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H-IIA 202 | GCOM-W1
Mitsubishi Heavy IndustriesLaunch Successful

GCOM-W1

H-IIA 202

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Historical mission record

This page records H-IIA 202 | GCOM-W1 and its reported outcome: Launch Successful. The date above is a historical record.

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Mission status
Launch Successful

Status reported by the mission data provider.

LAUNCH SITETanegashima Space Center, Japan

Mission

The GCOM-W (Global Change Observation Mission - Water) or Shizuku satellite aims to construct, use, and verify systems that enable continuous global-scale observations (for 10 to 15 years) of effective geophysical parameters for elucidating global climate change and water circulation mechanisms. Water circulation changes will be observed by a microwave radiometer onboard the GCOM-W (Water) satellite (scheduled to be launched in Japan Fiscal Year 2011). The GCOM-W will observe precipitation, vapor amounts, wind velocity above the ocean, sea water temperatures, water levels on land areas and snow depths. Climate change observation will be performed by a multi-wavelength optical radiometer onboard the GCOM-C (Climate) satellite (under consideration) on clouds, aerosol, seawater color (marine organisms), vegetation, snow and ice. These satellites will enable us to perform comprehensive observations of the surface layer of the Earth such as the atmosphere, including clouds, land, oceans and the cryosphere. The Advanced Microwave Scanning Radiometer 2 (AMSR2) is a sensor to observe radiometers, or microwaves emitted naturally from the ground, sea surface and atmosphere, using 6 different frequency bands ranging from 7 GHz to 89 GHz. The strength of a natural microwave is determined by its characteristics and moisture, including the surface condition and temperature of the material. Although it depends on the frequency, the microwave is very weak. AMSR2 will detect such weak microwaves at an altitude of 700 kilometers and measure the strength of them with a very high accuracy. For example, by measuring the strength of a microwave emitted from the sea surface with the AMSR2, one can understand the water temperature of the sea surface to an accuracy of 0.5 degrees Celsius.

Launch vehicle
H-IIA 202
Mission type
Earth Science
Destination orbit
Sun-Synchronous Orbit
Launch pad
Yoshinobu Launch Complex LP-1
Provider
Mitsubishi Heavy Industries

The vehicle

Published configuration and flight history.

H-IIA 202
Mitsubishi Heavy Industries
Launch vehicle

H-IIA 202

H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch Akatsuki, which studied the planet Venus. Launches occur at the Tanegashima Space Center.

Height
53 m
Diameter
4 m
Stages
2
Recorded launches
35
First flight
2001-08-29

Recorded timing

This is a mission record, not an upcoming calendar appointment.

Instantaneous windowPublished target
SCHEDULED MOMENT

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Launch site & orbit

Tanegashima Space Center, Japan

The mission in perspective

Launch site & orbit

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NASA Blue Marble map of Earth's continents and oceans
Representative orbit · accelerated illustrationNo live tracking or simulated ascent. NASA Blue Marble.

Coverage & sources

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