Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Intelsat V F-2

From Wikipedia, the free encyclopedia
Communications Satellite

Intelsat V F-2 → Intelsat 502
Mission typeCommunication
OperatorCOMSAT /Intelsat
COSPAR ID1980-098A[1]
SATCATno.12089
Mission duration7 years (planned)
Spacecraft properties
BusIntelsat V
ManufacturerFord Aerospace
Launch mass1928 kg
Dry mass1012 kg
Dimensions1.66 x 2.1 x 1.77 metres
Start of mission
Launch date6 December 1980, 23:31:00 UTC
RocketAtlas SLV-3D Centaur-D1AR (AC-54)
Launch siteCCAFS,LC-36B
ContractorGeneral Dynamics
Entered service1800 watts
End of mission
DisposalGraveyard orbit
Deactivated14 April 1998
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude21.5° West (1980-1994)
40.5° West (1994-1998)
Epoch6 December 1980
Transponders
Band21C-band
4Ku-band
Intelsat V

Intelsat V F-2, then namedIntelsat 502, was acommunications satellite operated byCOMSAT. Launched in 1980, it was the first of fifteenIntelsat V satellites to be launched. The Intelsat V series was constructed byFord Aerospace, based on theIntelsat Vsatellite bus. Intelsat V F-2 was part of an advanced series of satellites designed to provide greatertelecommunications capacity forINTELSAT's global network.

Satellite

[edit]

The satellite was box-shaped, measuring 1.66 by 2.1 by 1.77 metres;solar arrays spanned 15.9 metres tip to tip. The arrays, supplemented bynickel-hydrogen batteries during an eclipse, provided 1800 watts of power at mission onset of its seven-year design life. The payload housed 21C-band and 4Ku-band transponders. It could accommodate 15,000 two-way voice circuits and two TV channels simultaneously. It had a launch mass of 1928 kg.[2] In December 1992, the satellite enabled a direct link between United States and the Somalia. The satellite was deactivated on 14 April 1998.[3]

Launch

[edit]

The satellite was successfully launched into space on 6 December 1980, at 23:31:00 UTC, by means of anAtlas SLV-3D Centaur-D1AR vehicle from theCape Canaveral Air Force Station,Florida,United States.

References

[edit]
  1. ^"Intelsat 5 F-2 1980-098A". NASA. 14 May 2020. Retrieved30 June 2020.Public Domain This article incorporates text from this source, which is in thepublic domain.
  2. ^"Display: Intelsat 5A F-15 1989-086A". NASA. 14 May 2020. Retrieved30 June 2020.Public Domain This article incorporates text from this source, which is in thepublic domain.
  3. ^"Satellite V F-2". 31 May 2020. Retrieved30 June 2020.
Intelsat I,II,III
Intelsat IV
Intelsat V
Intelsat VI
Intelsat 7-10
ex-PanAmSat
Recent Intelsat
Galaxy
(Intelsat Americas)
Other
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated inunderline. Uncatalogued launch failures are listed initalics. Payloads deployed from other spacecraft are denoted in (brackets).
Stub icon

Thisspacecraft orsatellite related article is astub. You can help Wikipedia byadding missing information.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Intelsat_V_F-2&oldid=1286218412"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2026 Movatter.jp