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Astra 1K

Communications satellite


Communications satellite

FieldValue
nameAstra 1K
image_size300px
mission_typeCommunications
operatorSES
COSPAR_ID2002-053A
SATCAT27557
websitehttps://www.ses.com/
mission_duration15 years (planned)
Failed on orbit (DM03 failure)
spacecraft_typeSpacebus
spacecraft_busSpacebus-3000B3S
manufacturerAlcatel Space
launch_mass5250 kg
power13 kW
launch_date25 November 2002,
23:04:23 UTC
launch_rocketProton-K / DM03
launch_siteBaikonur, Site 81/23
launch_contractorKhrunichev State Research and Production Space Center
entered_serviceFailed on orbit (DM03 failure)
disposal_typeDeorbited
decay_date10 December 2002
orbit_referenceGeocentric orbit
orbit_regimeLow Earth orbit
Geostationary orbit (planned)
orbit_periapsis142 km
orbit_apoapsis288 km
orbit_inclination51.5°
orbit_period88.79 minutes
orbit_longitude19.2° East (planned)
apsisgee
trans_band54 transponders:
52 Ku-band
2 Ka-band
trans_coverageEurope
programmeAstra constellation
previous_missionAstra 3A
next_missionAstra 1KR

Failed on orbit (DM03 failure) 23:04:23 UTC Geostationary orbit (planned) 52 Ku-band 2 Ka-band

Astra 1K was a communications satellite manufactured by Alcatel Space for SES. When it was launched on 25 November 2002, it was the largest civilian communications satellite ever launched, with a mass of 5250 kg. Intended to replace the Astra 1B satellite and provide backup for 1A, 1C and 1D at the Astra 19.2°E orbital position, the Blok DM3 upper stage of the Proton-K launch vehicle failed to function properly, leaving the satellite in an unusable parking orbit.

Launch

Astra 1K was to be a European (Luxembourg-based) geostationary communications satellite that was launched by a Proton-K launch vehicle from Baikonur Cosmodrome at 23:04:23 UTC on 25 November 2002. However, the Blok DM3 upper stage attached to the 5250 kg, 13 kW satellite (reported to be the most massive of civilian communications satellite, with its 52 Ku-band and two Ka-band transponders to cover 1,100 channels) was miscommanded to separate after the first burn, resulting in the satellite orbiting at a very low orbit. In an effort to prevent imminent re-entry, the satellite was raised to a circular orbit at an altitude of 288 km, providing sufficient time to select the best course of action. Three options were then under consideration: a) to force its re-entry over the Pacific Ocean, b) to retrieve it by a Space Shuttle, and c) to use up all the fuel on board the satellite to move it to a geostationary orbit at 19.2° east. Although it was suggested that a separately-launched Orbital Recovery Corporation 'space tug' (then in development) might be used to take the satellite to geostationary orbit, the decision was taken in December 2002 to deorbit the satellite, resulting in a huge insurance loss and bringing into question both continued use of the Blok D series of upper stages and the "bigger is better" communications satellite philosophy. Astra 1K was intentionally de-orbited on 10 December 2002.

Overview

The satellite featured frequency re-use for some of its transponders, using dual patterns coverage, one covering eastern Europe, the other covering Spain. This design was meant to cover specific markets only, in order to expand the capacity of the fleet, as frequency re-use enables more channels to be transmitted simultaneously at the same frequency, with the drawback that channels broadcast on the Spain beam wouldn't be receivable by any means (no matter how large the receiving dish would be) in the east beam and vice versa. This would have left for example the Netherlands and parts of neighbouring countries without reception of either of the beams, as the beams overlap over those countries, efficiently jamming each other.

Astra 1K also featured multiple Ka-Band capabilities, originally intended to provide an upload path for satellite Internet access services. SES later developed such a 2-way commercial satellite internet service with ASTRA2Connect (now SES Broadband), using Ku-band for upload and download paths.

Replacement satellite

A replacement satellite, Astra 1KR was successfully launched in 2006.

References

References

  1. "Satellite Catalog". Jonathan's Space Report.
  2. (2019). "Proton-K/DM-2M". Encyclopedia Astronautica.
  3. (February 11, 1998). "ASTRA 1K UNDER PROCUREMENT WITH AÉROSPATIALE". SES ASTRA.
  4. (10 February 2021). "Display:Astra 1K 2002-053A". NASA.
  5. [https://spaceref.com/press-release/orbital-recovery-corporation-offers-space-rescue-for-stranded-astra-1k-telecommunications-satellite/ ''Orbital Recovery Corporation Offers Space Rescue for Stranded Astra 1K Telecommunications Satellite''] Space Ref. 5 December 2002. Accessed 27 January 2023
  6. [https://www.businessinsurance.com/article/20021202/story/20001701/satellite-loss-likely-despite-recovery-efforts ''Satellite loss likely despite recovery efforts''] Business Insurance. 2 December 2002. Accessed 27 January 2023
  7. "ASTRA 1K - Satellite Informations".
  8. (15 December 1998). "SES TO DEVELOP INTERACTIVE SATELLITE RETURN CHANNEL". SES ASTRA.
  9. (April 21, 2006). "ASTRA 1KR SATELLITE SUCCESSFULLY LAUNCHED". SES ASTRA.
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