mi).

1969 September 10 - 06:30 GMT - Launch Vehicle: Lambda. LS-C-2 Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1969 September 15 - 01:40 GMT - Launch Vehicle: S. JCR-1 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1969 September 16 - 06:40 GMT - Launch Vehicle: S. JCR-2 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1969 September 20 - 01:55 GMT - Launch Vehicle: S. NAL-16 NAL-16H F2 Test mission Agency: STA. Apogee: 100 km (60 mi).

1969 September 20 - 06:30 GMT - Launch Vehicle: S. NAL-7 NAL-7 F7 Test mission Agency: STA. Apogee: 20 km (12 mi).

1970 February 1 - 01:00 GMT - Launch Vehicle: S. JCR-3 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1970 February 3 - 06:03 GMT - Launch Vehicle: Lambda. LS-C-3 Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1970 February 4 - Launch Vehicle: S. JCR-4 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1970 September 7 - 06:30 GMT - Launch Vehicle: S. NAL-7 NAL-7 BS9 Test mission Agency: STA. Apogee: 20 km (12 mi).

1970 September 9 - 06:40 GMT - Launch Vehicle: Lambda. LS-C-4 Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1971 February 1 - 01:30 GMT - Launch Vehicle: S. JCR-5 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1971 February 3 - 01:35 GMT - Launch Vehicle: S. S-B SB-III A12 Test mission Agency: STA. Apogee: 75 km (46 mi).

1971 February 3 - 06:30 GMT - Launch Vehicle: S. S-B SB-III A13 Test mission Agency: STA. Apogee: 75 km (46 mi).

1971 September 6 - 01:35 GMT - Launch Vehicle: S. S-B SB-III A14 Test mission Agency: STA. Apogee: 75 km (46 mi).

1971 September 10 - 06:47 GMT - Launch Vehicle: Lambda. LS-C-5 Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1971 September 11 - 01:45 GMT - Launch Vehicle: S. S-B SB-III A15 Test mission Agency: STA. Apogee: 75 km (46 mi).

1971 September 17 - 06:40 GMT - Launch Vehicle: S. JCR-6 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1972 February 2 - 06:56 GMT - Launch Vehicle: MT-135. MT-135P T1 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1972 February 6 - 06:35 GMT - Launch Vehicle: S. JCR-7 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1972 February 7 - 06:45 GMT - Launch Vehicle: MT-135. MT-135P T2 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1972 August 30 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T3 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1972 August 30 - 06:15 GMT - Launch Vehicle: MT-135. MT-135P T4 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1972 September 25 - 06:05 GMT - Launch Vehicle: Lambda. LS-C-6 Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1973 February 5 - 01:52 GMT - Launch Vehicle: MT-135. MT-135P T5 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1973 February 7 - 01:50 GMT - Launch Vehicle: S. JCR-8 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1973 February 8 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T6 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1973 September 5 - 01:57 GMT - Launch Vehicle: MT-135. MT-135P T7 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1973 September 5 - 06:30 GMT - Launch Vehicle: MT-135. MT-135P T8 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1973 September 7 - 01:40 GMT - Launch Vehicle: S. JCR-9 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1974 February 1 - 06:30 GMT - Launch Vehicle: S. JCR-10 Test mission Agency: NASDA. Apogee: 200 km (120 mi).

1974 February 2 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T9 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1974 February 9 - 06:30 GMT - Launch Vehicle: Lambda. LS-C-7 LE-3 test Agency: NASDA. Apogee: 100 km (60 mi).

1974 February 10 - 06:30 GMT - Launch Vehicle: MT-135. MT-135P T10 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1974 September 3 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T11 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1974 September 3 - 06:00 GMT - Launch Vehicle: MT-135. MT-135P T12 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1975 January 30 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T13 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1975 February 7 - 01:00 GMT - Launch Vehicle: MT-135. MT-135P T14 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1975 August 17 - 06:00 GMT - Launch Vehicle: S. TT-210 TT-210-1F Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1975 September 10 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T15 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1976 January 27 - 06:00 GMT - Launch Vehicle: S. TT-210 TT-210-2F Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1976 September 23 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T16 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1976 September 24 - 01:30 GMT - Launch Vehicle: S. TT-210 TT-210-3F Test mission Agency: NASDA. Apogee: 100 km (60 mi).

1976 September 25 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T17 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1977 January 25 - 01:30 GMT - Launch Vehicle: S. TT-500 TT-500-1F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1977 February 24 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T18 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1977 August 23 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T19 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1977 August 25 - 01:30 GMT - Launch Vehicle: S. TT-500 TT-500-2F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1977 August 26 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T20 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1978 January 16 - 01:30 GMT - Launch Vehicle: S. TT-500 TT-500-3F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1978 February 17 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T21 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1978 August 24 - 01:45 GMT - Launch Vehicle: MT-135. MT-135P T22 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1978 August 25 - 01:30 GMT - Launch Vehicle: S. TT-500 TT-500-4F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1978 August 26 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T23 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1979 January 27 - 01:30 GMT - Launch Vehicle: S. TT-500 TT-500-5F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1979 February 7 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T24 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1979 August 25 - 01:40 GMT - Launch Vehicle: S. TT-500 TT-500-6F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1979 August 27 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T25 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1979 August 27 - 06:00 GMT - Launch Vehicle: MT-135. MT-135P T26 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1980 January 28 - 01:30 GMT - Launch Vehicle: S. TT-500 TT-500-7F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1980 February 23 - 01:55 GMT - Launch Vehicle: MT-135. MT-135P T27 Aeronomy mission Agency: NASDA. Apogee: 55 km (34 mi).

1980 September 13 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T28 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1980 September 13 - 22:00 GMT - Launch Vehicle: S. TT-500A TT-500A-8F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1980 September 15 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T29 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1981 January 14 - 22:00 GMT - Launch Vehicle: S. TT-500A TT-500A-9F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1981 February 12 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T30 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1981 August 1 - 22:00 GMT - Launch Vehicle: S. TT-500A TT-500A-10F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1982 February 2 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T31 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1982 February 3 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T32 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1982 August 15 - 23:15 GMT - Launch Vehicle: S. TT-500A TT-500A-11F Test mission Agency: NASDA. Apogee: 300 km (180 mi).

1982 September 5 - 01:30 GMT - Launch Vehicle: MT-135. MT-135P T33 Aeronomy mission Agency: NASDA. Apogee: 50 km (31 mi).

1983 January 26 - 23:00 GMT - Launch Vehicle: S. TT-500A TT-500A-12F Microgravity mission Agency: NASDA. Apogee: 300 km (180 mi).

1983 August 18 - 23:00 GMT - Launch Vehicle: S. TT-500A TT-500A-13F Microgravity mission Agency: NASDA. Apogee: 300 km (180 mi).

1988 September 5 - 23:00 GMT - Launch Vehicle: TR-1. TR-1 TR-1-1 H-II 1/4 Scale model test flight Agency: NASDA. Apogee: 85 km (52 mi).

1989 January 26 - 23:00 GMT - Launch Vehicle: TR-1. TR-1 TR-1-2 H-II 1/4 Scale model test flight Agency: NASDA. Apogee: 80 km (49 mi).

1989 August 19 - 23:00 GMT - Launch Vehicle: TR-1. TR-1 TR-1-3 H-II 1/4 Scale model test flight Agency: NASDA. Apogee: 85 km (52 mi).

1991 September 15 - 23:00 GMT - Launch Vehicle: TR-1. TR-1A TR-1A-1 Microgravity mission Agency: NASDA. Apogee: 270 km (160 mi).

1992 August 19 - 23:30 GMT - Launch Vehicle: TR-1. TR-1A TR-1A-2 Microgravity mission Agency: NASDA. Apogee: 290 km (180 mi).

1993 September 16 - 23:00 GMT - Launch Vehicle: TR-1. TR-1A TR-1A-3 Microgravity mission Agency: NASDA. Apogee: 264 km (164 mi).

1995 August 24 - 22:00 GMT - Launch Vehicle: TR-1. TR-1A TR-1A-4 Microgravity mission Agency: NASDA. Apogee: 270 km (160 mi).

1996 September 24 - 22:00 GMT - Launch Vehicle: TR-1. TR-1A TR-1A-5 Microgravity mission Agency: NASDA. Apogee: 100 km (60 mi).

1997 September 25 - 00:30 GMT - Launch Vehicle: TR-1. TR-1A TR-1A-6 Microgravity mission Agency: NASDA. Apogee: 100 km (60 mi).

1998 November 18 - 23:00 GMT - Launch Vehicle: TR-1. TR-1A TR-1A-7 Microgravity mission Agency: NASDA. Apogee: 100 km (60 mi).


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