Suisei probe

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Susei probe

Suisei (the Japanese name meaning 'Comet') was launched on August 18, 1985, by M-3SII-2 launch vehicle from Kagoshima Space Center into heliocentric orbit to fly by Comet 1P/Halley. It constituted "Halley Armada" together with VEGA, GIOTTO, ICE, and SAKIGAKE to explore Halley's comet when it made its closest encounter with the sun. It was identical to Sakigake apart from its payload: a CCD UV imaging system and a solar 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 the ecliptic plane. Solar wind parameters were measured for a much longer time period. The spacecraft 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-set parabolic dish is used for long range communication. Suisei began UV observations in November 1985, generating up to 6 images/day. The spacecraft encountered Comet 1P/Halley at 151,000 km on sunward side during March 8, 1986, suffering only 2 dust impacts. Fifteen burns of Suisei's 3 N motors over 5--10th of April 1987 yielded a 65 m/s velocity increase for a 60,000 km Earth gravity assist swingby on August 20, 1992, although the craft was then lost behind the Sun for the summer. The hydrazine was depleted on 22 February, 1991. Preliminary tracking indicated a 900,000 km flyby had been achieved. ISAS had decided during 1987 to guide Suisei to a November 24, 1998 encounter with 21P/Giacobini-Zinner, but due to depletion of the hydrazine, this, as well as plans to fly within several million kilometers of Comet 55P/Tempel-Tuttle on February 28, 1998 has been cancelled.

Weight: 140 kg Orbit : Heliocentric International Index: 1985-073A


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Template:Halley Armadade:Suisei it:Suisei hu:Suisei ja:すいせい (探査機) pt:Sonda Suisei sv:Suisei (rymdsond)