ORBITAL 轨道桥
UTC --:--:--

Rockets / Mitsubishi Heavy Industries

H-IIA

H-IIA 202 · Mitsubishi Heavy Industries · retired

Total launches
35
all time
Success rate
0.0%
35 of 35
Failed
0
all time
Pending
0
0 on the board
About this vehicle

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.

Source: Launch Library 2 record #32 · Wikipedia

Specifications
Manufacturer
Mitsubishi Heavy Industries
Status
Retired / inactive
Reusable
No
Maiden flight
2001-08-29
Height
53 m
Diameter
4 m
Liftoff mass
285 t
Thrust
2,260 kN
Stages
2
Payload to LEO
10,000 kg
Payload to GTO
4,100 kg
Launch cost
90000000

Next flights on this rocket

Full launch board
no upcoming flights for this vehicle right now

Where it flies from

Launch pads carry their own coordinates and flight history.

Open the pad list →