Hinotori

Launch Success

Liftoff Time (GMT)

00:30:00

Saturday February 21, 1981

Mission Details

Hinotori

Wiki

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.

Low Earth Orbit

1 Payload

188 kilograms

Rocket

Retired
Mu-III S

Active 1980 to 1984

Institute of Space and Aeronautical Science logo

Agency

ISAS

Payload to Orbit

LEO: 290 kg

Stages

3

Strap-ons

8

Launch Site

Mu Pad

Uchinoura Space Center, Japan

Fastest Turnaround

143 days 23 hours

Stats

Mu-III


9th

Mission

1st

Mission of 1981

Institute of Space and Aeronautical Science


13th

Mission

1st

Mission of 1981

1981


18th

Orbital launch attempt