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SESP

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SESP 1 Credit: Manufacturer Image

Status: Operational 1971. First Launch: 1971-06-08. Last Launch: 1976-07-08. Number: 3 . Gross mass: 260 kg (570 lb).

Family: Military technology sat, Technology. Country: USA. Launch Vehicles: Titan, Thor, Delta, Thor Burner 2, Titan IIID, Thor Burner. Launch Sites: Vandenberg, Vandenberg SLC10W, Vandenberg SLC4E. Agency: USAF. More at: 13084. Bibliography: 2, 279, 6.

• 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 Bus: SESP. 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. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

• SESP 73-5 - . Payload: P 73 5 / OPS 8452. Mass: 260 kg (570 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Military technology satellite. Spacecraft Bus: SESP. Spacecraft: SESP. Decay Date: 1975-05-26 . USAF Sat Cat: 7499 . COSPAR: 1974-085C. Apogee: 2,888 km (1,794 mi). Perigee: 150 km (90 mi). Inclination: 96.9000 deg. Period: 116.30 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

• SESP 74-2 - . Payload: P 74-2 / OPS 3986. Mass: 260 kg (570 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Military technology satellite. Spacecraft Bus: SESP. Spacecraft: SESP. Decay Date: 1986-04-24 . USAF Sat Cat: 9007 . COSPAR: 1976-065B. Apogee: 8,048 km (5,000 mi). Perigee: 236 km (146 mi). Inclination: 97.5000 deg. Period: 179.00 min. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .