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SDIO

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z SDIO American agency overseeing development of spacecraft. Strategic Defense Initiative Organization (renamed the BMDO), USA. AKA: Strategic Defense Initiative Organization, DoD. Location: Washington, DC-Pentagon. Country: USA. Spacecraft: LACE, RME. 1985 July 14 - . 15:05 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands KP. LV Family: Malemute. Launch Vehicle: Terrier Malemute. ACE I Target - . Nation: USA. Agency: Lincoln, SDIO. Type: ABM Target. Apogee: 497 km (308 mi). 1985 September 27 - . 15:20 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands KP. LV Family: Malemute. Launch Vehicle: Terrier Malemute. ACE II Target - . Nation: USA. Agency: Lincoln, SDIO. Type: ABM Target. Apogee: 497 km (308 mi). 1985 October 10 - . 15:25 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands KP. LV Family: Malemute. Launch Vehicle: Terrier Malemute. ACE III Target - . Nation: USA. Agency: Lincoln, SDIO. Type: ABM Target. Apogee: 479 km (297 mi). 1985 December 10 - . 15:50 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands KP. LV Family: Malemute. Launch Vehicle: Terrier Malemute. ACE IV Target - . Nation: USA. Agency: Lincoln, SDIO. Type: ABM Target. Apogee: 486 km (301 mi). 1986 September 5 - . 15:08 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 3920. USA 19 - . Payload: Delta 180 / Payload Adapter System. Mass: 6,000 kg (13,200 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: SDI. Decay Date: 1986-09-28 . USAF Sat Cat: 16937 . COSPAR: 1986-069A. Apogee: 748 km (464 mi). Perigee: 213 km (132 mi). Inclination: 39.10 deg. Period: 94.20 min. SDIO sensor tests. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). . Delta 180 Sensor Module - . Payload: DM 43 Sensor Module. Mass: 6,000 kg (13,200 lb). Nation: USA. Agency: SDIO. Spacecraft: SDI. Decay Date: 1986-11-25 . USAF Sat Cat: 16938 . COSPAR: 1986-069B. Apogee: 539 km (334 mi). Perigee: 215 km (133 mi). Inclination: 22.70 deg. Period: 92.09 min. 1986 September 5 - . 16:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Minuteman. Launch Vehicle: Aries. Delta 180 Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 300 km (180 mi). 1987 - . Launch Site: Barking Sands. Launch Complex: Barking Sands LC1. Launch Pad: LC1?. LV Family: Strypi. Launch Vehicle: Strypi XI. Nation: USA. Agency: SDIO. Apogee: 200 km (120 mi). 1987 July 27 - . Launch Site: Eareckson. LV Family: Minuteman. Launch Vehicle: Aries. ABM infrared sensor technology mission - . Nation: USA. Agency: SDIO. Apogee: 300 km (180 mi). 1987 August 24 - . 03:52 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral ETR. Launch Platform: SSBN 629. LV Family: Trident. Launch Vehicle: Trident C-4. JANUS Demonstration and shakedown operations launch - . Nation: USA. Agency: SDIO. Apogee: 1,000 km (600 mi). 1987 December 14 - . 01:45 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA2. LV Family: Black Brant. Launch Vehicle: Black Brant X. SPEAR I Active plasma mission - . Nation: USA. Agency: SDIO. Apogee: 370 km (220 mi). 1988 February 8 - . 22:08 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 3910. USA 30 - . Payload: Delta 181 Canister Cluster. Mass: 6,000 kg (13,200 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: SDI. Decay Date: 1988-03-01 . USAF Sat Cat: 18847 . COSPAR: 1988-008A. Apogee: 342 km (212 mi). Perigee: 225 km (139 mi). Inclination: 28.60 deg. Period: 90.20 min. Military tracking exercise; released subsatellites. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). . Delta 181 Sensor Module - . Payload: Thrusted Vector Sensor Mo. Mass: 6,000 kg (13,200 lb). Nation: USA. Agency: SDIO. Spacecraft: SDI. Decay Date: 1988-04-02 . USAF Sat Cat: 18848 . COSPAR: 1988-008B. Apogee: 314 km (195 mi). Perigee: 287 km (178 mi). Inclination: 30.70 deg. Period: 90.53 min. 1988 February 9 - . Launch Site: Barking Sands. Launch Complex: Barking Sands LC1. Launch Pad: LC1?. LV Family: Strypi. Launch Vehicle: Strypi XI. Reentry test - . Nation: USA. Agency: SDIO. Apogee: 200 km (120 mi). 