|
 |
H-2
Engines:
0. 2 × SRB
1. 1 × LE-7
2. 1 × LE-5A
Fairing:
4S
5S
4/4D |
|
H-2S
Engines:
0. 2 × SRB
1. 1 × LE-7
2. 1 × LE-5A
Fairing:
5S |
|
H-2+
Engines:
0. 2 × SRB
2 × SSR
1. 1 × LE-7
2. 1 × LE-5A
Fairing:
5/4D |
| Total mass: |
| 260,000 kg |
(H2) |
|
| |
| Apogee: |
| 200 km |
(H2) |
|
| |
| Payload: |
| (LEO) |
| 10,060 kg |
|
|
| |
| (GSTT) |
3,800 kg
3,930 kg
4,000 kg |
(H2) |
|
| (H2+) |
|
| (H2S) |
|
|
 |
Launches: 8 (Failures: 2)
/1994-1999/
(2)
(2+)
(2S) |
L
6
1
1 |
F
2 |
/1994-1998/
/1995/
/1999/ |
Payload:
(2) VE, OREX, ETS, ADEOS, JAS, TRMM, ETS-Chaser, ETS-Target, COMETS
(2+) SFU, GMS
(2S) MTSat |
|
 |
Retired |
|
| H-2A 202 |
 |
| H-2A 2022 |
|
| H-2A 2024 |
|
|
|
| H-2A 204 |
|
|
|
|
|
H-2A 202
Engines:
0. 2 × SRB-A
1. 1 × LE-7A
2. 1 × LE-5B
Fairing:
4S
5S
4/4D-LC |
|
H-2A 2022
Engines:
0.
1.
2. |
2 × SRB-A
2 × Castor-4AXL
1 × LE-7A
1 × LE-5B |
Fairing:
4S
5S |
|
H-2A 2024
Engines:
0.
1.
2. |
2 × SRB-A
4 × Castor-4AXL
1 × LE-7A
1 × LE-5B |
Fairing:
4S
5S
4/4D-LC |
|
H-2A 204
Engines:
0. 4 × SRB-A 1. 1 × LE-7A
2. 1 × LE-5B
Fairing:
4S
5S |
| Total mass: |
291.300 kg
322.500 kg
353.900 kg
444.900 kg |
(202)
(2022)
(2024)
(204) |
| |
| Apogee: |
| 300 km |
(2022) |
| |
| Payload: |
| (LEO) |
10,000 kg
11,730 kg |
(202)
(2022) |
| |
| (GSTT) |
3,800 kg
4,200 kg
4,700 kg
5,800 kg |
(202)
(2022)
(2024)
(204) |
| |
|
 |
|
|
Launches: 50 (Failures: 1)
/2001-2025/
(202)
(2022)
(2024)
(204) |
L
35
3
7
5 |
F
1 |
/2001-2025/
/2005-2007/
/2002-2008/
/2015-2021/ |
Payload:
(2020) VEP, LRE, ADEOS, WEOS, FedSat, Micro-Lab-Sat, GOSAT, SOHLA, SDS, SpriteSat, PRISM, Kagayaki, KKS, STARS, Planet C, IKAROS, DCAM, DCAM, UNITEC, Waseda-SAT, Negai, KSAT, QZS, IGS-Optical, IGS-Radar, IGS-Radar Spare, GCOM-W, GCOM-C, KOMPSat, Horyu, GPM-Core, ShindaiSat, TeikyoSat, OPUSAT, INVADER, ITF, ALOS, Rising, UNIFORM, SOCRATES, SPROUT, Himawari, Hayabusa, PROCYON, DESPATCH, Shin'en, ASTRO, ChubuSat, QZS, SLATS, KhalifaSat, Diwata, Al-Amal (EMM), JDRS, IGS-Radar, XRISM, SLIM, IGS-Optical
(2022 )MTSat, ALOS, SELENE, ALOSRstar
(2024) VEP, MDS, DASH, USERS, DRTS, IGS-Optical, IGS-Radar, MTSat, WINDS, Inmarsa
(2040) ETS, Telstar, DSN, QZS |
|
|
BT-4
R-4D
R-4D |
+ |
ion × 4
ion × 4
SPT-140 × 4 |
|
|
|
Retired |
|
|
| |
 |
H-2A 212
Engines:
|
Total mass: 406,000 kg |
Payload:
| (LEO) |
17,280 kg |
| (GSTT) |
7,500 kg |
|
|
H-2A 222
Engines:
|
 |
Never flown |
|
|
| H-2A 212 |
 |
|
|
|
|
| H-2B |
|
|
|
|
H-2B
Engines:
0. 4 × SRB-A
1. 2 × LE-7A
2. 1 × LE-5B
Total mass: 531,000 kg kg
Payload:
(LEO)
(GSTT) |
16,500 kg
8,000 kg |
|
|
Launches: 9 (Failures: 0)
/2009-2020/
 |
|
R-4D
HBT-5 |
× 2
× 2 |
|
|
Retired |
|
|
|
H-3
Engines:
0. none
2 × SRB-A3
4 × SRB-A3 |
(- - 0)
(- - 2)
(- - 4) |
1. 2 × LE-9
3 × LE-9 |
(- 2 -)
(- 3 -) |
2. 1 × LE-5B |
|
|
Total mass:
574,000 kg (24)
| Payload: |
| (SSO) |
| |
4,000 kg
4,000 kg
|
(22)
(24)
(30) |
|
| |
| (GSTT) |
| |
6,500 kg
2,100 kg
|
(22)
(24)
(30) |
|
| |
| Fairing: |
| |
|
(22)
(24)
(30) |
|
|
|
Launches: 6 (Failures: 1)
/2023-2025/
(22S)
(24S) |
L
5
1 |
F
1 |
/2023-2025/
/2025/ |
Payload:
(24S) ALOS, VEP, CE-SAT, TIRSAT, DSN, QZS
(24S) HTV-X |
|
|
R-4D × 2 |
|
 |
In service |
|
|
