Ulysses (spacecraft)

[3][4] To study the Sun at all latitudes, the probe needed to change its orbital inclination and leave the plane of the Solar System.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.The box mounted the 1.65 m (5 ft 5 in) dish antenna and the GPHS-RTG radioisotope thermoelectric generator (RTG) power source.The spacecraft used X-band for science return (downlink only), using dual 20 watts TWTAs until the failure of the last remaining TWTA in January 2008.Dual tape recorders, each of approximately 45-megabit capacity, stored science data between the nominal eight-hour communications sessions during the prime and extended mission phases.Documented 1802 usage includes dual-redundant 1802s in the COSPIN, and at least one 1802 each in the GRB, HI-SCALE, SWICS, SWOOPS and URAP instruments, with other possible microprocessors incorporated elsewhere.However, gravity assists are not limited to in-plane maneuvers; a suitable flyby of Jupiter could produce a significant plane change.NASA would provide the Radioisotope Thermoelectric Generator (RTG) and launch services, ESA would build the spacecraft assigned to Astrium GmbH, Friedrichshafen, Germany (formerly Dornier Systems).The changes delayed launch from February 1983 to May 1986 when it was to be deployed by the Space Shuttle Challenger (boosted by the proposed Centaur G Prime upper stage).However, the Challenger disaster forced a two-and-a-half year stand down of the shuttle fleet, mandated the cancellation of the Centaur-G upper stage, and pushed the launch date to October 1990.[22] ESA's Science Program Committee approved the fourth extension of the Ulysses mission to March 2004 [23] thereby allowing it to operate over the Sun's poles for the third time in 2007 and 2008.As the spacecraft traveled on its outbound trajectory to the orbit of Jupiter, the downlink signal would have eventually fallen below the receiving capability of even the largest antennas (70 meters - 229.7 feet - in diameter) of the Deep Space Network.Once the hydrazine froze, the spacecraft would no longer be able to maneuver to keep its high gain antenna pointing towards Earth, and the downlink signal would then be lost in a matter of days.[29] When the spacecraft was out of contact with a ground station, the S-band transmitter was switched off and the power was diverted to the internal heaters to add to the warming of the hydrazine.Typically, a determination came from comparing: one of several spacecraft orbiting the Earth, an inner-Solar-System probe (to Mars, Venus, or an asteroid), and Ulysses.However, there is a chance that in one of its re-encounters with Jupiter a close fly-by with one of the Jovian moons would be enough to alter its course and so the probe would enter a hyperbolic trajectory around the Sun and leave the Solar System.
Ulysses spacecraft
Ulysses instruments
Ulysses radial boom test
Ulysses sits atop the PAM-S and IUS combination
Illustration of Ulysses after deployment
Illustration of Solar Polar on IUS
1981 concept showing one of two ISPM probes orbiting the Sun
Ulysses after deployment from STS-41
Ulysses ' second orbit (1999–2004)
Animation of Ulysses 's trajectory from 6 October 1990 to 29 June 2009
Ulysses · Earth · Jupiter · C/2006 P1 · C/1996 B2 · C/1999 T1
STS-41 launches from Kennedy Space Center , 6 October 1990.
HeliophysicsCOSPAR IDSATCAT no.AstriumFriedrichshafenDornier SystemsSpace Shuttle DiscoverySTS-41Inertial Upper StageKennedy Space CenterLC-39BHeliocentric orbitPerihelion altitudeAphelion altitudeInclinationPeriodJupiterrobotic space probeEuropean Space AgencyNational Aeronautics and Space AdministrationNational Research Councilorbital inclinationplane of the Solar Systemlaunch vehiclegravity assistRadioisotope Thermoelectric GeneratorGPHS-RTGspacecrafttranslationOdysseusInfernoSpace ShuttleSTS-61-Floss of ChallengerDiscoverydish antennaFaraday cagespin-stabilisedwhip antennashydrazinemonopropellantSun sensorsconical scanningX-bandCassegrainRCA CDP1802beryllium copperdipolemonopole antennasiliconsolar flaresauroraemagnetometersmagnetic search coilelectronscosmic raysgravitational wavesDoppler shiftsradio occultationDust Experiment (DUST)interplanetaryinterstellar dusteclipticMariner 10Pioneer 11Voyagers 1 and 2Pioneer HGermanySpace Shuttle ChallengerCentaur G PrimeChallenger disasterBoeingMcDonnell DouglasPayload Assist Moduleyo-yo de-spunNew HorizonsHohmann transfer orbitC/2006 P1C/1996 B2C/1999 T1swing-by maneuvernorthernComet HyakutakeC/1999 T1 (McNaught-Hartley)coronal mass ejectionaphelionattitude controldesign lifeDownlinkS-bandbeamwidthhigh gain antennadata ratetrajectoryDeep Space Networkfreezeradioisotope thermal generatorstraveling-wave tube amplifiersgamma-rayInterPlanetary Networkgamma ray burstsmultilaterationasteroidsolar windhyperbolic trajectoryleave the Solar SystemAdvanced Composition ExplorerList of heliophysics missionsList of missions to the outer planetsParker Solar ProbeSolar and Heliospheric ObservatorySTEREOSolar OrbiterHerzberg Institute of AstrophysicsBibcodeGalvin, A.ScienceGalvin, A. 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