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Vandenberg LF03
Part of Vandenberg Family
Minuteman, Minotaur launch silo. Originally a Minuteman 394 SMS silo. Upgraded for use as a Launch Facility in 1964, and later again modified to launch the Minotaur.

AKA: 394A2. First Launch: 1963-04-30. Last Launch: 2001-07-15. Number: 96 . Longitude: -120.5699 deg. Latitude: 34.8427 deg.



Launch Vehicles: Minuteman 1A, Minuteman 1B, Minuteman 2, Minotaur 2. Launch Sites: Vandenberg.

1963 April 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1A.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 July 11 - . 23:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1A.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1963 November 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1A.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 January 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. 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 - . 02:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

    The first successful multiple Minuteman ICBM launch was executed at the Pacific Missile Range when two Wing II Minuteman I (LGM-30B) missiles (FTM 813 and 688) were launched by SAC's First Strategic Aerospace Division (ISTRAD). Both missiles were launched separately in the salvo mode; the ripple mode was not used for these launches. These were also the initial two Minuteman IB operational test launches.


1964 March 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. FAILURE: Failure.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1.00 km (0.60 mi).

1964 April 23 - . 11:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 May 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 July 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 August 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 September 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 November 3 - . 00:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1965 January 20 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1965 March 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1965 April 30 - . 22:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1965 June 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1965 July 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1966 March 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. 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 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. 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 31 - . 20:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. 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 11 - . 19:22 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. 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 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1966 September 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. FAILURE: Failure.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 100 km (60 mi).

1966 October 13 - . 22:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1966 November 22 - . 21:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1966 December 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Flight operational test / salvo launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 January 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 February 21 - . 22:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - ripple launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 March 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. 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 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). The 100th Minuteman IB (LGM-30B) missile (#65-101) was launched from Vandenberg AFB, California. .

1967 May 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 June 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 September 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GB46 Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 December 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GB50 Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 December 22 - . 00:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT02B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). The 125th Minuteman I (LGM-30B) missile was launched from Vandenberg AFB and was the 200th Minuteman ICBM to be launched down the Western Test Range since September 1962. .

1968 April 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ST Olympic T. B-2 operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1968 May 22 - . 10:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ST Olympic T. B-3 operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1968 July 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ST Olympic T. B-4 operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 January 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT32B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 March 25 - . 19:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT34B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 July 1 - . 04:36 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT38B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 August 28 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT42B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 October 3 - . 01:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT44B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). SAC's 1st Strategic Aerospace Division launched the 150th Minuteman IB, LGM-30B #64-424, to be launched from Vandenberg. .

1969 November 26 - . 05:27 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT49B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 March 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT62B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 May 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT65B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 June 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT73B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 September 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT75B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 October 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT78B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 March 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT92B-3 Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 December 10 - . 01:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • FOT GT99B-1 Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1973 April 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • HK-2 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 December 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • HK-4? Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 April 27 - . 08:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-35 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 July 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES/SAMAST re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 August 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-46 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 January 19 - . 11:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Trident SFT-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). The first Minuteman launch in the HAVE FLY Program occurred. This was part of the Navy's Trident Supplemental Flight Test program. .

1975 May 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES NTV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 September 30 - . 10:02 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-05 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 November 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-16 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 February 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ANT-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

    The advanced nosetip test vehicle (A.N.T.)-l was successfully launched from Vandenberg AFB. The purpose of the flight was to test the performance of four nosetips of various materials and shapes with fine-weave carbon-carbon nosetips in high stagnation pressure and clean air.


1978 June 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ANT-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Four small reentry vehicles were successfully launched down the Western Test Range in an effort to evaluate the performance of several nosetip materials in clear weather. The launch was referred to as Advanced Nosetip Test III (A.N.T. III). .

