NEXT SPACEFLIGHT

Status

Success

Himawari 4

Launch Time
Tue Sep 05, 1989 19:11 UTC

First, and last launch of H-I UM-129A (6SO).

Rocket

H-I UM-129A (6SO)
MHI
Status: Retired
Payload to LEO: 3,200 kg
Payload to GTO: 1,100 kg
Stages: 3
Strap-ons: 6
Rocket Height: 42.0 m
Fairing Diameter: 2.44 m

Mission Details

Himawari 4

The GMS, also called Himawari, built by Hughes Space and Communications Company (HSC) for Japan have provided uninterrupted monitoring of weather conditions since 1977 over more than 65 million square miles of the Pacific Basin - about one-third of the Earth's surface.

The principal instrument on board all satellites in the GMS series is the visible and infrared spin scan radiometer (VISSR), which is produced by Hughes' Santa Barbara Research Center. The spacecraft body carries the VISSR and spins at 100 rpm, while the antennas are despun and remain pointed toward Earth.

The spinning motion of the satellite carries the west-east scan. The north-south scan is produced by the VISSR scan mirror, which steps approximately 0.008° with each satellite revolution.

Visible spectrum information consists of reflected sunlight and is obtained when Earth's surface is illuminated by the sun. Infrared spectrum information consists of heat radiation from Earth's surface and cloud tops. Since this information contains very little sunlight reflection, it can be obtained day and night. Extremely sensitive detectors, which are kept cold by a radiative cooler, convert Earth's infrared radiation into analog signals.

Payloads: 1
Total Mass: 325.0 kg
Geostationary Transfer Orbit

Location

LA-Y1, Tanegashima Space Center, Japan

Stats

1989

71st orbital launch attempt

H-I

5th mission
1st mission of 1989
5th successful mission