H-II
Mitsubishi Heavy Industries
Hersteller
Mitsubishi Heavy Industries
Familie
H-II
Erstflug
1994-02-03
Länge
49 m
Durchmesser
4 m
Nutzlast LEO
10.060 kg
Nutzlast GTO
3.930 kg
Starts
7
Erfolgreich
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
Montag, 15.11.1999, 07:29 UTC

H-IISuccess
Kakehashi · Japan Aerospace Exploration Agency
Samstag, 21.02.1998, 07:55 UTC

H-IISuccess
TRMM & ETS 7 · Japan Aerospace Exploration Agency
Donnerstag, 27.11.1997, 21:27 UTC

H-IISuccess
Midori · Japan Aerospace Exploration Agency
Samstag, 17.08.1996, 01:53 UTC

H-IISuccess
SFU & Himawari 5 · Japan Aerospace Exploration Agency
Samstag, 18.03.1995, 08:01 UTC

H-IISuccess
Kiku-6 · Japan Aerospace Exploration Agency
Sonntag, 28.08.1994, 07:50 UTC

H-IISuccess
Myojo & Ryusei · Japan Aerospace Exploration Agency
Donnerstag, 03.02.1994, 22:20 UTC
Noch keine Medien vorhanden. Livestreams erscheinen meist kurz vor dem Start.