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EntityQ156081· pop 40· linked from 811 articles

Also known as International Solar Polar Mission, ISPM, Ulysses spacecraft, Ulysses orbiter, Odysseus, Ulysses Heliospheric Mission

NASA robotic space probe that studied the Sun

Key facts

Names
Odysseus
Mission type
High-inclination solar orbiter
Operator
NASA / ESA
Cospar id
1990-090B
Website
NASA Page , ESA Page
Mission duration
18 years, 8 months, 24 days
Manufacturer
Astrium GmbH, Friedrichshafen , (formerly Dornier Systems )
Launch mass
371 kg (818 lb)
Payload mass
55 kg (121 lb)
Dimensions
3.2 m × 3.3 m × 2.1 m (10.5 ft × 10.8 ft × 6.9 ft)
Power
285 watts
Launch date
6 October 1990, 11:47:16 UTC
Rocket
Space Shuttle Discovery ( STS-41 ) with Inertial Upper Stage and PAM-S
Launch site
Kennedy Space Center , LC-39B
Contractor
NASA
Disposal
Decommissioned
Deactivated
30 June 2009
Reference system
Heliocentric orbit

via Wikipedia infobox

Wikidata facts

Mass
371
Orbital period
2264.26
Image
Ulysses at Jupiter H1.jpg
Show 9 more facts
Commons category
Ulysses (spacecraft)
UTC date of spacecraft launch
1990-10-06
native label
Ulysses
service retirement
2009-06-30
periapsis
1.35
apoapsis
5.40
orbital eccentricity
0.60262
orbital inclination
79.110
semi-major axis of an orbit
3.37
Sources (10)

via Wikidata · CC0

~24 min read

Article

Ulysses (/juːˈlɪsiːz/ yoo-LISS-eez, UK also /ˈjuːlɪsiːz/ 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. The last day for mission operations on Ulysses was 30 June 2009.

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).

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