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Program: Tiros. Objective: Earth. Type: Weather. TIROS spacecraft were the beginning of a long series of polar-orbiting meteorological satellites. TIROS was followed by the TOS (TIROS Operational System) series, and then the ITOS (Improved TIROS) series, and later the NOAA series. TIROS spacecraft were developed by GSFC and managed by ESSA (Environmental Science Services Administration). The objective was to establish a global weather satellite system.
Major Events:

  • 1960 April 1 - Tiros 1.  Spacecraft: Tiros. Mass: 120 kg (260 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    TV and Infrared Observation Satellite; returned 22952 cloud cover photos. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1960 November 23 - Tiros 2.  Spacecraft: Tiros. Mass: 130 kg (280 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1961 July 12 - Tiros 3.  Spacecraft: Tiros. Mass: 129 kg (284 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1961 September 28 - Tiros 2 rocket test.. 

    Pair of spinup rockets on Tiros II successfully fired after more than 10 months in orbit.

  • 1962 February 8 - Tiros 4.  Spacecraft: Tiros. Mass: 129 kg (284 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Returned 32593 cloud cover photos. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1962 June 19 - Tiros 5.  Spacecraft: Tiros. Mass: 129 kg (284 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Returned 58226 cloud cover images. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1962 September 18 - Tiros 6.  Spacecraft: Tiros. Mass: 127 kg (279 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Returned 66674 cloud cover images. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1963 June 19 - Tiros 7.  Spacecraft: Tiros. Mass: 135 kg (297 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Returned over 150000 cloud cover images. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1963 December 21 - Tiros 8.  Spacecraft: Tiros. Mass: 119 kg (262 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Returned more than 100,000 cloud cover images. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1965 January 22 - Tiros 9.  Spacecraft: Tiros. Mass: 138 kg (304 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1965 July 2 - Tiros 10.  Spacecraft: Tiros. Mass: 127 kg (279 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1966 February 3 - ESSA 1.  Spacecraft: Tiros. Mass: 138 kg (304 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Environmental Survey Satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1966 February 28 - ESSA 2.  Spacecraft: Tiros. Mass: 132 kg (291 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Environmental Survey Satellite; carried APT cameras. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1966 October 2 - ESSA 3.  Spacecraft: TOS. Mass: 145 kg (319 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Environmental Survey Satellite 3; replace ESSA 1. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1967 January 26 - ESSA 4.  Spacecraft: TOS. Mass: 132 kg (291 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Replaced ESSA 2. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1967 April 20 - ESSA 5.  Spacecraft: TOS. Mass: 145 kg (319 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Replaced ESSA 3. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1967 November 10 - ESSA 6.  Spacecraft: TOS. Mass: 132 kg (291 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Returned cloud cover images. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1968 August 16 - ESSA 7.  Spacecraft: TOS. Mass: 145 kg (319 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1968 December 15 - ESSA 8.  Spacecraft: TOS. Mass: 132 kg (291 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1969 February 26 - ESSA 9.  Spacecraft: TOS. Mass: 145 kg (319 lb). Launch Site: Cape Canaveral. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1970 January 23 - ITOS 1.  Spacecraft: ITOS. Mass: 309 kg (681 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Improved TIROS Operational Satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1970 December 11 - NOAA 1.  Spacecraft: ITOS. Mass: 306 kg (674 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Built for NASA; operated by NOAA. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1970 December 11 - CEPE.  Launch Site: Vandenberg. Launch Vehicle: Delta.

  • 1971 October 21 - ITOS B.  Spacecraft: ITOS. Mass: 308 kg (679 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Unusable orbit.

  • 1972 October 15 - NOAA 2.  Spacecraft: ITOS. Mass: 344 kg (758 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1973 July 16 - ITOS E.  Spacecraft: ITOS. Mass: 345 kg (760 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Improved TIROS Operational System.

