- Suisei probe
Infobox_Spacecraft
Name = Suisei
Caption = Spacecraft Suisei
Organization = ISAS (now part ofJapanese Aerospace Exploration Agency )
Major_Contractors =
Mission_Type = Flyby
Satellite_Of =Comet Halley
Launch = 1985-08-18,Uchinoura Space Center
Launch_Vehicle = M-3SII-2
Decay =
Mission_Duration =August 20 ,1992
Mass = 139.5 kg
NSSDC_ID = 1985-073A
Webpage = [http://www.isas.ac.jp/e/enterp/missions/complate/suisei.shtml Suisei]
Semimajor_Axis =
Eccentricity = -
Inclination =
Orbital_Period =
Apoapsis =
Periapsis = 151000 km (Comet Halley)
Orbits =Suisei (すいせい; Japanese for "Comet"), originally known as Planet-A, was an unmanned
space probe developed by theInstitute of Space and Astronautical Science (now part of theJapanese Aerospace Exploration Agency , or JAXA). It constituted a part of theHalley Armada together withSakigake , the Soviet/French Vega probes, the ESA Giotto and the NASAInternational Cometary Explorer , to exploreHalley's Comet during its 1986 sojourn through the inner solar system.pacecraft
Suisei was identical in construction and shape to Sakigake, but carried a different payload: a CCD
UV imaging system and asolar wind instrument.The main objective of the mission was to take UV images of the hydrogen
corona for about 30 days before and after Comet Halley's descending crossing of theecliptic plane . Solar wind parameters were measured for a much longer time period. Thespacecraft is spin-stabilized at two different rates (5 and 0.2 rpm).Hydrazine thrusters are used for attitude and velocity control;star and sun sensors are for attitude control; and a mechanically despun off-setparabolic dish is used for long rangecommunication .Launch
Suisei was launched on
August 18 ,1985 by M-3SII-2 launch vehicle fromKagoshima Space Center . It was sent on an intercept course with Comet Halley, after which it would remain in aheliocentric orbit for later use as long as it was viable.Halley encounter
Suisei began UV
observations inNovember 1985 , generating up to 6 images/day.The spacecraft encountered Comet Halley at 151,000 km on sunward side during
March 8 ,1986 , suffering only 2 dust impacts.Earth flyby
Fifteen burns of Suisei's 3 N motors during the period of April 5–10, 1987, yielded a 65 m/s velocity increase for a 60,000 km
Earth gravity assist swingby onAugust 20 ,1992 , although the craft was then lost behind the Sun for thesummer .The
hydrazine fuel was depleted onFebruary 22 ,1991 . Preliminary tracking indicated a 900,000 km flyby had been achieved.Other planned encounters
ISAS had decided during 1987 to guide Suisei to a
November 24 ,1998 , encounter with21P/Giacobini-Zinner , but due to depletion of the hydrazine, this, as well as plans to fly within several million kilometers of Comet55P/Tempel-Tuttle onFebruary 28 ,1998 , were cancelled.External links
* [http://www.isas.ac.jp/e/enterp/missions/complate/suisei.shtml Suisei]
* [http://solarsystem.nasa.gov/missions/profile.cfm?MCode=Suisei Suisei Mission Profile] by [http://solarsystem.nasa.gov NASA's Solar System Exploration]
* [http://stardust.jpl.nasa.gov/comets/susei.html Halley's Comet Flyby]
Wikimedia Foundation. 2010.