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GGTS
GGTS 1
GGTS 1
Credit: Manufacturer Image
American gravity gradient technology satellite. Gravity gradient stabilization tests.

Status: Operational 1966. First Launch: 1966-06-16. Last Launch: 1966-06-16. Number: 1 . Gross mass: 47 kg (103 lb).



Subtopics

GGTS 1, 2 Technology, gravity gradient stabilization satellite operated by USAF, USA. Launched 1966.

Family: Geosynchronous orbit, Gravity gradient technology satellite, Technology. Country: USA. Launch Vehicles: Titan, Titan IIIC. Launch Sites: Cape Canaveral, Cape Canaveral LC41. Agency: USAF. Bibliography: 2, 279, 6.

1966 June 16 - . 14:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. LV Family: Titan. Launch Vehicle: Titan IIIC.
  • GGTS 1 - . Mass: 47 kg (103 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Gravity gradient technology satellite. Spacecraft: GGTS. USAF Sat Cat: 2207 . COSPAR: 1966-053A. Apogee: 33,858 km (21,038 mi). Perigee: 33,663 km (20,917 mi). Inclination: 4.2000 deg. Period: 1,334.00 min. Gravity gradient stabilization tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .


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