H-II
Mitsubishi Heavy Industries
Manufacturer
Mitsubishi Heavy Industries
Family
H-II
Maiden flight
1994-02-03
Length
49 m
Diameter
4 m
Payload to LEO
10,060 kg
Payload to GTO
3,930 kg
Launches
7
Successful
6
The H-II rocket was a Japanese satellite launch system which flew seven times between 1994 and 1999 with 5 successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two stage liquid fuelled rocket Japan made using only domestic technologies.


H-IIFailure
MTSAT · Japan Aerospace Exploration Agency
Monday, Nov 15, 1999, 07:29 UTC

H-IISuccess
Kakehashi · Japan Aerospace Exploration Agency
Saturday, Feb 21, 1998, 07:55 UTC

H-IISuccess
TRMM & ETS 7 · Japan Aerospace Exploration Agency
Thursday, Nov 27, 1997, 21:27 UTC

H-IISuccess
Midori · Japan Aerospace Exploration Agency
Saturday, Aug 17, 1996, 01:53 UTC

H-IISuccess
SFU & Himawari 5 · Japan Aerospace Exploration Agency
Saturday, Mar 18, 1995, 08:01 UTC

H-IISuccess
Kiku-6 · Japan Aerospace Exploration Agency
Sunday, Aug 28, 1994, 07:50 UTC

H-IISuccess
Myojo & Ryusei · Japan Aerospace Exploration Agency
Thursday, Feb 3, 1994, 22:20 UTC
No media yet. Livestreams usually appear shortly before launch.