Intelsat VA F-12
{{Short description|Communications satellite}}
{{Use British English|date=June 2020}}
{{Use dmy dates|date=June 2020}}
{{Infobox spaceflight
| name = Intelsat VA F-12 → Intelsat 512
| image =
| image_caption =
| mission_type = Communication
| operator = Intelsat
| website =
| COSPAR_ID = 1985-087A {{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1985-087A|title=Display: Intelsat 5A F-12 1985-087A|publisher=NASA|access-date=April 23, 2017}} {{PD-notice}}
| SATCAT = 16101
| mission_duration = 7 years (planned)
| spacecraft_bus = Intelsat VA
| manufacturer = Ford Aerospace
| dry_mass = 1098 kg
| launch_mass = 1981 kg
| power = 1800 watts
| launch_date = 29 September 1985,
23:36:00 UTC {{cite web|url=http://planet4589.org/space/log/launchlog.txt|title=Launch Log|first=Jonathan|last=McDowell|work=Jonathan's Space Page|access-date=April 23, 2017}}
| launch_rocket = Atlas G-Centaur D1AR (AC-65)
| launch_contractor = General Dynamics
| entered_service =
| dimensions = 1.66 x 2.1 x 1.77 metres
| disposal_type = Graveyard orbit
| deactivated = July 1998
| orbit_epoch = 29 September 1985
| orbit_reference = Geocentric orbit
| orbit_regime = Geostationary orbit
| orbit_longitude = 34.5° West (1985-1991)
1.0° West (1991-1994)
21.5° West (1994-1996)
55.5° West (1996-1998)
| apsis = gee
| trans_band = 26 C-band
6 Ku-band
| trans_frequency =
| trans_capacity =
| trans_coverage =
| trans_TWTA =
| trans_EIRP =
| trans_HPBW =
| programme = Intelsat V
| previous_mission = Intelsat VA F-11
| next_mission = Intelsat VA F-13
}}
Intelsat VA F-12, then named Intelsat 512, was a communications satellite operated by Intelsat. Launched in September 1985, it was the twelfth of fifteen Intelsat V satellites to be launched. The Intelsat V series was constructed by Ford Aerospace, based on the Intelsat VA satellite bus. Intelsat VA F-12 was part of an advanced series of satellites designed to provide greater telecommunications capacity for Intelsat's global network.
Satellite
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 by nickel-hydrogen batteries during eclipse, provided 1800 watts of power at mission onset, approximately 1280 watts at the end of its seven-year design life. The payload housed 26 C-band and 6 Ku-band transponders. It could accommodate 15,000 two-way voice circuits and two TV channels simultaneously. It also provided maritime communications for ships at sea.{{cite web |url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1989-006A|title=Display: Intelsat 5A F-15 1989-086A|publisher=NASA|date=14 May 2020|access-date=20 June 2020}} {{PD-notice}}
Launch
The satellite was successfully launched into space on 29 September 1985, at 23:36:00 UTC, by means of an Atlas G-Centaur D1AR vehicle from the Cape Canaveral Air Force Station, Florida, United States. It had a launch mass of 1981 kg.{{cite web|url=http://www.tbs-satellite.com/tse/online/sat_intelsat_512.html|title=Intelsat 512|publisher=TSE|access-date=April 23, 2017}} The satellite was deactivated in July 1998.
References
{{Portal|Spaceflight}}
{{reflist}}
{{Intelsat}}
{{SES satellites}}
{{Orbital launches in 1985}}
Category:Spacecraft launched in 1985
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