NATO 3 (original) (raw)

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NATO 3

NATO 3A
Credit: Manufacturer Image

British military communications satellite. Military communications. Military communication satellite built by Philco Ford Space & Reentry Systems Division for NATO, International. Launched 1976 - 1984. Used NATO-3 Bus.

Status: Operational 1976. First Launch: 1976-04-22. Last Launch: 1984-11-14. Number: 4 . Gross mass: 720 kg (1,580 lb).

More at: NATO 3.

Family: Communications, Geosynchronous orbit, Military communications sat. Country: UK. Engines: Star 27B. Launch Vehicles: Thor, Delta, Delta 2914, Delta 3914, Delta 2000, Delta 3000. Launch Sites: Cape Canaveral, Cape Canaveral LC17B, Cape Canaveral LC17A. Agency: NATO. Bibliography: 2, 279, 6, 12872.

1973 March 5 - .

NATO III satellite contract - . Spacecraft Bus: NATO. Spacecraft: NATO 3. The Air Force announced that a $27.6 million contract had been awarded to Philco-Ford Corporation for development of the NATO III satellite communications system. SAMSO provided the program management.

1976 April 22 - . 20:46 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 2914.

NATO 3A - . Mass: 310 kg (680 lb). Nation: NATO. Agency: NATO. Program: NATO. Class: Communications. Type: Military communications satellite. Spacecraft: NATO 3. Completed Operations Date: 1992-12-17 . USAF Sat Cat: 8808 . COSPAR: 1976-035A. Apogee: 36,017 km (22,379 mi). Perigee: 35,801 km (22,245 mi). Inclination: 13.30 deg. Period: 1,442.40 min.
A Thor/Delta carrying the NATO IIIA satellite was successfully launched from LC-17B, Eastern Test Range. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Atlantic Ocean at 18 deg W in 1976-1982; over the Atlantic Ocean 30 deg W in 1982-1984; over the Atlantic Ocean 50 deg W in 1984-1985; over the Atlantic Ocean at 30 deg W in 1985-1989; over the Americas at 125 deg W in 1989-1991 As of 5 September 2001 located at 4.12 deg E drifting at 1.524 deg W per day. As of 2007 Mar 9 located at 142.00E drifting at 1.522W degrees per day.

1976 July 26 - .

The NATO IIIA satellite became fully operational. 30 July. - . Spacecraft: NATO 3.

1976 September 17 - .

Defense Communications Agency use of NATO IIIB spacecraft - . Spacecraft: NATO 3, DSCS II. A U.S./NATO memorandum of agreement was signed which allowed the Defense Communications Agency the use of the NATO IIIB spacecraft until December 1977. This would supplement the DSCS II satellite coverage..

1977 January 28 - . 00:49 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 2914.

NATO 3B - . Mass: 701 kg (1,545 lb). Nation: NATO. Agency: NATO. Program: NATO. Class: Communications. Type: Military communications satellite. Spacecraft: NATO 3. Completed Operations Date: 1993-07-29 . USAF Sat Cat: 9785 . COSPAR: 1977-005A. Apogee: 37,421 km (23,252 mi). Perigee: 37,079 km (23,039 mi). Inclination: 10.50 deg. Period: 1,511.50 min.
A Delta booster launched the NATO III-B communications satellite into orbit from Cape Canaveral, Florida. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Pacific Ocean at 135 deg W in 1977-1979 over the Atlantic Ocean 20 deg W in 1979-1982 over the Atlantic Ocean 18 deg W in 1983-1986 over the Atlantic Ocean60 deg W in 1987-1993 As of 5 September 2001 located at 74.61 deg W drifting at 18.018 deg W per day. As of 2007 Mar 10 located at 40.43E drifting at 18.015W degrees per day.

1978 November 19 - . 00:46 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 2914.

NATO 3C - . Mass: 720 kg (1,580 lb). Nation: NATO. Agency: NATO. Program: NATO. Class: Communications. Type: Military communications satellite. Spacecraft: NATO 3. Completed Operations Date: 1992-06-15 . USAF Sat Cat: 11115 . COSPAR: 1978-106A. Apogee: 36,299 km (22,555 mi). Perigee: 36,289 km (22,548 mi). Inclination: 11.80 deg. Period: 1,462.10 min.
A Delta 2914 booster was launched from Cape Canaveral carrying the NATO IIIC satellite. The launch was successful, and the satellite performed satisfactorily in orbit. Positioned in geosynchronous orbit over the Atlantic Ocean at 50 deg W in 1979-1982 over the Atlantic Ocean 21 deg W in 1983-1986 over the Atlantic Ocean 18 deg W in 1987-1991 over the Atlantic Ocean21 deg W in 1991-1992 As of 31 August 2001 located at 122.29 deg E drifting at 6.431 deg W per day. As of 2007 Mar 10 located at 114.22E drifting at 6.438W degrees per day.

1979 July 31 - .

NATO III program completed. - . Spacecraft Bus: NATO. Spacecraft: NATO 3. SAMSO's NATO III Program Office was abolished, bringing the NATO III program to an end. Three satellites had been built and launched during the program, which had cost a total of $79.1 million..

1984 November 14 - . 00:34 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 3914.

NATO 3D - . Mass: 320 kg (700 lb). Nation: NATO. Agency: NATO. Program: NATO. Class: Communications. Type: Military communications satellite. Spacecraft: NATO 3. USAF Sat Cat: 15391 . COSPAR: 1984-115A. Apogee: 35,796 km (22,242 mi). Perigee: 35,779 km (22,231 mi). Inclination: 2.20 deg. Period: 1,436.20 min.
Stationed at 138 deg W. Positioned in geosynchronous orbit at 30 deg W in 1985; 50 deg W in 1985-1986; 21 deg W in 1986-1991; 30 deg W in 1991-1993; 21 deg W in1993-1997; 18 deg W in 1997-1999 As of 31 August 2001 located at 19.33 deg W drifting at 0.021 deg W per day. As of 2007 Mar 10 located at 120.20W drifting at 19.149W degrees per day.

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