|
|
|
|
| L-4S |
 |
|
|
|
 |
Lambda L-4S
Engines:
0. 2 × SB-310
1. 1 × L7350
2. 1 × L735(1/3)
3. 1 × L500
4. 1 × L480S
Total mass: 9,400 kg
Payload (LEO): 26 kg |
 |
Launches: 5 (Failures: 4)
/1966-1970/
|
 |
Retired |
|
|
|
|
Mu-4S
Engines:
1. 8 × SB-310
1. 1 × M-10
2. 1 × M-20
1. 1 × M-30
1. 1 × M-40 |
|
Mu-3C
Engines:
1. 8 × SB-310
2. 1 × M-10
3. 1 × M-22-TVC
4. 1 × M-3A |
|
Mu-3H
Engines:
1. 8 × SB-310
2. 1 × M-13
3. 1 × M-22-TVC
4. 1 × M-3A |
|
Mu-3S
Engines:
1. 8 × SB-310
2. 1 × M-13-TVC
3. 1 × M-22-TVC
4. 1 × M-3A |
| Payload: |
| (LEO) |
|
180 kg
195 kg
300 kg |
(Mu 4S)
(Mu 3C)
(Mu 3H / 3 S) |
|
| |
| Apogee: |
6,500 km
3,500 km
1,000 km |
(Mu 4S)
(Mu 3C)
(Mu 3H / 3 S) |
|
| |
| Total mass: |
43,600 kg
41,600 kg
44,700 kg
49,300 kg |
(Mu 4S)
(Mu 3C)
(Mu 3H)
(Mu 3S) |
|
|
|
Launches: 15 (Failures: 2)
/1970-1984/
(4S)
(3C)
(3H)
(3S1) |
L
4
4
3
4 |
F
1
1 |
/1970-1972/
/1974-1979/
/1977-1979/
/1980-1984/ |
Payload:
(4S) SS, MS (Tansei), SS (Shinsei), REXS (Denpa)
(3C) MS (Tansei), SRATS (Taiyo) Corsa (Hakucho)
(3H) MS (Tansei), Exos (Kyokko, Jikiken)
(3S1) MS (Tansei), Astro (Hinotori, Tenma), Exos (Ohzora) |
|
|
Retired |
|
|
|
| Mu-3S2 |
|
|
|
|
|
Mu-3S2
Engines:
1. 2 × SB-735
2. 1 × M-13-TVC
3. 1 × M-23
4. 1 × M-3B Payload (LEO): 800 kg
Apogee: 1,400
km
Total mass: 61,700
kg |
|
Launches: 8 (Failures: 1)
/1985-1995/
|
Payload: MS (Sakigake), Planet (Suisei), Astro (Ginga, ASCA, Asuka), Exos (Akebono), Muses (Hiten, Hagoromo), Solar (Yohkoh), EXPRESS |
|
|
Retired |
|
|
|
| J-1 SRB |
|
|
|
|
|
J-1 SRBA (3Stage)
| Engines: |
1.
2.
3. |
4 ×
1 ×
1 × |
SRB A
M-23
none
M-3B |
Payload:
(LEO)
(GSTT) |
850 kg
600 kg |
Total mass: 91,500
kg
Apogee: 250 km |
|
Launches: 1 (Failures: 0)
/1996/
(SRB)
· 2 Stages
(SRBA)
· 3 Stages |
L
1
- |
F |
/1996/ |
|
|
Retired |
|
| |
|
|
|
| M - 5.1 |
|
|
|
|
| M - 5.2 |
|
|
|
|
C
|
Mu-5 (M-V)
Engines:
1. 1 × M-14
2. 1 × M-24 (M 5
1)
1 × M-25 (M 5
2)
3. 1 × M-34 |
Total mass: 61,700
kg
Payload:
| (LEO) |
1,800 kg (M 5.1)
1,850 kg (M 5.2) |
|
|
Launches: 7 (Failures:
1)
/1997-2006/
(M 5
1)
(M 5
2) |
L
3
4 |
F |
/1997-2000/
/2003-2006/ |
Payload:
(M 5.1) Muses (Haruka, HALCA), Planet (Nozomi), Astro
(M 5.2) Muses (Hayabusa), Astro (Suzaku, Akari), CUTE, APD, SSSat, Solar (Hinode), HITSAT, SSSat |
|
|
Retired |
|
|
|
| Epsilon CLPS |
|
| Epsilon 2 |
|
| Epsilon 2 CLPS
| |
|
|
|
C
|
Epsilon
Engines:
1. 2 × SRB-A3
2. 1 × M-34c
3. 1 × KM-V2b (Epsilon 1)
1 × KM-V2c (Epsilon 2)
4. none
1 × CLPS
Payload:
(LEO)
(SSO) |
1,200 kg
590 kg
|
(2)
(2) |
|
|
Launches: 5 (Failures: 1)
/2013-2022/
(CLPS)
(2)
(2 CLPS) |
L
1
1
4 |
F
1 |
/2013/
/2016/
/2018-2022/ |
|
Payload: EXCEED (SPRINT), ERG (SPRINT), ASNARO, RAPIS, ALE, Hodoyoshi, MicroDragon, OrigamiSat, AOBA-VEO, NEXUS, RAISE |
|
 |
In service |
|
|
|
|
|
| SS-520 |
|
|
|
|
|
|
|
|
| NL-520 |
 |
|
|
|
|
|
|
SS-520
Total mass: 2,600 kg
Payload: 3 kg
|
|
Orbital Launches: 2 (Failures: 1)
/2017-2018/
|
Payload: TRICOM (Cubesat) |
|
|
In service |
C
 |
Total mass: 3,400 kg
Payload: 10 kg
|
 |
Never flown |
|
|
|
| Kairos
| 
|
|
|
|
C
|
Kairos
Engines:
1. 1 × Stage 1
2. 1 × Stage 2
3. 1 × Stage 3
4. 1 × PBS
Total mass: 23,400 kg
Payload:
| (LEO) |
250 kg |
| (SSO) |
150 kg |
|
|
Launches: 2 (Failures: 2)
/2024/
|
Payload: CSICE, Tarara, Ishiki, SC-Sat, PARUS |
|
|
In service |
|
|
