Japanese solar satellite. One launch, 1991.08.30. X-ray imaging of Sun.
Gross mass: 420 kg (920 lb).
First Launch: 1991.08.30.
Number: 1 .
More... - Chronology...
Associated Countries
See also
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Mu The Japanese Mu launcher series provided a flexible all-solid propellant launch vehicle for access to space. It was the first Japanese launch vehicle designed from the start as an orbital launch vehicle. More...
Associated Launch Vehicles
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Mu The Japanese Mu launcher series provided a flexible all-solid propellant launch vehicle for access to space. It was the first Japanese launch vehicle designed from the start as an orbital launch vehicle. More...
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Mu-3S-II Japanese all-solid orbital launch vehicle. Four stage vehicle consisting of 2 x SB-735 + 1 x M-13 + 1 x M-23 + 1 x M-3B More...
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Mu-3 The Japanese Mu launcher series provided a flexible all-solid propellant launch vehicle for access to space. More...
Associated Manufacturers and Agencies
Bibliography
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McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
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JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: here.
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McDowell, Jonathan, Launch Log, October 1998. Web Address when accessed: here.
Associated Launch Sites
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Kagoshima Japanese launch center for solid fueled sounding rockets and satellite launchers. Limited to two months a year due to disturbance of local fisheries. More...
Solar Chronology
1991 August 30 - .
02:30 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima M.
Launch Pad: M1.
LV Family:
Mu.
Launch Vehicle:
Mu-3S-II.
LV Configuration: Mu-3S-II M-3S2-6.
- Solar-A - .
Payload: Yohkoh. Mass: 420 kg (920 lb). Nation: Japan. Agency: ISAS. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: Solar. Decay Date: 2005-09-12 . USAF Sat Cat: 21694 . COSPAR: 1991-062A. Apogee: 754 km (468 mi). Perigee: 516 km (320 mi). Inclination: 31.3000 deg. Period: 97.40 min. Summary: X-ray imaging of Sun..
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