Yohkoh

Yohkoh
Artist concept of the Japanese Yohkoh spacecraft
NamesSolar-A (before launch
Mission typeHeliophysics
OperatorISAS / NASA / PPARC
COSPAR ID1991-062A Edit this at Wikidata
SATCAT no.21694
WebsiteYohkoh home page
Mission duration10 years, 3 months and 14 days (achieved)
Spacecraft properties
Launch mass390 kilograms (860 lb)
Dimensions2 m (6 ft 7 in) x 2 m (6 ft 7 in) x 4 m (13 ft)
Start of mission
Launch date02:30, 30 August 1991 (UTC) (1991-08-30T02:30Z)
RocketMu-3S-II
Launch siteKagoshima M1
End of mission
DisposalSpacecraft lost accidentally
Last contact14 December 2001
Decay date12 September 2005
Orbital parameters
Reference systemGeocentric
Perigee altitude516 kilometres (321 mi)
Apogee altitude754 kilometres (469 mi)
Inclination31.3°
Period97.4 min

Yohkoh (Japanese: ようこう, 'Sunbeam'), known before launch as Solar-A, was a Solar observatory spacecraft of the Institute of Space and Astronautical Science (Japan), in collaboration with space agencies in the United States and the United Kingdom. It was launched into Earth orbit on August 30, 1991 by the M-3SII rocket from Kagoshima Space Center. It took its first soft X-ray image on 13 September 1991, 21:53:40,[1] and movie representations of the X-ray corona over 1991-2001 are available at the Yohkoh Legacy site.

  1. ^ Ogawara, Yoshiaki; Acton, Loren W.; Bentley, Robert D.; Bruner, Marilyn E.; Culhane, J. Leonard; Hiei, Eijiro; Hirayama, Tadashi; Hudson, Hugh S.; Kosugi, Takeo; Lemen, James R.; Strong, Keith T.; Tsuneta, Saku; Uchida, Yutaka; Watanabe, Tetsuya; Yoshimori, Masato (1992). "The status of YOHKOH in orbit - an introduction to the initial scientific results". Publications of the Astronomical Society of Japan. 44: L41. Bibcode:1992PASJ...44L..41O.

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