1979 January 24 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ABRV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 July 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES LBRV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

    The Large Ballistic Recovery Vehicle (LBRV) was launched from Vandenberg AFB to Kwajalein lagoon on a Minuteman 1 booster. The purpose of the experiment was to recover the external shell of a Mark 12A reentry vehicle intact after reentry in order to assess the performance of staple-fiber heatshields. The LBRV was successfully


1979 December 20 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES AMARV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 April 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES STREP-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 October 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES AMARV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 March 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TDV-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 October 4 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES AMARV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1982 October 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-21 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 January 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP LBRV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 May 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-22 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 May 28 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-12 (HOE) Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 December 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-12A (HOE) Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1984 June 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-13 (HOE) Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1984 October 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP IPA-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1985 May 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP IPA-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1986 March 17 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP IPA-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1987 January 20 - . 08:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. FAILURE: Failure.
  • SENT-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 90 km (55 mi).

1987 September 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SENT-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1988 January 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP TDMaRV re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1990 February 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP MAST re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1991 January 28 - . 18:03 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • GBI-1 ERIS Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1991 May 11 - . 20:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • GBI-2 ERIS Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

    This was intended to be the second ERIS intercept flight, but there was either an ERIS launcher problem or a range safety problem that aborted the attempt after the target vehicle was on its way towards Kwajalein.It took just over one year to recover from that abort and to perform the intercept attempt against target vehicle "2B".


1991 June 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP AST re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1992 March 13 - . 18:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • GBI-2B ERIS Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1992 October 25 - . 01:06 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. FAILURE: Failure.
  • RSLP AST-DT 2 Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 100 km (60 mi).

1993 June 15 - . 17:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. FAILURE: Failure.
  • RSLP TDT-1 Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1.00 km (0.60 mi).

1996 September 27 - . 16:51 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • MSLS - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi).

1997 January 17 - . 01:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • IFT-1 EKV Target Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,300 km (800 mi). Minuteman launched an MSLS target vehicle for the EKV anti-ballistic missile interceptor launched from Kwajalein Atoll..

1997 June 24 - . 03:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • MSLS IFT-1A Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi).

    RSLP (MSLS) IFT-1A. The target cluster consisted of 10 objects: one mock warhead, one bus (the stage of the missile which releases the warhead and decoys), and eight decoys. Three decoys were conical in shape, like the warhead, and five were spherical balloons. One balloon was large – 2.2 meters in diameter – and had a brighter IR signature than the mock warhead. The two medium-sized balloons were about as bright as the mock warhead; they did not deploy as expected and were not reliable parts of the testing program. The two small balloons were released via a canister and were much dimmer than the mock warhead.


1998 January 16 - . 03:25 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • MSLS IFT-2 Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi). The same decoy set used in IFT-1A was also used in IFT-2. The target cluster consisted of 10 objects: one mock warhead, the bus (the stage of the missile which releases the warhead and decoys), and eight decoys..

1999 October 3 - . 02:01 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • MSLS IFT-3 Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi).

    The only decoy used in IFT-3 was the large balloon from IFT-1A and IFT-2. It had an IR signature six times higher than that of the mock warhead. Because the decoy was so much brighter than the mock warhead, the EKV saw it first. Once the EKV realized that the balloon’s IR signature did not match the target data loaded prior to the test, the interceptor shifted to the nearby target.


2000 January 19 - . 02:19 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • MSLS IFT-4 Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi). The only decoy used was the single large balloon from the previous tests. Smaller balloons originally had been planned to be a part of IFT-4, but were dropped in an attempt to simplify the test..

2000 July 8 - . 04:19 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • MSLS IFT-5 Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,300 km (800 mi).

    A C-band transponder on the mock warhead provided location information; its data was compared against its GPS receiver to determine its accuracy. The only decoy used was the large balloon from previous tests. It did not inflate properly, causing MDA officials to use a different decoy in the future.


2001 July 15 - . 02:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • IFT-6 GMDS target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi).

    The Minuteman II flew a suborbital trajectory with an apogee of around 1600 km and reentered near Kwajalein Atoll. The Boeing Minuteman II had an M55E1 first stage, an SR19 second stage and an M57A1 third stage. One large decoy balloon was used, 1.7 meters in diameter, slightly smaller than the balloon used earlier as a decoy. This new decoy still had an IR signature much brighter (approximately three times) than that of the mock warhead.


2002 March 16 - . 02:11 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minotaur 2.
  • IFT-8 GMDS target mission - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,600 km (900 mi). A mock warhead and three decoy balloons (one large, two small) were used to increase the difficulty of determining the target’s location..


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