PAS-22

Last updated

  AsiaSat 3 / HGS-1
   Moon
   Earth

The satellite was transferred to Hughes Global Services Inc., which was then a subsidiary of Hughes Space and Communications, with an agreement to share any profits with the consortium of 27 insurers. [6]

Edward Belbruno and Rex Ridenoure heard about the problem and proposed a 3–5 month low-energy transfer trajectory that would swing past the Moon and leave the satellite in geostationary orbit around the Earth. Hughes had no ability to track the satellite at such a distance and considered this trajectory concept unworkable. Instead, Hughes used an Apollo-style free-return trajectory that required only a few days to complete, a trajectory designed and subsequently patented [7] [8] by Hughes Chief Technologist Jerry Salvatore. [9] This maneuver removed only 40° of orbital inclination and left the satellite in a geosynchronous orbit, whereas the Belbruno maneuver would have removed all 51° of inclination and left it in geostationary orbit. [6]

Although Hughes did not end up using the low-energy transfer trajectory, the insight to use a lunar swingby was key to the spacecraft rescue. According to Cesar Ocampo, Hughes had not considered this option until it was contacted by Ridenoure, [10] although the Hughes engineers involved in the lunar flyby operations have stated that they were already working on the lunar swingby mission design before being contacted by him. [9]

Rescue of satellite

Using on-board propellant and lunar gravity, the orbit's apogee was gradually increased with several manoeuvres at perigee until it flew by the Moon [10] at a distance of 6,200 km from its surface in May 1998, becoming in a sense the first commercial lunar spacecraft. Another lunar fly-by was performed later that month (6 June 1998) at a distance of 34,300 km to further improve the orbital inclination. [6]

These operations consumed most of the satellite's propellant, but still much less than it would take to remove the inclination without the Moon-assist manoeuvres. With the remaining fuel, the satellite could be controlled as a geosynchronous satellite, with half the life of a normal satellite – a huge gain, considering that it had been declared a total loss. The satellite was then maneuvered to geosynchronous orbit at 158° West. [6]

Once the satellite was in a stable orbit, it was commanded to release its solar panels, which had been stowed during takeoff and maneuvering. Of the satellite's two solar panels, only one released, and it became apparent that a tether was not operating correctly on board, which engineers attributed to heating and cooling cycles due to the satellite operating outside its design range while traveling to its final orbit. [6]

PAS-22

In April 1999, Hughes filled to request authorization to operate the satellite at 60° West in C-band and in Ku-band. In 1999, HGS-1 was acquired by PanAmSat, and renamed as PAS-22, and moved to 60° West. It was deactivated in July 2002 and moved to a graveyard orbit. [4]

See also

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References

  1. "AsiaSat-3, -3S / HGS-1 / PAS-22". Gunter's Space Page. Retrieved 15 May 2010.
  2. "AsiaSat 3 → HGS-1 → PAS-22". NASA's Solar System Exploration website. Retrieved 1 December 2022.
  3. "Launch Log". Jonathan's Space Report. 14 March 2021. Retrieved 3 May 2021.
  4. 1 2 "Asiasat 3". The Satellite Encyclopedia. Retrieved 15 May 2010.
  5. "AsiaSat 3" . Retrieved 15 May 2010.
  6. 1 2 3 4 5 "HGS-1 Arrives in Earth Orbit: First Commercial Lunar Mission". NASA. 17 June 1998. Archived from the original on 30 July 2010. Retrieved 4 May 2021.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  7. Salvatore, Jeremiah O., and Ocampo Cesar A. (Assignee: Hughes Electronics Corporation) U.S. Patent 6,116,545, "Free return lunar flyby transfer method for geosynchronous satellites", Filed April 9, 1998.
  8. Salvatore, Jeremiah O. and Ocampo, Cesar A. (Assignee: Hughes Electronics Corporation) U.S. Patent 6,149,103, "Free return lunar flyby transfer method for geosynchronous satellites having multiple perilune stages", filed May 15, 1998
  9. 1 2 J. Fisher, "AsiaSat Rescue: The Real Story, Part 1" Hughes, July 8, 2013 (accessed 10 December 2014)
  10. 1 2 "New Book Reveals How Engineers Saved Hughes Satellite on Christmas Day 1997". Space Daily. 11 January 2006.
AsiaSat 3 → HGS-1 → PAS-22
NamesAsiaSat 3
HGS-1
PAS-22
Mission type Communications
Operator AsiaSat (1997–1998)
Hughes (1998–1999)
PanAmSat (1999–2002)
COSPAR ID 1997-086A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 25126
Mission duration15 years (planned) [1]
4 years (achieved)
Spacecraft properties
SpacecraftAsiaSat 3
Spacecraft type Boeing 601
Bus HS-601HP
Manufacturer Hughes Space and Communications
Launch mass3,465 kg [2]
Dry mass2,500 kg (5,500 lb)
Dimensions3.4 m x 3.5 m x 5.8 m
Span: 26.2 m on orbit
Power9.9 kW
Start of mission
Launch date24 December 1997,
23:19:00 UTC [3]
Rocket Proton-K / DM-2M
Launch site Baikonur, Site 81/23
Contractor Khrunichev State Research and Production Space Center
Entered serviceJuly 1998
End of mission
Disposal Graveyard orbit
DeactivatedJuly 2002
Orbital parameters
Reference system Geocentric orbit
Regime Geostationary orbit
Longitude105.5° East (intended)
158° West (1998-1999)
62° West (1999–2002) [4]
Flyby of Moon
Closest approach13 May 1998, 19:00 UTC [5]
Distance6,200 km (3,900 mi)