|
|
|
|
| DF-5 |
 |
|
|
|
 |
DF-5
Engines:
1. 4 × YF-20
2. 1 × YF-24
Total mass: 181,000 kg
Apogee: 1,000 km
Maximum
range: 12,020 km
Warhead: 3,000
kg/3.3 MT
Accuracy (CEP): 0.44
km
Operational Capability: 1981 |
|
|
|
| FB-1 |
 |
| CZ-2A |
|
|
|
|
 |
FB-1
Engines:
1. 4 × YF-20
2. 1 × YF-24
Total mass: 181,000 kg
Apogee: 200 km
Payload (LEO): 2,500
kg (200 km)
|
|
CZ-2A
Engines:
1. 4 × YF-20
2. 1 × YF-24
Total mass: 190,000 kg |
 |
Launches: 11 (Failures: 5)
/1972-1978/
(FB-1)
(CZ-2A) |
L
7
4 |
F
4
1 |
/1972-1981/
/1974-1978/ |
Payload:
(FB-1) FSW-0
(CZ-2A) JSSW, DDDS, SJ-2 |
 |
 |
FG-14 (retro motor) |
|
 |
Retired |
|
|
|
| CZ-2C |
|
|
|
|
|
| CZ-2C (2) |
|
| CZ-2C (2) SD |
|
| CZ-2C (2) CTS |
|
| CZ-2C (3) |
|
| CZ-2C (3) SMA |
|
|
|
|
|
| CZ-2C (3) YZ-1S |
|
|
|
|
|
|
|
CZ-2C (2) SD
Engines:
1. 4 × YF-20A
2. 1 × YF-24
1 × FG-47
|
|
CZ-2C (2) CTS
Engines:
1. 4 × YF-20A
2. 1 × YF-24
1 × SpaB-140C
|
|
CZ-2C (3) SMA
Engines:
1. 4 × YF-20A
2. 1 × YF-24
1 × FG-47
|
| Total mass: |
192,000 kg
213,000 kg |
(2C)
(2C SD) |
|
| |
| Apogee: |
200 km
1,000 km |
(CZ-2C)
(CZ-2C SD) |
|
| |
| Payload: |
| (LEO) |
2,500 kg
2,800 kg |
(2C)
(2C SD) |
|
| |
| (SSO) |
750 kg
1,400 kg
2,000 kg |
(2C)
(2C SD)
(2C YZ-1S) |
|
| |
| (MoO) |
| 500 kg |
(2C (3)) |
|
|
|
Launches: 102 (Failures: 2)
/1982-2026/
| |
L |
F |
|
| ( ) |
19 |
|
/1982-1993/ |
| |
(2)
(2) SD
(2) CTS |
2
7
2 |
|
/2004/
/1997-1999/
/2003-2004/ |
| |
(3)
(3) SMA
(3) YZ-1S |
59
3
10 |
2 |
/2004-2026/
/2008-2018/
/2018-2026/ |
Payload:
( ) FSW-0, FSW-1
(2) SY, NS
(2 SD) Iridium
(2 CTS) TC, Double Star
(3) 4FSW-4, SJ, HY, Yaogan, HJ, DF-ZF, × JS, Chinese FOBS, Yinhe, Siwei Gaojing, GeeSAT, APStar, Horus, Aomen Kexue, MisrSat, Einstein Probe, SVOM, CATCH, PIESAT, Shi Jian, AlSat
(3 SMA) HJ, SJ, PRSS, PakTES
(3 YZ-1S) Yaogan, RSW, Hulianwang Jishu Shiyan, HY |
|
|
FG-14 (retro motor)
FG-23 (retro motor) |
|
|
 |
In service |
|
|
|
| CZ-2D |
|
| CZ-2D (2) |
|
|
|
|
|
|
CZ-2D (2)
Engines:
1. 4 × YF-21B
2. 1 × YF-24B
| Total mass: |
| 232,250 kg |
(2D) |
|
| |
| Apogee: |
| 200 km |
(2D) |
|
| |
| Payload: |
| (LPEO) |
| 2,750 kg |
(2D) |
|
| |
| (SSO) |
| 2,000 kg |
(2D) |
|
| |
|
|
Launches: 105 (Failures: 1)
/1992-2026/
·
(2)
(2) YZ-3 |
L
3
98
4 |
F
1 |
/1992-1996/
/2003-2026/
/2018-2024/ |
