Encyclopedia Astronautica
USAF STP


American agency overseeing development of spacecraft. USAF STP, USA.

AKA: USAF.

More... - Chronology...


Associated Countries
Associated Spacecraft
  • Musketball American technology satellite. One launch, 1971.08.07. Space craft engaged in investigation of spaceflight techniques and technology. More...
  • REX American earth ionosphere satellite. 2 launches, 1991.06.29 (REX) and 1996.03.09 (REX-II). The REX satellites were designed to study scintillation effects of the Earth's atmosphere on RF transmissions. More...
  • STEP American technology satellite. 2 launches, 1995.06.22 (STEP 3) and 2000.06.07 (TSX 5). More...

See also
  • Agency Agencies or institutions overseeing design, development, construction, or operation of space-related systems. More...

Associated Programs
  • STEP Space Test Experiment Program; series of USAF technology test satellites. More...

USAF STP Chronology


1971 June 8 - . 14:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC10W. LV Family: Delta. Launch Vehicle: Thor Burner 2. LV Configuration: Thor Burner 2 210.
  • SESP 70-1 - . Payload: P70-1 / Burner II No. 12 / OPS 3850. Mass: 260 kg (570 lb). Nation: USA. Agency: USAF STP. Class: Technology. Type: Military technology satellite. Spacecraft: SESP. Decay Date: 1982-01-31 . USAF Sat Cat: 5285 . COSPAR: 1971-054A. Apogee: 580 km (360 mi). Perigee: 544 km (338 mi). Inclination: 90.2000 deg. Period: 95.80 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1971 August 7 - . 00:11 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 76F / OV-1 (2x).
  • OV1-20P - . Mass: 70 kg (154 lb). Nation: USA. Agency: USAF STP. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1971-08-28 . USAF Sat Cat: 5394 . COSPAR: 1971-067A. Apogee: 1,932 km (1,200 mi). Perigee: 136 km (84 mi). Inclination: 92.0000 deg. Period: 105.90 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OV1-21P - . Mass: 70 kg (154 lb). Nation: USA. Agency: USAF STP. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 5397 . COSPAR: 1971-067B. Apogee: 896 km (556 mi). Perigee: 778 km (483 mi). Inclination: 87.6000 deg. Period: 101.70 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • Cannonball 2 - . Payload: LOADS 2. Mass: 364 kg (802 lb). Nation: USA. Agency: USAF STP. Class: Military. Type: Radar calibration target. Spacecraft: Cannonball. Decay Date: 1972-01-31 . USAF Sat Cat: 5382 . COSPAR: 1971-067C. Apogee: 1,970 km (1,220 mi). Perigee: 133 km (82 mi). Inclination: 92.0000 deg. Period: 106.30 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • Musketball 1 - . Payload: RTDS. Nation: USA. Agency: USAF STP. Class: Technology. Type: Navigation technology satellite. Spacecraft: Musketball. Decay Date: 1971-09-19 . USAF Sat Cat: 5383 . COSPAR: 1971-067D. Apogee: 859 km (533 mi). Perigee: 134 km (83 mi). Inclination: 87.6000 deg. Period: 94.60 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1971 October 17 - . 13:36 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1W. LV Family: Delta. Launch Vehicle: Thorad Agena D SLV-2G. LV Configuration: Thorad SLV-2G Agena D 570.
  • ASTEX - . Payload: P71-2 / Agena D. Mass: 1,500 kg (3,300 lb). Nation: USA. Agency: USAF STP. Class: Technology. Type: Navigation technology satellite. Spacecraft: ASTEX. USAF Sat Cat: 5560 . COSPAR: 1971-089A. Apogee: 761 km (472 mi). Perigee: 738 km (458 mi). Inclination: 92.7000 deg. Period: 99.80 min. Summary: Space Test Program; technology experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1976 May 22 - . 07:42 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout B-1. LV Configuration: Scout B-1 S179CR.
  • P 76-5 - . Mass: 73 kg (160 lb). Nation: USA. Agency: USAF STP. Class: Technology. Type: Communications technology satellite. Spacecraft: P 76. USAF Sat Cat: 8860 . COSPAR: 1976-047A. Apogee: 1,044 km (648 mi). Perigee: 981 km (609 mi). Inclination: 99.6000 deg. Period: 105.40 min. Summary: Communications propagation experiments..

1983 June 27 - . 15:37 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout D-1. LV Configuration: Scout D-1 S205C.
  • HILAT - . Payload: Transit O-16 / P83-1. Nation: USA. Agency: USAF STP. Class: Communications. Type: Military communications satellite. Spacecraft: Transit. USAF Sat Cat: 14154 . COSPAR: 1983-063A. Apogee: 818 km (508 mi). Perigee: 754 km (468 mi). Inclination: 82.0000 deg. Period: 100.60 min. Summary: Modification of Transit O-16 for military communications research. Officially: Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..

1986 November 14 - . 00:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout G. LV Configuration: Scout G-1 S199C.
  • Polar Bear - . Payload: Transit O-16 / P 87-1. Mass: 125 kg (275 lb). Nation: USA. Agency: USAF STP. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Transit. USAF Sat Cat: 17070 . COSPAR: 1986-088A. Apogee: 1,013 km (629 mi). Perigee: 955 km (593 mi). Inclination: 89.6000 deg. Period: 104.80 min. Tranist O-17 had been turned over to the National Air and Space Museum in 1976 and was displayed to the public for more than 8 years. In 1984, it was refurbished at APL and launched as the Polar Beacon Experiment and Auroral Research satellite to collect data for studying communications over the Earth’s polar regions.

