NEXT SPACEFLIGHT

Status

Success

Hinotori

Launch Time
Sat Feb 21, 1981 00:30 UTC

Rocket

Mu-III S
ISAS
Status: Retired
Payload to LEO: 290 kg
Stages: 3
Strap-ons: 8

Mission Details

Hinotori

The main objective of the Astro A (Hinotori) mission was the detailed study of solar flares during solar maximum.

Wavelength scanning was achieved by the spacecraft revolution, with an offset pointing of the spin axis with respect to the sun. Investigations of both experiments each had a time resolution of 6 s. In addition, the following investigations were included: three solar flare X-ray monitors that recorded the time profile and spectrum of the X-ray flares in the range of 2 to 20 keV. a solar flare gamma-ray detector for the range 0.2 to 9.0 MeV, a particle detector that monitored electron flux above 100 keV. and plasma probes for the measurement of electron density and temperature.

Payloads: 1
Total Mass: 188.0 kg
Low Earth Orbit

Location

Mu Pad, Uchinoura Space Center, Japan

Stats

1981

18th orbital launch attempt

Institute of Space and Aeronautical Science

13th mission
1st mission of 1981
11th successful mission
6th consecutive successful mission

Mu-III

9th mission
1st mission of 1981
8th successful mission
6th consecutive successful mission