H-IIA

H-IIA is a 2-stage H-II rocket built by Mitsubishi Heavy Industries.

H-IIA cover image

Specifications

Height
53 m
Diameter
4 m
Mass
445000 kg
Stages
2
Thrust
2260 kN
LEO payload
—
First flight
Dec 18, 2006

Manufacturer & operator

Family
H-II
Variant
204
Manufacturer
Mitsubishi Heavy Industries
Operator
—
Country
Japan

Launch sites

  1. Tanegashima Space Center, Japan (5 launches)

Launch history

5 launches to date.

H-IIA 204 | Inmarsat-6 F1 cover imageSUCCESS
H-IIA

H-IIA 204 | Inmarsat-6 F1

Dec 22, 2021 UTC

Tanegashima Space Center, Japan

Mitsubishi Heavy Industries
H-IIA 204 | Michibiki 3 (QZS-3) cover imageSUCCESS
H-IIA

H-IIA 204 | Michibiki 3 (QZS-3)

Aug 19, 2017 UTC

Tanegashima Space Center, Japan

Mitsubishi Heavy Industries
H-IIA 204 | DSN 2 (Kirameki 2) cover imageSUCCESS
H-IIA

H-IIA 204 | DSN 2 (Kirameki 2)

Jan 24, 2017 UTC

Tanegashima Space Center, Japan

Mitsubishi Heavy Industries
H-IIA 204 | Telstar 12 VANTAGE cover imageSUCCESS
H-IIA

H-IIA 204 | Telstar 12 VANTAGE

Nov 24, 2015 UTC

Tanegashima Space Center, Japan

Mitsubishi Heavy Industries
H-IIA 204 | Kiku-8 cover imageSUCCESS
H-IIA

H-IIA 204 | Kiku-8

Dec 18, 2006 UTC

Tanegashima Space Center, Japan

Japan Aerospace Exploration Agency

Last updated: