|
|
 |
DF-3
Engines:
1. 4 × YF-2A
Total mass: 64,000 kg
Apogee: 500 km
Maximum range: 2,660 km
Warhead: 2,140 kg / 3.3 MT
Accuracy (CEP): 0.87 km
First Launch: 1966
Operational Capability: 1971
|
|
|
|
| DF-3 |
 |
|
|
|
|
|
| DF-4 |
|
|
|
|
DF-4
Engines::
1. 4 × YF-2A
2. 1 × YF-2A
Total mass: 82,000 kg
Apogee: 500 km
Maximum range: 4,760 km
Warhead: 2,190 kg / 3.3 MT
Accuracy (CEP): 1.19 km
First Launch: 1969
Operational Capability: 1981
|
|
|
|
| CZ-1 |
 |
|
|
|
|
| CZ-1D |
|
|
|
|
 |
CZ-1
Engines:
1. 4 × YF-2A
2. 1 × YF-2A
2. 1 × GF-02
Total mass: 81,310 kg
Payload mass:
(LEO) 300 kg (440
km) |
 |
CZ-1D
Engines:
1. 4 × YF-2A
2. 1 × YF-3
2. 1 × CZ-1D-3
Total mass: 79,400 kg
Apogee: 300 km
Payload mass:
(LEO) 740 kg (300 km) |
 |
Launches: 3 (Failures: 1)
/1970-2002/
(1)
(1D) |
O
2 |
S
1
3 |
F
1 |
/1970-1971/
/1995-2002/ |
Payload:
(1) DFH, SJ
(1D) Reentry Test |
|
 |
Retired |
|
|
Retired |
 |
|
|
|
|
