Taiyo

Launch Success

Liftoff Time (GMT)

05:25:00

Monday February 24, 1975

Mission Details

Taiyo

Wiki

SRATS, also called Taiyo, was an aeronomy research satellite. It had an octagonal column form (75 cm in diameter and 65 cm in height), in which the experiment instruments were mounted. The satellite was spin-stabilized in a rolling wheel mode by a geomagnetic attitude control system. Four plasma probes were extended perpendicular to the spin axis by 0.5-m metallic booms. Power at an average rate of 15 W was provided by 6000 silicon n-p solar cells. The objectives of the satellite were to study the ionosphere systematically by simultaneously observing solar ionizing radiations (hydrogen Lyman-Alpha and X-rays), the ultraviolet albedo of the earth, positive ion composition, and plasma parameters such as electron and ion densities and temperatures in the ionosphere.

Medium Earth Orbit

1 Payload

86 kilograms

Rocket

Retired
Mu-III C

Active 1974 to 1979

Institute of Space and Aeronautical Science logo

Agency

ISAS

Payload to Orbit

LEO: 195 kg

Stages

3

Strap-ons

8

Launch Site

Mu Pad

Uchinoura Space Center, Japan

Fastest Turnaround

143 days 23 hours

Stats

Mu-III


2nd

Mission

1st

Mission of 1975

Institute of Space and Aeronautical Science


6th

Mission

1st

Mission of 1975

1975


15th

Orbital launch attempt