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
(46.2°, 200 km) |
LEO Payload
(87.1°, 200 km) |
SSO Payload
(98.6°, 800 km) |
Estimated Launch Price |
Dnepr 1
(RS-20) |
9,920 lbm
4,500 kg |
6,390
lbm
2,900 kg |
330 lbm
150 kg |
US $10-13 M |
Dnepr M
(RS-20) |
9,260 lbm
4,200 kg |
2,500 lbm
5,510 kg |
2,650 lbm
1,200 kg |
US
$10-20 M |
* Performance provided by
AIAA, "International Reference Guide to Space Launch
Systems", 3rd edition.
Vehicle Configuration
| |
Stage 1 |
Stage 2 |
Stage 3
(R-36M2) |
| Length |
73.3 ft
22.3 m |
18.7 ft
5.7 m |
3.3 ft
1.0 m |
| Diameter |
9.8 ft
3.0 m |
9.8 ft
3.0 m |
9.8 ft
3.0 m |
| Gross Mass |
464,700
lbm
210,800 kg |
108,700 lbm
49,300 kg |
18,000 lbm
8,200 kg |
Propellant
Propellant Mass |
N2O4 / UDMH
? lbm
? kg |
N2O4 / UDMH
? lbm
? kg |
N2O4 / UDMH
? lbm
? kg |
Engine**
Thrust
Isp |
RD-0233
1,017,000 lbf
4,525 kN
? sec |
RD-0235
170,000 lbf
760,000 N
? sec |
S5.98M
4,200 lbf
18,600 N
? sec |
| Number of Engines |
4
thrust chambers |
1 + 4
verniers |
1
(multiple chambers + ? verniers) |
| Nominal Burn Time |
? sec |
? sec |
? sec |
|
