MSTI (original) (raw)
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MSTI
MSTI-3
Credit: Manufacturer Image
American military strategic defense satellite. BMDO technology demonstration; Miniature Seeker Technology Demonstration. Research satellite built by Spectrum Astro for SDIO, USA. Launched 1992. Used the SA-200S bus.
Status: Operational 1992. First Launch: 1992-11-21. Last Launch: 1996-05-17. Number: 3 . Gross mass: 170 kg (370 lb).
More at: MSTI.
Family: Military, Military strategic defense sat. Country: USA. Launch Vehicles: Scout, Scout G-1, Pegasus, Pegasus H. Launch Sites: Vandenberg, Vandenberg SLC5, Point Arguello WADZ. Agency: USAF. Bibliography: 2, 276, 279, 6, 12859, 12860, 12861.
Photo Gallery
MSTICredit: Manufacturer Image |
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MSTI-2Credit: Manufacturer Image |
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1992 November 21 - . 13:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout G-1.
- MSTI - . Payload: MSTI 1. Mass: 180 kg (390 lb). Nation: USA. Class: Military. Type: Strategic defense satellite. Spacecraft Bus: SA-200. Spacecraft: MSTI. Decay Date: 1993-07-18 . USAF Sat Cat: 22229 . COSPAR: 1992-078A. Apogee: 366 km (227 mi). Perigee: 289 km (179 mi). Inclination: 96.70 deg. Period: 91.10 min. BMDO technology demonstration; Miniature Seeker Technology Demonstration. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .
1994 May 9 - . 02:47 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout G-1.
- MSTI-2 - . Payload: MSTI 2. Mass: 163 kg (359 lb). Nation: USA. Class: Military. Type: Strategic defense satellite. Spacecraft Bus: SA-200. Spacecraft: MSTI. Decay Date: 1998-11-28 . USAF Sat Cat: 23101 . COSPAR: 1994-028A. Apogee: 433 km (269 mi). Perigee: 415 km (257 mi). Inclination: 93.10 deg. Period: 97.10 min. Last Scout launch; BMDO technology tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1996 May 17 - . 02:44 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Vandenberg.. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus H.
- MSTI-3 - . Payload: MSTI 3. Mass: 170 kg (370 lb). Nation: USA. Agency: BMDO. Class: Military. Type: Strategic defense satellite. Spacecraft Bus: SA-200. Spacecraft: MSTI. Decay Date: 1997-12-11 . USAF Sat Cat: 23868 . COSPAR: 1996-031A. Apogee: 432 km (268 mi). Perigee: 420 km (260 mi). Inclination: 97.10 deg. Period: 90.70 min. LEO. Sensor technology tests Air dropped in Point Arguello WADZ..
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