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Singleton

Spacecraft · USA

Original archive entry. The text, images and links below are kept as they were written.

American signals intelligence satellite; possibly some kind of imaging also done. On-board propulsion boosts spacecraft to 800 km operating orbit.

Family
SIGINT
Country
USA
Launch Vehicles
Titan, Titan II, Titan II SLV
Agency
USAF
Bibliography
172, 2, 278, 6, 6877, 13092

Chronology

3 events

1988 September 5

09:25 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan II SLV.
  • USA 32 - . Payload: SBWASS R1. Mass: 1,700 kg (3,700 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: SIGINT. Spacecraft: Singleton. USAF Sat Cat: 19460 . COSPAR: 1988-078A. Apogee: 292 km (181 mi). Perigee: 185 km (114 mi). Inclination: 85.00 deg. Period: 89.30 min. New class of signals intelligence satellite; possibly some kind of imaging also done. On-board propulsion boosts spacecraft to 800 km operating orbit. First Titan 2 standard launch vehicle launch..

1989 September 6

01:49 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan II SLV.
  • USA 45 - . Payload: SBWASS R2. Mass: 1,700 kg (3,700 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: SIGINT. Spacecraft: Singleton. USAF Sat Cat: 20220 . COSPAR: 1989-072A. Signals intelligence. Reentered from initial parking orbit of 200 km after failure of on-board boost motor..

1992 April 25

08:53 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan II SLV.
  • USA 81 - . Payload: SBWASS R3. Mass: 1,700 kg (3,700 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: SIGINT. Spacecraft: Singleton. USAF Sat Cat: 21949 . COSPAR: 1992-023A. Apogee: 175 km (108 mi). Perigee: 145 km (90 mi). Inclination: 84.90 deg. Period: 89.30 min. Signals intelligence satellite; possibly some kind of imaging also done. On-board propulsion boosts spacecraft to 800 km operating orbit..