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Launch Complex: 395-A1.
Vandenberg. Latitude: 34.8066 deg. Longitude: -120.5442 deg. Used by: Titan. First Launch: 1961-09-23. Last Launch: 1964-12-08. Number Launches: 11. Silo

395-A1 Chronology

1961 September 23 - 20:36 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-2 Mk 4 re-entry vehicle research and development mission Agency: USAF. Apogee: 1,000 km (600 mi). Launched from Titan II silo

1962 February 23 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-18 FAILURE: Failure. Research and development Cat II / operational test Agency: USAF AFSC. Apogee: 50 km (31 mi).

1962 May 4 - 21:43 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-34 Research and development Category II test Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1962 October 6 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-35 Research and development Category II test Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1962 December 5 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-11 Research and development Category II test Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1963 January 29 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-8 Research and development Category II test Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1963 April 5 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I V-1 Research and development launch Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1963 May 1 - 10:15 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I V-4 FAILURE: Failure. Research and development launch Agency: USAF AFSC.

1963 August 15 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-7 Demonstration and shakedown operations launch Agency: USAF SAC. Apogee: 1,000 km (600 mi).

1963 November 14 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-68 Demonstration and shakedown operations launch Agency: USAF SAC. Apogee: 1,000 km (600 mi).

1964 December 8 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I SM-85 ST West Wind I operational test launch Agency: USAF SAC. Apogee: 1,000 km (600 mi).


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