H-2 (original) (raw)
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 H-2 (ETS 6) [NASDA] |
 H-2 (TRMM / ETS 7) [NASDA] |
 H-2 (ADEOS 1) [NASDA] |
|---|
→ all H-2 launches
→ all launches of H-2 / H-2A family vehicles
| Version | Strap-On | Stage 1 | Stage 2 |
|---|---|---|---|
| H-2 (2 × SRB) | 2 × SRB | LE-7 | LE-5A |
| Performance (kg) | LEO | LPEO | SSO | GTO | GEO | MolO | IP |
|---|---|---|---|---|---|---|---|
| H-2 (2 × SRB) | 3800 |
No: TNr: Serial: Type: Fair Date: LS Payload
1 1 TF1 H-2 4S 03.02.1994 Ta YLP-1 VEP / OREX 2 2 TF2 H-2 4S 28.08.1994 Ta YLP-1 ETS 6 [LAPS] 4 3 4F H-2 5S 17.08.1996 Ta YLP-1 ADEOS 1 / JAS 2 5 4 6F H-2 4/4D 27.11.1997 Ta YLP-1 TRMM / ETS-7-Chaser / ETS-7-Target 6 5 5F H-2 4S 21.02.1998 Ta YLP-1 P COMETS
Failures:
Flight 2: LAPS apogee kick motor failed to ignite Flight 6: Stage 2 shorter than planned burn
Launch sites:
Ta = Tanegashima Space Center, Tanegashima, Japan 