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Vandenberg LF10
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Launch Facility 10 - Launch Site: Vandenberg. Launch Pads: 1. Latitude: 34.8715 N. Longitude: 120.6057 W. Minuteman 3. - 1987 July 12 - FOT GT123GM-1 Follow-on Test launch Launch Vehicle: Minuteman 3. Apogee: 1,300 km (800 mi).
- 1988 October 27 - FOT GT130GM Follow-on Test launch Launch Vehicle: Minuteman 3. Apogee: 1,300 km (800 mi).
- 1989 March 7 - FOT GT133GM Follow-on Test launch Launch Vehicle: Minuteman 3. Apogee: 1,300 km (800 mi).
- 1989 November 6 - FOT GT136GM Follow-on Test launch Launch Vehicle: Minuteman 3. Apogee: 1,300 km (800 mi).
- 1991 July 2 - FOT GT143GM Follow-on Test launch Launch Vehicle: Minuteman 3. Apogee: 1,300 km (800 mi).
- 1992 May 5 - FOT GT147GM-1 Follow-on Test launch Launch Vehicle: Minuteman 3. Apogee: 1,300 km (800 mi).
- 1996 June 26 12:17 - FOT GT162GM Follow-on Test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT162GM Apogee: 1,300 km (800 mi).
- 1997 June 18 10:01 - FOT GT165GM Follow-on Test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT165GM Apogee: 1,300 km (800 mi).
- 1998 June 24 12:46 - FOT GT168GM Follow-on Test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT168GB Apogee: 1,300 km (800 mi). FOT. Part of dual Minuteman 3 shot.
- 1999 August 20 08:45 - RCT-1 GT170GM/RRF-6 operational test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT170GM Apogee: 1,300 km (800 mi).
- 2000 June 9 08:01 - FOT GT172GM Follow-on Test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT172GM Apogee: 1,300 km (800 mi).
- 2001 February 7 09:28 - GT175GB Functional Dependency gate operational test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT176GM Apogee: 1,300 km (800 mi).
- 2002 April 8 09:29 - GT178GM Functional Dependency gate operational test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT178GM Apogee: 1,300 km (800 mi).
- 2003 September 10 11:31 - GT181GM Functional Dependency gate operational test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT181GM Apogee: 1,300 km (800 mi). Delayed from May
- 2004 June 23 08:32 - GT185GM Functional Dependency gate operational test launch Launch Vehicle: Minuteman 3. Minuteman 3 GT185GM Apogee: 1,300 km (800 mi). Missile Test Flight. Delayed from February.
- 2006 February 16 08:01 - SERV 3 Launch Vehicle: Minuteman 3. Apogee: 1,300 km (800 mi). Test
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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