/
Launch Success
Liftoff Time (GMT)
02:30:00
Friday August 30, 1991
The objective of Solar A or Yohkoh (Japanese for sunbeam) is to study the high-energy radiations from solar flares (hard and soft X-rays and energetic neutrons) as well as quiet structures and pre-flare conditions. The mission is a successor to Hinotori, a previous Japanese spacecraft flown at the previous solar activity maximum in 1981. Yohkoh is a three-axis stabilized observatory-type satellite in a nearly-circular Earth orbit, carrying four instruments: two imagers and two spectrometers. The spacecraft is a rectangular solid about 2 m square and 4 m long. The imaging instruments have almost full-Sun fields of view, to avoid missing any flares on the visible disk of the Sun. Approximately 50 MB of data are accumulated per day, and stored on an on-board tape recorder with 10.5 Mbyte capacity. The Yohkoh mission is a cooperative mission of Japan, the US, and the United Kingdom.
Low Earth Orbit
1 Payload
390 kilograms
17th
Mission
1st
Mission of 1991
21st
Mission
1st
Mission of 1991
64th
Orbital launch attempt