| Design Features |
- |
| Core Stages |
2 |
| Strap-on Boosters |
4 |
| Length |
53.075 m |
| Diameter |
3.35 m |
| Gross Mass |
597 t |
| Lift-off Thrust |
7200 kN |
| Payload Capacity |
13.5 t (LEO) or 5.5 t (SSO) |
| First flight |
25 June 2016 |
| Launch centre |
Wenchang |
|
| Stage |
1st Stage K3 |
Strap-on boosters K2 |
2nd Stage (CZ-8) |
| Length (m) |
25.083 m |
26.903 m |
12.375 m |
| Diameter (m) |
3.35 m |
2.25 m |
3 m |
| Engine |
2x YF-100 |
1x YF-100 |
2x YF-75 |
| Mass (Gross) (kg) |
N/A |
N/A |
N/A |
| Thrust (kN) |
2400 kN (sea-level) |
1200 kN (sea-level) |
167 kN (vacuum) |
| Propellants |
RP-1 / LOX |
RP-1 / LOX |
LH2 / LOX |
| Stage |
Payload fairing |
| Length (m) |
12.5 m |
| Diameter (m) |
4.2 m |
|