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USAF AFMC
Part of USAF
American agency. Air Force Materiel Command, USA.
Country:
USA.
Spacecraft:
Landsat.
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).
1993 August 2 - .
19:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Titan.
Launch Vehicle:
Titan 403A.
FAILURE: Failure.
1993 October 5 - .
17:56 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4W.
LV Family:
Titan.
Launch Vehicle:
Titan II SLV.
FAILURE: Star-37XFP-ISS kick-motor malfunction..
Failed Stage: 3.
- Landsat 6 - .
Nation: USA.
Agency: USAF AFMC.
Program: Landsat.
Class: Earth.
Type: Earth resources satellite. Spacecraft: Landsat 6.
Decay Date: 1993-05-10 . Apogee: 724 km (449 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 January 27 - .
03:03 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC8.
LV Family:
Minuteman.
Launch Vehicle:
Minotaur 1.
- JAWSAT - .
Payload: P98-1. Mass: 64 kg (141 lb). Nation: USA.
Agency: USAF AFMC.
Manufacturer: Weber.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: JAWSAT.
USAF Sat Cat: 26061 . COSPAR: 2000-004A. Apogee: 805 km (501 mi). Perigee: 753 km (468 mi). Inclination: 100.20 deg. Period: 100.36 min. Joint USAF Academy/Weber State Satellite. Payloads included a plasma experiment, a particle detector, and a technology test..
- Falconsat - .
Mass: 52 kg (114 lb). Nation: USA.
Agency: USAF AFMC.
Manufacturer: USAF Colorado Springs.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: Falconsat.
USAF Sat Cat: 26064 . COSPAR: 2000-004D. Apogee: 810 km (503 mi). Perigee: 754 km (468 mi). Inclination: 100.20 deg. Period: 100.41 min. USAF Academy satellite, carried the CHAWS-LD (Charging Hazards and Wake Studies-Long Duration) experiment to measure spacecraft charging effects in LEO..
- OPAL - .
Payload: Orbiting Picosat Launcher. Mass: 13 kg (28 lb). Nation: USA.
Agency: USAF AFMC.
Manufacturer: Stanford.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: OPAL.
USAF Sat Cat: 26063 . COSPAR: 2000-004C. Apogee: 808 km (502 mi). Perigee: 754 km (468 mi). Inclination: 100.20 deg. Period: 100.39 min.
Stanford University Orbiting Picosat Automated Launcher. Carried an acclerometer, a magnetometer, and six small picosatellites - Picosat 1 and 2, Stensat, and the Artemis triplets (JAK, Thelma, and Louise). The first two were deployed on February 7 at 0334:16 GMT. OPAL transmitter problems delayed the initial release.
- ASUSAT - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Agency: USAF AFMC.
Manufacturer: Arizona.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: ASUSAT.
USAF Sat Cat: 26065 . COSPAR: 2000-004E. Apogee: 809 km (502 mi). Perigee: 754 km (468 mi). Inclination: 100.20 deg. Period: 100.40 min. Arizona State University satellite with an Earth imager and an amateur radio transponder..
2000 May 28 - .
20:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF06.
LV Family:
Minuteman.
Launch Vehicle:
Minotaur 2.
- OSPTLV 1 Target mission - .
Nation: USA.
Agency: USAF AFMC.
Apogee: 1,300 km (800 mi). OSP-TLV (TLV-Demo) Missile Defense Technology.
2000 July 8 - .
04:19 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF03.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
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.
2001 August 31 - .
20:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF21.
LV Family:
GBI.
Launch Vehicle:
GBI BV-Plus.
- GMDS BVT-2 test - .
Nation: USA.
Agency: USAF AFMC.
Manufacturer: Lockheed.
Apogee: 200 km (120 mi).
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