Vehicle Overview
Note: Payload
performance and estimated cost provided for information only. If you are interested
in contracting for launch services, we recommend that you contact the service provider
directly using the information above.
| |
LEO Payload
(57 deg.) |
Estimated Launch Price |
Launch Mass |
| CZ-2F |
18,500
lbm
8,400 kg |
US
$45-55 M |
1,022
klbm
464,000 kg |
Vehicle Configuration (Note: engine performance values have been estimated)
| |
Stage
0 |
Stage
1 |
Stage
2 |
| Length |
50.2 ft
15.3 m |
90 ft
23.7 m |
50.9 ft
15.5 m |
| Diameter |
7.55 ft
2.3 m |
11.2 ft
3.4 m |
11.2 ft
3.4 m |
| Gross Mass |
90.4 klbm
41,000 kg |
433 klbm
196,500 kg |
202 klbm
91,500 kg |
Propellant
Propellant Mass |
N2O4 /
UDMH
83.3 klbm
37,800 kg |
N2O4 /
UDMH
412 lbm
187,000 kg |
N2O4 /
UDMH
190 klbm
86,000 kg |
Engine**
Thrust
Isp |
YF -
20B
183.5 klbf
816 kN
291 sec |
YF -
20B
734 klbf
3,256 kN
289 sec |
YF -
25/23
187 klbf
831 kN
425 sec |
| Number of Engines |
1 |
4 |
1 |
| Nominal Burn Time |
128 sec |
166 sec |
295
sec
|
** Note: Vacuum engine
performance unless otherwise specified.
|
