Payload Performance
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
(65 deg., 200 km) |
Estimated Launch Price |
Configuration |
Launch Mass |
Rockot
(RS-18) |
4,100 lb
1,850 kg |
US $10-13 M |
Three Stage Storable
Propellant |
235,000 lb
107,000 kg |
* Performance provided by
Eurockot.
Vehicle Configuration
| |
Stage 1 |
Stage 2 |
Stage 3
(Breeze-KM) |
| Length |
56.4 ft
17.2 m |
20.0 ft
6.1 m |
4.3 ft
1.3 m |
| Diameter |
8.2 ft
2.5 m |
8.2 ft
2.5 m |
8.2 ft
2.5 m |
| Gross Mass |
170,115 lb
77,150 kg |
26,890 lb
12,195 kg |
14,480 lbm
6,565 kg |
Propellant
Propellant Mass |
N2O4 / UDMH
157,560 lb
71,455 kg |
N2O4 / UDMH
23,615 lb
10,710 kg |
N2O4 / UDMH
10,950 lbm
4,965 kg |
Engine**
Thrust
Isp |
RD-0233
420,400 lbf
1,870 kN
310 sec |
RD-0235
54,000 lbf
240,000 N
320 sec |
S5.98M
4,410 lbf
19,620 N
325.5 sec |
| Number of Engines |
4 |
1 |
1 |
| Nominal Burn Time |
121 sec |
155 sec |
1,000 sec
max |
|