1993 April 25 - . 13:56 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: NB-52 008. LV Family: Pegasus. Launch Vehicle: Pegasus. LV Configuration: Pegasus 004/F4.
  • Alexis - . Payload: Alexis (P 89-1B). Mass: 115 kg (253 lb). Nation: USA. Agency: USAF STP. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Alexis. USAF Sat Cat: 22638 . COSPAR: 1993-026A. Apogee: 746 km (463 mi). Perigee: 741 km (460 mi). Inclination: 69.8000 deg. Period: 99.70 min. Summary: Test of X-ray imaging sensors; solar array deployment malfunction. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..

1994 May 19 - . 17:03 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: NB-52 008. LV Family: Pegasus. Launch Vehicle: Pegasus/HAPS. LV Configuration: Pegasus/HAPS 005/F5.
  • STEP 2 (SIDEX) - . Payload: STEP M2 / P 91-A. Mass: 180 kg (390 lb). Nation: USA. Agency: USAF STP. Program: STEP. Class: Military. Type: Strategic defense satellite. Spacecraft: Eagle. USAF Sat Cat: 23105 . COSPAR: 1994-029A. Apogee: 813 km (505 mi). Perigee: 597 km (370 mi). Inclination: 82.0000 deg. Period: 98.90 min. Summary: Did not achieve planned orbit, though still useful. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1994 August 3 - . 14:38 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: NB-52 008. LV Family: Pegasus. Launch Vehicle: Pegasus. LV Configuration: Pegasus F7.
  • P90-6 APEX - . Payload: APEX/Orion 38. Mass: 260 kg (570 lb). Nation: USA. Agency: USAF STP. Class: Technology. Type: Navigation technology satellite. Spacecraft: APEX. USAF Sat Cat: 23191 . COSPAR: 1994-046A. Apogee: 2,534 km (1,574 mi). Perigee: 360 km (220 mi). Inclination: 69.9800 deg. Period: 114.82 min. Summary: Advanced Photovoltaic and Electronic Experiments; studied radiation and plasma effects on solar power systems..

1996 March 9 - . 01:53 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F10.
  • REX-II - . Nation: USA. Agency: USAF STP. Class: Earth. Type: Ionosphere satellite. Spacecraft: REX. USAF Sat Cat: 23814 . COSPAR: 1996-014A. Apogee: 835 km (518 mi). Perigee: 799 km (496 mi). Inclination: 90.0000 deg. Period: 101.20 min. Summary: LEO .

1997 August 29 - . 15:02 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL 019/F17.
  • FORTE - . Nation: USA. Agency: USAF STP. Manufacturer: Los Alamos. Class: Technology. Type: Navigation technology satellite. Spacecraft: FORTE. USAF Sat Cat: 24920 . COSPAR: 1997-047A. Apogee: 833 km (517 mi). Perigee: 799 km (496 mi). Inclination: 70.0000 deg. Period: 101.20 min. FORTE - 'Fast On-orbit Recording of Transient Events' - was a US Los Alamos National Laboratory satellite designed to study natural and artificial radio emissions from the ionosphere. This data was needed to develop technology for monitoring nuclear test ban treaties.

1997 October 22 - . 13:13 GMT - . Launch Site: Wallops Island DZ. Launch Pad: 37.0 N x 72.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F18.
  • STEP-4 - . Payload: STEP M4. Nation: USA. Agency: USAF STP. Program: STEP. Class: Military. Type: Strategic defense satellite. Spacecraft: Eagle. Decay Date: 2001-03-31 . USAF Sat Cat: 25013 . COSPAR: 1997-063A. Apogee: 500 km (310 mi). Perigee: 432 km (268 mi). Inclination: 45.0000 deg. Period: 93.80 min.

2000 June 7 - . 13:19 GMT - . Launch Site: Point Arguello WADZ. Launch Pad: 36.0 N x 123.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F29.
  • TSX 5 - . Payload: P95-2. Mass: 247 kg (544 lb). Nation: USA. Agency: USAF STP. Manufacturer: McLean. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: STEP. USAF Sat Cat: 26374 . COSPAR: 2000-030A. Apogee: 1,695 km (1,053 mi). Perigee: 412 km (256 mi). Inclination: 68.9379 deg. Period: 106.19 min. Military Technology satellite. Launch delayed from May 20 and June 6. Fifth STEP (Space Test Experiments Program) satellite. The satellite's main section was the STRV-2 experiment module, sponsored by the Ballistic Missile Defense Organization and the UK Ministry of Defense. This was to take infrared images of UK military aircraft at perigee, and then downlink data via laser. STRV-2 also carried vibration isolation and debris impact sensors. A secondary payload was the S97-1 CEASE (Compact Environmental Anomaly Sensor). This was an AFRL prototype sensor package to provide warning of spacecraft charging and radiation events.

2000 July 19 - . 20:09 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC8. LV Family: Minotaur. Launch Vehicle: Minotaur 1. LV Configuration: Minotaur 1 2.
  • Mightysat 2.1 - . Payload: SA-200B. Mass: 120 kg (260 lb). Nation: USA. Agency: USAF STP. Manufacturer: Gilbert. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: SA-200. Decay Date: 2002-11-12 . USAF Sat Cat: 26414 . COSPAR: 2000-042A. Apogee: 581 km (361 mi). Perigee: 547 km (340 mi). Inclination: 97.7835 deg. Period: 95.86 min. Mightysat 2.1, also known as Sindri, used a Spectrum Astro SA-200B satellite bus. The spacecraft carried a hyperspectral imager for earth imaging and spectroscopy, as well as satellite technology experiments such as advanced solar arrays. An Aerospace Corp./DARPA picosatellite experiment, consisting of two small boxes connected by a deployable tether, was deployed later. Similar picosats were deployed on the previous Minotaur launch in January 2000.

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