Payload:
( ) FSW-2
(2) FSW-3, SJ, Yaogan, TH, SY, CX, VRSS (Francisco Miranda), Göktürk 2, Gaofen, TurkSat-3USat, CubeBug, NEE Pegaso, Jilin Optical, Jilin Video, DAMPE (Wukong), QSS (Mozi), Lixing, 3Cat, Yunhai, TanSat , Spark, GaoJing, GaoJing, BY70, VRSS (Antonio José de Sucre), LKW, SLS, Zhangheng, ÑuSat, GOMX 4A, Luojia, × JS, CHASE (Xihe), Tianhui, Beijing, ASO, Luojia, Qilu, Sixiang, Siwei Gaojing, PIESAT, PAK-EO, Tianlu, Lantan, Hulianwang Jishu Shiyan, Taikong Jisuan
(2 YZ-3) Hongyan, Yunhai-2, Gaosu Jiguang Zuanshi |
|
| |
FG-23 (retro motor) |
|
|
In service |
|
|
|
| CZ-2E |
|
|
|
|
CZ-2E
Total mass: 460,000 kg
Payload:
(LEO)
(GSTT) |
9,200
kg (200 km)
3,370
kg |
|
|
Launches: 7 (Failures: 2)
/1990-1995/
|
Payload: Badr, Optus, APStar, EchoStar |
 |
|
R-4D
LEROS × 2 |
|
|
Retired |
|
|
|
|
|
|
| CZ-2F |
|
| CZ-2F / G |
|
| CZ-2F / T |
|
|
|
|
|
CZ-2F
Engines:
0. 4 × YF-20B
1. 4 × YF-20B
2. 1 × YF-24B
Total mass: 498.400
kg
Payload (LEO): 8,080
kg (185 km) |
|
CZ-2F G
Engines:
0. 4 × YF-20B
1. 4 × YF-20B
2. 1 × YF-24B
Total mass: 495.900
kg
Payload (LEO): 8.600
kg (185 km) |
|
Launches: 28 (Failures: 0)
/1999-2026/
( )
(T)
(G) |
L
7
5
16 |
F |
/1999-2008/
/2011-2023/
/2011-2026/ |
Payload:
( ) Shenzhou 1-7
(G) Shenzhou 8-13
(T) Tiangong, Chongfu Shiyong Shiyan Hangtian Qi |
|
|
In service |
|
|
|
| CZ-3 |
|
|
|
|
CZ-3
Engines:
1. 4 × YF-20A
2. 1 × YF-24
3. 1 × YF-73 | H-8
Total mass: 204,000 kg
Payload:
(LEO)
(GSTT) |
4,800 kg (200 km)
1,400 kg |
|
|
Launches: 13 (Failures: 3)
/1984-2000/
|
Payload: DFH (STTW), AsiaSat, APStar, ZX, FY |
|
|
FG-15
FG-15B
FG-36
Star-30C / CBP |
|
|
Retired |
|
|
|
| CZ-3A |
|
|
|
|
CZ-3A
Engines:
1. 4 × YF-20B
2. 1 × YF-24B
3. 2 × YF-75 | H-18
Total mass: 241,000 kg
Payload:
(LEO)
(SSO)
(GSTT)
(IPT) |
6,200
kg (200 km)
5,000
kg
2,600 kg
1,420 kg |
|
|
Launches: 27 (Failures:0)
/1994-2018/
|
Payload: KF, DFH-3, FH-1, BD-1, ST-1, FY-2, BD-2, Sinosat, Chang'e, FY-2 |
|
|
Retired |
|
|
|
| CZ-3B |
|
|
|
|
|
| CZ-3B / G1 |
|
| CZ-3B / G2 |
|
| CZ-3B / G3 |
|
| CZ-3B / G5 |
|
| CZ-3B / G3Z YZ-1 |
|
|
|
|
|
CZ-3B
Total mass: 425,800 kg
| Payload: |
| (LEO) |
| 11,200
kg |
|
|
| |
| (SSO) |
5,700
kg
6,900 kg
6,900 kg
6,900 kg
6,900 kg |
(3B)
(3B/G1)
(3B/G2)
(3B/G2Z)
(3B/G3Z) |
|
| |
| (GSTT) |
5,100 kg