1988 August 1 - . Launch Site: Eareckson. LV Family: Minuteman. Launch Vehicle: Aries. Recovery failed ABM infrared sensor technology mission - . Nation: USA. Agency: SDIO. Apogee: 300 km (180 mi). 1989 January 1 - . Launch Site: Barking Sands. Launch Complex: Barking Sands LC1. Launch Pad: LC1?. LV Family: Strypi. Launch Vehicle: Strypi XI. THORNY MERIT Reentry test - . Nation: USA. Agency: SDIO. Apogee: 200 km (120 mi). 1989 February 4 - . 03:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral ETR. Launch Platform: SSBN 643. LV Family: Trident. Launch Vehicle: Trident C-4. DASO-32 technology mission / demonstration and shakedown operations launch - . Nation: USA. Agency: SDIO. Apogee: 1,000 km (600 mi). 1989 March 24 - . 21:50 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 3920-8. USA 36 - . Payload: Delta Star. Mass: 6,000 kg (13,200 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: SDI. Decay Date: 1992-06-23 . USAF Sat Cat: 19911 . COSPAR: 1989-026A. Apogee: 312 km (193 mi). Perigee: 307 km (190 mi). Inclination: 47.70 deg. Period: 90.70 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). . 1989 July 1 - . Launch Site: Eareckson. LV Family: Minuteman. Launch Vehicle: Aries. ABM infrared sensor technology mission - . Nation: USA. Agency: SDIO. Apogee: 300 km (180 mi). 1989 July 13 - . 08:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Minuteman. Launch Vehicle: Aries. BEAR Active plasma mission - . Nation: USA. Agency: SDIO. Apogee: 195 km (121 mi). The Beam Experiment Aboard Rocket (BEAR) payload was recovered with minimal damage via parachute after an 11-minute flight to a maximum altitude of 195 km. The neutral partical beam experiment was provided by Los Alamos National Laboratory. The Attitude Control System spun-up the payload at various rates and orientations with respect to the earths magnetic field after separation from the booster. After re-entry, at 5,000 m, the nose was jettisoned and the recovery parachute system deployed. The payload impacted the ground at less than 30 feet per second. The BEAR mission was declared a total success by SDIO. 1989 July 24 - . 08:39 GMT - . Launch Site: Poker Flat. LV Family: Black Brant. Launch Vehicle: Black Brant 8C. CHEER / Black Star 1 Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 340 km (210 mi). 1989 July 31 - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant X. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 900 km (550 mi). 1989 July 31 - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant X. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 900 km (550 mi). 1989 July 31 - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant VC. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 250 km (150 mi). 1989 August 13 - . 09:00 GMT - . Launch Site: Poker Flat. LV Family: Black Brant. Launch Vehicle: Black Brant 8C. CHEER / Black Star 2 Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 340 km (210 mi). 1989 September 4 - . Launch Site: Barking Sands. LV Family: Malemute. Launch Vehicle: Terrier Malemute. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 724 km (449 mi). 1989 September 11 - . Launch Site: Barking Sands. LV Family: Malemute. Launch Vehicle: Terrier Malemute. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 724 km (449 mi). 1989 September 15 - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant VC. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 250 km (150 mi). 1990 January 26 - . Launch Site: White Sands. Launch Complex: White Sands LC37. LV Family: Sprint ABM. Launch Vehicle: HEDI. KITE-1 test - . Nation: USA. Agency: SDIO. Apogee: 10 km (6 mi). 1990 February 14 - . 16:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 6920-8. USA 51 - . Payload: LACE. Mass: 1,430 kg (3,150 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: LACE. Decay Date: 2000-05-24 . USAF Sat Cat: 20496 . COSPAR: 1990-015A. Apogee: 480 km (290 mi). Perigee: 463 km (287 mi). Inclination: 43.10 deg. Period: 94.00 min. Low-power Atmospheric Compensation Experiment for SDIO. Research and exploration of the upper atmosphere and outer space. The McDonnell Douglas Corporation has provided the following information for its launch of the Losat spacecraft on 14 Feb 1990: LACE spacecraft (Losat-L), launch time 1615:00.626 GMT, ETR Launch Complex 17. Programmed orbital parameters 95.6 min, apogee 551 km, inc. 43.1 deg. Evaluate laser beam distortion in space. USA 52 - . Payload: RME. Mass: 1,040 kg (2,290 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: RME. Decay Date: 1992-05-24 . USAF Sat Cat: 20497 . COSPAR: 1990-015B. Apogee: 281 km (174 mi). Perigee: 261 km (162 mi). Inclination: 43.10 deg. Period: 89.90 min. Relay Mirror Experiment; also known as Losat-R. RME validated stabilization, tracking, and pointing technologies for Strategic Defense Initiative (SDI) missions through a credible demonstration of a space-based relay mirror system. The Wideband Angular Vibration Experiment (WAVE) measured low-level angular vibrations affecting performance of acquisition, tracking, and pointing systems. The experiment demonstrated that a laser beam can be accurately relayed from the earth to an orbiting satellite 450 kilometers away and then back to a 3-meter target on the ground. It achieved relay beam pointing accuracy which was 16 times better than the technical requirement. WAVE demonstrated the capability to discern platform disturbance amplitudes of a few nanoradians at discrete frequencies and is therefore a candidate to fulfill similar requirements for future ATP experiments. 1990 March 29 - . Launch Site: Wallops Island. LV Family: Malemute. Launch Vehicle: Terrier Malemute. Firefly 1 Target - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 462 km (287 mi). 1990 April 25 - . 05:32 GMT - . Launch Site: Wallops Island. LV Family: Malemute. Launch Vehicle: Terrier Malemute. Bow Shock 1 re-entry vehicle test flight - . Nation: USA. Agency: SDIO. Apogee: 721 km (448 mi). 1990 April 27 - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Minuteman. Launch Vehicle: Aries. EXCEDE-3 Active plasma mission - . Nation: USA. Agency: SDIO. Apogee: 116 km (72 mi). 1990 July 26 - . 05:51 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Minuteman. Launch Vehicle: Aries. FAILURE: Failure. Technology mission - . Nation: USA. Agency: SDIO. Apogee: 2.00 km (1.20 mi). 1990 August 25 - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant 10CM1. SPFE 1 (LACE Target) Technology test - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 200 km (120 mi). 1990 October 20 - . Launch Site: Wallops Island. LV Family: Malemute. Launch Vehicle: Terrier Malemute. Firefly 2 Target - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 456 km (283 mi). 1991 February 18 - . 14:30 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands LC1. LV Family: Strypi. Launch Vehicle: Strypi XI. Bow Shock 2 re-entry vehicle test flight - . Nation: USA. Agency: SDIO. Apogee: 120 km (70 mi). 1991 April 17 - . 07:46 GMT - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant 10CM1. SPFE 2 (LACE Target) Technology test - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 300 km (180 mi). 1991 April 28 - . 11:33 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP2. LV Family: Shuttle. Launch Vehicle: Space Shuttle. CRO-C - . Payload: Discovery F12 / IBSS-SPAS 02 / CRO A / CRO B / CRO. Mass: 197 kg (434 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: CRO. Decay Date: 1991-05-14 . USAF Sat Cat: 21245 . COSPAR: 1991-031D. Apogee: 85 km (52 mi). Perigee: 67 km (41 mi). Inclination: 56.90 deg. Period: 85.70 min. Chemical Release Observation; deployed 2 May 1991; released gases for observation by IBSS.. IBSS - . Payload: SPAS-2. Mass: 1,901 kg (4,190 lb). Nation: USA. Agency: SDIO. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: IBSS. Decay Date: 1991-05-06 . USAF Sat Cat: 21244 . COSPAR: 1991-031B. Apogee: 255 km (158 mi). Perigee: 245 km (152 mi). Inclination: 57.00 deg. Period: 89.50 min. Infrared Background Signature Survey; sensor technology test; retrieved 2 May 1991.. CRO-A - . Payload: Discovery F12 / IBSS-SPAS 02 / CRO A / CRO B / CRO. Mass: 197 kg (434 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: CRO. Decay Date: 1991-05-13 . USAF Sat Cat: 21247 . COSPAR: 1991-031F. Apogee: 236 km (146 mi). Perigee: 215 km (133 mi). Inclination: 57.00 deg. Period: 89.00 min. Chemical Release Observation; deployed 3 May 1991; released gases for observation by IBSS.. CRO-B - . Payload: Discovery F12 / IBSS-SPAS 02 / CRO A / CRO B / CRO. Mass: 197 kg (434 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: CRO. Decay Date: 1991-05-12 . USAF Sat Cat: 21246 . COSPAR: 1991-031E. Apogee: 88 km (54 mi). Perigee: 68 km (42 mi). Inclination: 56.90 deg. Period: 85.80 min. Chemical Release Observation; deployed 2 May 1991; released gases for observation by IBSS.. 1991 July 4 - . 02:32 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 7925. Losat X - . Mass: 75 kg (165 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: Losat. Decay Date: 1991-11-15 . USAF Sat Cat: 21553 . COSPAR: 1991-047B. Apogee: 417 km (259 mi). Perigee: 405 km (251 mi). Inclination: 40.00 deg. Period: 92.80 min. Test flight of DOD sensors; Low Altitude Satellite Experiment. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).. 1991 August 20 - . 09:45 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Minuteman. Launch Vehicle: Aries. FAILURE: Failure. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 2.00 km (1.20 mi). 1991 September 23 - . 15:40 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC37. LV Family: Sprint ABM. Launch Vehicle: HEDI. FAILURE: Failure. KITE-2 test - . Nation: USA. Agency: SDIO. Apogee: 0 km (0 mi). 1991 October 14 - . 10:17 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Minuteman. Launch Vehicle: Aries. Target - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 320 km (190 mi). LEAP-1. Missile Tracking and Discrimination for SDIO.. 1992 February 18 - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Minuteman. Launch Vehicle: Aries. Technology mission - . Nation: USA. Agency: SDIO. Apogee: 320 km (190 mi). 1992 May 24 - . Launch Site: Barking Sands. LV Family: Malemute. Launch Vehicle: Terrier Malemute. CDX (LWIS) Target - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 290 km (180 mi). 1992 June 19 - . 11:01 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Minuteman. Launch Vehicle: Aries. Technology test - . Nation: USA. Agency: SDIO. Apogee: 330 km (200 mi). LEAP-2. Missile Tracking and Discrimination for SDIO.. 1992 August 26 - . 14:31 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC37. LV Family: Sprint ABM. Launch Vehicle: HEDI. KITE-2A test - . Nation: USA. Agency: SDIO. Apogee: 12 km (7 mi). 1992 October 22 - . Launch Site: Wallops Island. LV Family: Minuteman. Launch Vehicle: Aries. FAILURE: Failure.. SPFE-3 / Orbus 1 Target - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 20 km (12 mi). LEAP-3. Missile Tracking and Discrimination for SDIO.. 1993 March 16 - . 02:12 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA2. LV Family: Black Brant. Launch Vehicle: Black Brant 9CM1. SPEAR 3 Active plasma mission - . Nation: USA. Agency: SDIO. Apogee: 290 km (180 mi). 1993 May 23 - . 09:17 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Talos. Launch Vehicle: Space Data LCLV. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 378 km (234 mi). 1993 May 28 - . 08:34 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Talos. Launch Vehicle: Space Data LCLV. Target mission - . Nation: USA. Agency: SDIO. Type: ABM Target. Apogee: 390 km (240 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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