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T200

Spacecraft

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

TRW satellite bus launched in 1997-1999.

More at: T200.

Subtopics

  • Lewis satellite American earth land resources satellite. Lewis was selected in the NASA SSTI (Small Spacecraft Technology Initiative) program, along with Clark, to demonstrate advanced spacecraft technologies. Earth observing satellite built by TRW for NASA, USA. Launched 1997. Used the T200B bus.
  • ROCSAT Taiwanese earth sea satellite. Taiwan's ROCSAT (Republic of China Satellites) were built for Taiwan's National Space Program Office. Earth Observing satellite built by TRW for NSPO, Taiwan. Launched 1999. Used the T200A bus.
  • KOMPSAT South Korean technology satellite. KOMPSAT was the first joint spacecraft development project for the South Korean aerospace agency KARI (Korea Aerospace Research Institute). Earth Observing satellite built by KARI, TRW (Bus) for KARI, Korea South. Launched 1999. Used the T200B bus.

Chronology

10 events

1994 July 11

  • Contract for Lewis satellite issued. - . Nation: USA. Spacecraft Bus: T200. Spacecraft: Lewis satellite. Lewis was selected in the NASA SSTI (Small Spacecraft Technology Initiative) program, along with Clark, to demonstrate advanced spacecraft technologies..

1994 September 19

  • Kompsat contract - . Nation: Korea South. Spacecraft Bus: T200. Spacecraft: KOMPSAT. TRW and Korean engineers would work together to develop the spacecraft. KOMPSAT was based on TRW's Eagle class of light weight, modular spacecraft..

1997 August 23

06:51 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC6. LV Family: Athena. Launch Vehicle: Athena-1.
  • Lewis - . Payload: SSTI/Lewis. Nation: USA. Agency: NASA, TRW. Manufacturer: Chantilly. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: T200. Spacecraft: Lewis satellite. Decay Date: 1997-09-28 . USAF Sat Cat: 24909 . COSPAR: 1997-044A. Apogee: 134 km (83 mi). Perigee: 124 km (77 mi). Inclination: 97.50 deg. Period: 87.10 min. Reentered Sep 28.

1999 January 27

00:34 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC46. Launch Pad: SLC46. LV Family: Athena. Launch Vehicle: Athena-1.
  • ROCSAT-1 - . Mass: 400 kg (880 lb). Nation: Taiwan. Agency: NSPO. Manufacturer: TRW. Class: Earth. Type: Seismology satellite. Spacecraft Bus: T200. Spacecraft: ROCSAT. USAF Sat Cat: 25616 . COSPAR: 1999-002A. Apogee: 523 km (324 mi). Perigee: 479 km (297 mi). Inclination: 34.96 deg. Period: 94.63 min.

    Taiwan's first satellite, with experimental communications, ocean imagery, and ionospheric studies instruments. The Primex OAM placed itself and the payload into an elliptical transfer orbit. A second OAM burn circularized the orbit, and ROCSAT separated into a 588 x 601 km x 35.0 deg orbit.

1999 December 21

07:13 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576E. LV Family: Taurus. Launch Vehicle: Taurus 2110.
  • Kompsat - . Payload: Arirang. Mass: 470 kg (1,030 lb). Nation: Korea South. Agency: KARI. Manufacturer: KAIST. Class: Earth. Type: Sea satellite. Spacecraft Bus: T200. Spacecraft: KOMPSAT. USAF Sat Cat: 26032 . COSPAR: 1999-070A. Apogee: 677 km (420 mi). Perigee: 670 km (410 mi). Inclination: 97.80 deg. Period: 98.20 min.

    Korean Multipurpose Satellite; carried an ocean color sensor developed by TRW and particle detectors. KOMPSAT was built by the Korean Aerospace Research Institute (KARI) based on a test model built by TRW; it used the TRW STEP Lightsat bus and had a mass of around 500 kg, with 73 kg of hydrazine fuel.

2004 May 20

17:47 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576E. LV Family: Taurus. Launch Vehicle: Taurus 3210.
  • ROCSAT 2 - . Payload: LeoStar 500XO. Mass: 760 kg (1,670 lb). Nation: Taiwan. Agency: NSPO. Manufacturer: EADS Astrium. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft Bus: T200. Spacecraft: ROCSAT. USAF Sat Cat: 28254 . COSPAR: 2004-018A. Apogee: 891 km (553 mi). Perigee: 887 km (551 mi). Inclination: 99.10 deg. Period: 102.80 min. Delayed from October, November 25, 2003; January 17, February 26, April 9 and 22, May 17, 2004..

2008 October 1

Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Theos - . Mass: 715 kg (1,576 lb). Nation: Thailand. Agency: Makeyev bureau. Manufacturer: EADS Astrium. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft Bus: T200. Spacecraft: ROCSAT. USAF Sat Cat: 33396 . COSPAR: 2008-049A. Apogee: 693 km (430 mi). Perigee: 673 km (418 mi). Inclination: 98.80 deg. Period: 98.40 min. Thai surveillance satellite, based on EADS Astrium bus used for ROCSAT-2..

2012 May 17

16:39 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.
  • Arirang-3 - . Payload: Kompsat-3. Mass: 800 kg (1,760 lb). Nation: Korea South. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: T200. Spacecraft: Kompsat. USAF Sat Cat: 38338 . COSPAR: 2012-025B. Apogee: 677 km (420 mi). Perigee: 665 km (413 mi). Inclination: 98.10 deg. Period: 98.20 min. South Korean imaging satellite..

2013 August 22

14:39 GMT - . Launch Site: Dombarovskiy. Launch Pad: Yasniy Sh370/13. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Arirang-5 - . Payload: Kompsat-5. Mass: 1,400 kg (3,000 lb). Nation: Korea South. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: T200. Spacecraft: Kompsat. USAF Sat Cat: 39227 . COSPAR: 2013-042A. Apogee: 560 km (340 mi). Perigee: 545 km (338 mi). Inclination: 97.60 deg. Period: 95.70 min. South Korea's first X-band SAR satellite..

2015 March 25

22:08 GMT - . Launch Site: Dombarovskiy. Launch Complex: Yasniy Sh370/13. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Arirang-3A - . Payload: KOMPSAT 3A. Mass: 800 kg (1,760 lb). Nation: Korea South. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: T200. Spacecraft: Kompsat. USAF Sat Cat: 40536 . COSPAR: 2015-014A. Apogee: 538 km (334 mi). Perigee: 522 km (324 mi). Inclination: 97.53 deg. Period: 95.23 min. South Korean imaging satellite with submeter resolution. Sun synchronous orbit; 0130 GMT local time of the descending node..