Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Multi-Functional Transport Satellite

From Wikipedia, the free encyclopedia
(Redirected fromMTSAT-1)
Series of weather and aviation control satellites

MTSAT-1Himawari 6

Multifunctional Transport Satellites (MTSAT) were a series ofweather andaviation control satellites. They were replaced byHimawari 8 on 7 July 2015. They weregeostationary satellites owned and operated by the JapaneseMinistry of Land, Infrastructure, Transport and Tourism (MLIT) and theJapan Meteorological Agency (JMA), and provide coverage for the hemisphere centred on 140.0° East; this includes Japan and Australia who are the principal users of thesatellite imagery that MTSAT provides. They replace theGMS-5 satellite, also known asHimawari 5 ("himawari" or "ひまわり" meaning "sunflower"). They can provide imagery in five wavelength bands —visible and fourinfrared, including thewater vapour channel. The visible light camera has a resolution of 1 km; the infrared cameras have 4 km (resolution is lower away from the equator at 140° East). The spacecraft have a planned lifespan of five years. MTSAT-1 and 1R were built bySpace Systems/Loral. MTSAT-2 was built byMitsubishi.

MTSAT-1 and GOES-9

[edit]

Launch failure

[edit]

The launch of MTSAT-1, on a JapaneseH-II rocket, failed on 15 November 1999 and the spacecraft was destroyed.GMS-5, the satellite MTSAT-1 was intended to replace, was decommissioned on 1 April 2003 leaving Japan without weather satellite imagery.

NOAA loan

[edit]

To fill in the void, the United StatesNational Oceanic and Atmospheric Administration (NOAA) loaned theGOES-9 satellite to the JMA and repositioned it over 155.0° East on 22 May 2003.[1]

MTSAT-1R

[edit]

MTSAT-1R (also known asHimawari 6) was successfully launched on aH-IIA on 26 February 2005 and became partially operational on 28 June 2005 — the aviation payload was not functional as two MTSATs are required for air traffic control. GOES-9 was decommissioned when MTSAT-1R came online in June 2005.

Itssolar sail counteracts the torque produced by sunlight pressure on the solar array. The trim tab on the solar array makes small adjustments to the torque balance.[2]

MTSAT-1R was decommissioned on 4 December 2015, due to fuel limitations.[3][4]

MTSAT-2

[edit]

MTSAT-2 (also known asHimawari 7) successfully launched on 18 February 2006 and is positioned at 145.0° East. The weather functions of MTSAT-2 were put into hibernation until the end of MTSAT-1R's life (5 years from launch). The transportation and communication functions of MTSAT-2 are utilised prior to that time. It was replaced byHimawari 8 on 7 July 2015.

Attitude control malfunction

[edit]

On 5 November 2007,Japan Meteorological Agency (JMA) announced a malfunction in theattitude control of MTSAT-2. Attitude control was restored 7 November 2007. The presumed cause of the malfunction was improper functioning of an attitude control thruster. A spare thruster was used to return the spacecraft to normal operation.[5]

Ground segment

[edit]

Ground stations for both satellites are located inKobe andHitachiōta, Ibaraki, Japan.

References

[edit]
  1. ^"JAPANESE NOW USING NOAA GOES-9 ENVIRONMENTAL SATELLITE".noaa.gov. 22 May 2003. Archived fromthe original on 4 February 2017. Retrieved19 August 2017.Public Domain This article incorporates text from this source, which is in thepublic domain.
  2. ^"MTSAT (Multi-functional Transport Satellite)".globalsecurity.org. Retrieved19 August 2017.
  3. ^"Administrative: (Final Update) MTSAT-2 Weekly Special".ssd.noaa.gov. Retrieved19 August 2017.Public Domain This article incorporates text from this source, which is in thepublic domain.
  4. ^"Internal Waves in the Banda Sea".cimss.ssec.wisc.edu. 30 October 2015. Retrieved19 August 2017.
  5. ^"Recovery of MTSAT-2". JMA. 7 November 2007.

External links

[edit]
Generations
Geostationary Meteorological Satellites (GMS)
Multi-Functional Transport Satellites (MTSAT)
Himawari
  • Italics indicates projects in development.
  • Symbol indicates failed projects.
  • Strikethrough lines indicate cancelled projects.
National space agencies
Joint development partners
Past
Active
Future
Past
Active
Future
Past
Active
Future
Engineering tests
Past
Active
Future
Past
Active
Future
The Moon
Past
Active
Future
Others
Past
Active
Future
Past
  • IGS-Optical
    • 1
    • 2
    • Experimentally 3
  • IGS-Radar
    • 1
    • 2
Active
  • IGS-Optical
    • 3
    • 4
    • 5
    • 6
    • Experimentally 5
  • IGS-Radar
    • 3
    • 4
    • Spare
    • 5
    • 6
Future
  • IGS-Optical
    • 7
    • 8
  • IGS-Radar
    • 7
    • 8
Past
Active
Future
January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Retrieved from "https://en.wikipedia.org/w/index.php?title=Multi-Functional_Transport_Satellite&oldid=1260907724#MTSAT-1_and_GOES-9"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp