H-IIA 204 | Inmarsat-6 F1

H-IIA 204 | Inmarsat-6 F1

Yoshinobu Launch Complex LP-1
Tanegashima Space Center, Japan

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Mitsubishi Heavy Industries

Mitsubishi Heavy Industries, Ltd. is a Japanese multinational engineering, electrical equipment and electronics company headquartered in Tokyo, Japan. MHI is one of the core companies of the Mitsubishi Group. MHI's products include aerospace components, air conditioners, aircraft, automotive components, forklift trucks, hydraulic equipment, machine tools, missiles, power generation equipment, printing machines, ships and space launch vehicles. Through its defense-related activities, it is the world's 23rd-largest defense contractor measured by 2011 defense revenues and the largest based in Japan.

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Inmarsat-6 F1

Inmarsat-6 is the sixth generation of satellites for the London-based global mobile satellite communications operator Inmarsat. It consists of a dual mission to augment both L-band and Ka-band Global Xpress services. Airbus Defence and Space has been awarded a contract by Inmarsat to design and develop the first two Inmarsat-6 (I-6) mobile communications satellites, creating the most versatile mobile services satellites in its fleet. The two I-6 satellites are based on Airbus Defence and Space's Eurostar platform in its E3000e variant, which exclusively uses electric propulsion for orbit raising. The satellites take advantage of the reduction in mass that this electric propulsion technology enables for a dual payload mission, with an exceptionally large next generation digitally processed payload. I-6 F1 and F2 both carry a large 9 m aperture L-band antenna and nine multibeam Ka-band antennas, and feature a high level of flexibility and connectivity. A new generation modular digital processor provides full routing flexibility over up to 8000 channels and dynamic power allocation to over 200 spot beams in L-band. Ka-band spot beams are steerable over the full Earth disk, with flexible channel to beam allocation.

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H-IIA 204


Height 53.00 Meters

Max Stages 2

Mass To GTO 6000 kg

Liftoff Thrust 2260 kN

Diameter 4.00 Meters

Mass To LEO 0 kg

Liftoff Mass 445 Tonnes


Launch Success 5

Consecutive Success 5

Maiden Flight 2006-12-18

Launch Failures 0


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Updates

SwGustav

2021-12-22T18:26:39+0000

Successful launch confirmed by Inmarsat

Source

Cosmic_Penguin

2021-12-19T06:43:33+0000

One day slip due to weather forecasts.

Source

Nosu

2021-12-18T22:41:13+0000

T-0 confirmed

Source

Cosmic_Penguin

2021-11-04T03:38:28+0000

Launch date and window announced.

Source

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