Ulysses (spacecraft)

Ulysses
Ulysses spacecraft
NamesOdysseus
Mission typeHeliophysics
OperatorNASA / ESA
COSPAR ID1990-090B Edit this at Wikidata
SATCAT no.20842
WebsiteNASA Page
ESA Page
Mission duration18 years, 8 months, 24 days[1]
Spacecraft properties
ManufacturerAstrium GmbH, Friedrichshafen
(formerly Dornier Systems)
Launch mass371 kg (818 lb)[2]
Payload mass55 kg (121 lb)
Dimensions3.2 m × 3.3 m × 2.1 m (10.5 ft × 10.8 ft × 6.9 ft)
Power285 watts
Start of mission
Launch date6 October 1990, 11:47:16 UTC[2]
RocketSpace Shuttle Discovery (STS-41) with Inertial Upper Stage and PAM-S
Launch siteKennedy Space Center, LC-39B
ContractorNASA
End of mission
DisposalDecommissioned
Deactivated30 June 2009
Orbital parameters
Reference systemHeliocentric orbit
Perihelion altitude1.35 AU
Aphelion altitude5.40 AU
Inclination79.11°
Period2,264.26 days (6.2 years)
Flyby of Jupiter (gravity assist)
Closest approach8 February 1992
Distance440,439 km (6.3 Jupiter radii)
Ulysses mission insignia
Ulysses mission patch  

Ulysses (/jˈlɪsz/ yoo-LISS-eez, UK also /ˈjlɪsz/ YOO-liss-eez) was a robotic space probe whose primary mission was to orbit the Sun and study it at all latitudes. It was launched in 1990 and made three "fast latitude scans" of the Sun in 1994/1995, 2000/2001, and 2007/2008. In addition, the probe studied several comets. Ulysses was a joint venture of the European Space Agency (ESA) and the United States' National Aeronautics and Space Administration (NASA), under leadership of ESA with participation from Canada's National Research Council.[3] The last day for mission operations on Ulysses was 30 June 2009.[4][5]

To study the Sun at all latitudes, the probe needed to change its orbital inclination and leave the plane of the Solar System. To change the orbital inclination of a spacecraft to about 80° requires a large change in heliocentric velocity, the energy to achieve which far exceeded the capabilities of any launch vehicle. To reach the desired orbit around the Sun, the mission's planners chose a gravity assist maneuver around Jupiter, but this Jupiter encounter meant that Ulysses could not be powered by solar cells. The probe was powered instead by a General Purpose Heat Source Radioisotope Thermoelectric Generator (GPHS-RTG).[6]

The spacecraft was originally named Odysseus, because of its lengthy and indirect trajectory to study the solar poles. It was renamed Ulysses, the Latin translation of "Odysseus", at ESA's request in honor not only of Homer's mythological hero but also of Dante's character in the Inferno.[7] Ulysses was originally scheduled for launch in May 1986 aboard the Space Shuttle Challenger on STS-61-F. Due to the 28 January 1986 loss of Challenger, the launch of Ulysses was delayed until 6 October 1990 aboard Discovery (mission STS-41).

  1. ^ "Ulysses". NASA's Solar System Exploration website. Retrieved 25 September 2023.
  2. ^ a b "Ulysses". NASA's Solar System Exploration website. Retrieved 2 December 2022.
  3. ^ "Welcome to the HIA Ulysses Project". Herzberg Institute of Astrophysics. Archived from the original on 17 August 2011. The Herzberg Institute of Astrophysics (HIA) of the National Research Council of Canada provided instrumentation and test equipment for the COsmic ray and Solar Particle INvestigation (COSPIN) on the Ulysses spacecraft. The COSPIN instrument consists of five sensors which measure energetic nucleons and electrons over a wide range of energies. This was the first participation by Canada in a deep-space interplanetary mission.
  4. ^ Cite error: The named reference ESA News was invoked but never defined (see the help page).
  5. ^ The odyssey concludes ... Archived February 24, 2012, at the Wayback Machine
  6. ^ https://rps.nasa.gov/missions/13/ulysses/
  7. ^ "Inferno of Ulysses' urge to explore an uninhabited world behind the Sun. In Jane's Spaceflight Directory 1988, ISBN 0-7106-0860-8

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