Yohkoh

Launch Success

Liftoff Time (GMT)

02:30:00

Friday August 30, 1991

Mission Details

Yohkoh

Wiki

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

Rocket

Retired
Mu-III S2

Active 1985 to 1995

Institute of Space and Aeronautical Science logo

Agency

ISAS

Payload to Orbit

LEO: 770 kg

Stages

4

Strap-ons

2

Launch Site

Mu Pad

Uchinoura Space Center, Japan

Fastest Turnaround

143 days 23 hours

Stats

Mu-III


17th

Mission

1st

Mission of 1991

Institute of Space and Aeronautical Science


21st

Mission

1st

Mission of 1991

1991


64th

Orbital launch attempt