  • 1973 November 6 - NOAA 3.  Spacecraft: ITOS. Mass: 345 kg (760 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1974 November 15 - NOAA 4.  Spacecraft: ITOS. Mass: 340 kg (740 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1976 July 29 - NOAA 5.  Spacecraft: ITOS. Mass: 340 kg (740 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1978 October 13 - Tiros N.  Spacecraft: Tiros N. Mass: 734 kg (1,618 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1979 June 27 - NOAA 6.  Spacecraft: Tiros N. Mass: 723 kg (1,593 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1980 May 29 - NOAA B.  Spacecraft: Tiros N. Mass: 1,405 kg (3,097 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Unusable orbit; would have been NOAA 7. At engine start up, one of the booster engines suffered an internal fuel leak, causing it to run at about 80% thrust. As a result the booster was low on velocity and heavy on propellant over much of its flight and ran an incredible 50 seconds longer than the nominal burn. The NOAA Advanced TIROS payload was designed with no direct communication with the booster, and unaware of the booster problem, at 375 sec after liftoff attempted to separate with the booster still firing. The booster's continued thrusting defeated the payload's attempt to perform the required pitch maneuver. When the payload fired its apogee kick motor, it blew the top of the booster's liquid oxygen tank off. The spacecraft survived all this, but the resultant orbit was highly elliptical rather than the desired circular sun-synchronous. The mission was a total loss. Officially: Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).>

  • 1981 June 23 - NOAA 7.  Spacecraft: Tiros N. Mass: 1,405 kg (3,097 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1983 March 28 - NOAA 8.  Spacecraft: Advanced Tiros N. Mass: 3,775 kg (8,322 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Carried search and rescue package. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1984 December 12 - NOAA 9.  Spacecraft: Advanced Tiros N. Mass: 1,712 kg (3,774 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1986 September 17 - NOAA 10.  Spacecraft: Advanced Tiros N. Mass: 1,700 kg (3,700 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1988 September 24 - NOAA 11.  Spacecraft: Advanced Tiros N. Mass: 1,712 kg (3,774 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Carried search & rescue package. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1991 May 14 - NOAA 12.  Spacecraft: Tiros N. Mass: 1,416 kg (3,121 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).

  • 1993 August 9 - NOAA 13.  Spacecraft: Advanced Tiros N. Mass: 1,712 kg (3,774 lb). Launch Site: Vandenberg. Launch Vehicle: Atlas.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

  • 1998 May 13 - NOAA 15.  Spacecraft: Advanced Tiros N . Launch Site: Vandenberg. Launch Vehicle: Titan.

    NOAA K carried a new microwave sensor in addition to the standard optical/near-infrared radiometers and imagers and the SARSAT search and rescue package. It was the first NOAA launch to use the Titan 23G launch vehicle, a refurbished ICBM. Titan 23G-12 placed NOAA K into a suborbital trajectory 6 minutes after launch. A Star 37XFP solid motor on the satellite fired at apogee to put NOAA K in orbit.

  • 2000 September 21 - NOAA 16.  Spacecraft: Advanced Tiros N. Mass: 1,476 kg (3,254 lb). Launch Site: Vandenberg. Launch Vehicle: Titan.

    Launch attempt on September 20 scrubbed. The NOAA polar orbit weather satellite, an Advanced Tiros N with a suite of imaging and sounding instruments. The two-stage Titan II launch vehicle, serial 23G-13, put NOAA-L into a suborbital -2500 x 800 km x 98.0 deg trajectory. The spacecraft's Thiokol Star 37XFP solid motor fired at apogee to circularize the sun-synchronous orbit at 800 km.

  • 2002 June 24 - NOAA 17.  Spacecraft: Tiros N. Mass: 1,475 kg (3,251 lb). Launch Site: Vandenberg. Launch Vehicle: Titan.

    Launch delayed from August 2001. The refurbished Titan 2 missile put the NOAA M satellite on a suborbital trajectory of about -2500 x 820 km x 98 deg. at 1829 UTC. At 1837 UTC the NOAA M propulsion module fired its ATK/Thiokol Star 37XFP solid motor for the orbit insertion burn, followed by a hydrazine trim burn to put the satellite in an 807 x 822 km x 98.8 deg operational orbit. NOAA M became NOAA 17 on entering service with the US National Oceanic and Atmospheric Administration as the primary morning weather satellite, supplementing the NOAA 16 afternoon satellite. Built by Lockheed Martin, NOAA M carried weather imagers and microwave and infrared sounders, as well as a SARSAT search-and-rescue package. It had an on-orbit mass of 1475 kg.

  • 2005 May 20 - NOAA 18.  Spacecraft: Advanced Tiros N. Mass: 1,420 kg (3,130 lb). Launch Site: Vandenberg. Launch Vehicle: Delta.

    Delayed from June 30, 2004, February 12, March 10 and 19, May 11, 12, 13 and 14.


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