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Vandenberg LF02
Part of Vandenberg
Minuteman test and training silo. Operational 21 November 1961. Originally for Minuteman I, converted to Minuteman II in 1967 and later to Minuteman III; converted to Peacekeeper in 1985. Finally adopted for Minotaur launches.
AKA: 394A1. First Launch: 1963-04-12. Last Launch: 2003-03-12. Number: 76 . Longitude: -120.57 deg. Latitude: 34.84 deg.
Country:
USA.
Launch Vehicles:
Minuteman 1A,
Minuteman 1B,
Minuteman 2,
Minuteman 3,
Peacekeeper.
Launch Sites:
Vandenberg.
1963 April 12 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1A.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1963 June 28 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1A.
- Demonstration and shakedown operations launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1963 August 8 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1A.
- Demonstration and shakedown operations launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1963 December 13 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Demonstration and shakedown operations launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1964 January 16 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Demonstration and shakedown operations launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1964 February 25 - .
02:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
1964 March 24 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1964 May 7 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1964 June 15 - .
12:40 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1964 July 7 - .
19:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1964 September 10 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1964 November 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
FAILURE: Failure.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 0 km (0 mi).
1964 December 9 - .
20:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1965 February 2 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1965 March 16 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1965 April 13 - .
21:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1965 June 10 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
FAILURE: Failure.
- Operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 10 km (6 mi).
1966 March 8 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Follow-on operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1966 April 4 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Follow-on operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1966 May 2 - .
20:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Follow-on operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1966 June 2 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Follow-on operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1966 July 13 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
FAILURE: Failure.
- Follow-on operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 10 km (6 mi).
1966 August 16 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Follow-on operational missile test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1967 April 28 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1967 May 19 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1967 June 29 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1967 July 15 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- GIN BABY I research and development mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1967 November 3 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- GIN BABY II research and development mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1967 December 8 - .
21:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 1B.
- GIN BABY IV research and development mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1969 January 29 - .
10:34 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
- ST - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1969 April 11 - .
08:55 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi). Minuteman III (LGM-30G) flight test missile (FTM) 301, the first test missile launched from Vandenberg but the fourth R&D missile to be fired, completed a 5,000-mile flight and impacted near the Marshall Islands. .
1969 May 29 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1969 September 13 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1969 October 15 - .
11:16 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1969 October 31 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1970 April 22 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1970 May 8 - .
07:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1970 June 17 - .
08:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi).
1970 July 28 - .
23:17 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi). The final flight test missile in the basic Minuteman III research and development program was launched from Vandenberg AFB. Twenty-five missiles had been launched in the program - eleven from Vandenberg and fourteen from Cape Canaveral. .
1970 September 26 - .
07:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OLD FOX 02M demonstration and shakedown operations launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1971 February 17 - .
07:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OLD FOX 05M demonstration and shakedown operations launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1971 May 27 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT03GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi). A Minuteman III fired for a SAC Phase I Operational Test was the 350th Minuteman missile launched from Vandenberg AFB since September 1962. .
1971 July 8 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT04GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1971 September 3 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT05GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1971 October 15 - .
09:05 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT06GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1971 November 23 - .
06:55 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT08GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1972 January 26 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT11GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1972 June 11 - .
20:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- OT GT14GM operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1972 October 20 - .
09:05 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
- FOT GT110M Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1972 December 5 - .
02:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- FOT GT41GM Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1973 April 18 - .
04:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
- FOT GT112M Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1973 September 5 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- FOT GT43GM Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1974 April 2 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
- FOT GT119M Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1974 May 2 - .
22:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- FOT GT44GM Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1974 August 17 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- FOT GT45GM Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1974 October 8 - .
03:35 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
- FOT GT118M Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1975 May 16 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- PAVE PEPPER test - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi). Special Test Missile-9W (STM-9W) was the first Pave Pepper flight test. It was successful. The program was designed to evaluate the use of increased numbers of reentry vehicles on the Minuteman III missile. .
1975 July 26 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- PAVE PEPPER test - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi). Special Test Missile (STM)-IOW was successfully launched from Vandenberg AFB. .
1986 August 23 - .
18:25 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Test mission - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,000 km (600 mi).
1986 December 5 - .
16:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- 10 RV (2 ft deploy) - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,000 km (600 mi).
1989 September 14 - .
19:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
FAILURE: Failure.
- Operational test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 200 km (120 mi).
1991 March 12 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,000 km (600 mi).
1991 September 17 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,000 km (600 mi).
1992 July 1 - .
02:20 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF ACC.
Apogee: 1,000 km (600 mi).
1993 March 2 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF ACC.
Apogee: 1,000 km (600 mi).
1993 September 15 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 1,000 km (600 mi).
1994 May 17 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 1,000 km (600 mi).
1995 January 19 - .
20:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 1,000 km (600 mi).
1995 August 30 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 1,000 km (600 mi).
1996 May 30 - .
08:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 1,000 km (600 mi).
1996 November 6 - .
13:06 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- Operational test - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 1,000 km (600 mi).
1997 November 5 - .
21:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- 8 RVs operational test launch - .
Nation: USA.
Agency: USAF.
Apogee: 1,000 km (600 mi).
1999 March 10 - .
08:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- 8 RVs operational test launch - .
Nation: USA.
Agency: USAF.
Apogee: 1,000 km (600 mi).
2001 July 27 - .
08:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
FAILURE: ICBM was destroyed during flight.
- 9 RVs Functional Dependency gate operational test launch - .
Nation: USA.
Agency: USAF AFSPC.
Apogee: 100 km (60 mi). FDEP. The Peackeeper ICBM was destroyed during flight and did not reach its planned 1000 km apogee..
2002 June 3 - .
08:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- GT-31PA - 9 RVs Functional Dependency gate operational test launch - .
Nation: USA.
Agency: USAF.
Apogee: 1,000 km (600 mi).
2004 July 21 - .
08:01 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF02.
Launch Vehicle:
Peacekeeper.
- GT-33PA - 8 RVs Functional Dependency gate operational test launch - .
Nation: USA.
Agency: USAF.
Apogee: 1,000 km (600 mi). ICBM Demonstration Flight. Delayed from March..
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