5,500 kg
5,500 kg
5,400 kg
5,200 kg
5,500 kg |
(3B)
(3B/G1)
(3B/G2)
(3B/G3Z)
(3B/YZ1)
(3BG3) |
|
| |
| (GSO) |
| 2,000 kg |
(3B) |
|
| |
| (IPT) |
3,300 kg
3,500 kg |
(3B)
(3B/G3Z) |
|
|
|
|
|
Launches: 115 (Failures: 3)
/1999-2025/
( )
(G1)
(G2)
(G3)
(G3Z YZ-1)
(G5) |
L
10
2
48
38
15
2 |
F
2
1 |
/1999-2008/
/2012/
/2007-2025/
/2011-2025/
/2015-2013/
/2020-2025/ |
Payload:
( ) Intelsat, Agila, APStar, Zhongwei, Sinosat, APStar, ZX, Palapa
(G1) BD-2
(G2) NIGCOMSAT, FY, VENESAT, ZX, Paksat, TJS, Eutelsat, APStar, Tiantong, Túpac KatariBelintersat,, BD-3, APSta, LaoSat, Gaofen, SJ, Alcomsat, APStar, ChinaSat, Palapa, PStar, JS, TJS, ZX, Shiyan, SY, PakSAT, Tianwen, Shi Jian
(G2 YZ-1) Chang'e
(G3) FH, ST, Tiantong, FY, BD, ZX, TL, TJS, Gaofen, Tiantong, HWGGW, Zhihui Tianwang, HG
(G5) Gaofen
(G3Z YZ-1) BD-3 |
|
|
LEROS
R-4D
S400 |
|
| |
|
(G1) |
|
| |
FY-25 |
| DFH-3 Bus |
| |
 |
(G2) |
|
| Electric |
| DFH-4 Bus |
| |
|
(G3) |
|
| |
( ? )
FY-25 |
| SAST-500
| DFH-3 Bus |
|
|
| Electric |
| DFH-4 Bus |
|
|
In service |
|
|
|
|
|
|
| CZ-3C |
|
| CZ-3C / G2 |
|
| CZ-3C / G3Z YZ-1 |
|
|
|
|
|
CZ-3C
Payload:
(LEO)
(GSTT)
(IPT) |
9,100 kg
3,800 kg
2,300 kg |
Total mass: 345,000
kg |
|
Launches: 21 (Failures: 0)
/2008-2025/
( )
(G2)
(G3Z) YZ-1 |
L
11
7
3 |
F |
/2008-2016/
/2014-2025/
/2015-2016/ |
Payload:
( ) TL-1, BD-2, Chang'e
(G2) Chang'e, BD-2, TL-1, TJS
(G3Z YZ-1) BD-3, Shiyan |
|
|
LEROS
R-4D
S400 |
|
| |
|
(G1) |
|
| |
FY-25 |
| DFH-3 Bus |
| |
|
(G3) |
|
| |
( ? )
FY-25 |
| SAST-500
| DFH-3 Bus |
|
|
In service |
|
|
|
|
|
| Total mass: |
239,600 kg
244,950 kg
246,000 kg
246,000 kg |
(4)
(4B)
(4B+)
(4C) |
|
| |
| Apogee: |
200 km
1,000 km
1,000 km |
(4)
(4B)
(4C) |
|
| |
| Payload: |
| (LEO) |
4,000 kg
4,200 kg
4,200 kg |
(4)
(4B)
(4C) |
|
| |
| (SSO) |
2,100 kg
2,230 kg
2.950 kg
2,950 kg |
(4)
(4B)
(4B+)
(4C) |
|
| |
|
|
Launches: 116 (Failures:3)
/1988-2026/
(4)
(4B)
(4C) |
L
2
56
59 |
F
1
2 |
/1988-1990/
/2009-2025/
/2006-2026/ |
Payload:
(4) FY-1, QQW
(4B) FY-1, CBERS, ZY-1, ZY-2, ZY-3, SJ-6, SJ-16, Yaogan, HY-2, ZY-1, ZY-2, ZY-3, VesselSat, ÑuSat, HXMT, OVSi, HJ, SY, Tianhu, FY-3, Shi Jian
(4C) Yaogan, FY-3, SJ-15, SY, CX, HEAD, Daqi, Gaofen, Queqiao, DSLWP, HJ, ZY, XW, ZY, Ludi Tance, Tianhu, Feng Yun, Shiyan |
|
|
In service |
|
|
