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
(51.6 deg.) |
SSO Payload
(98.6 deg.) |
Estimated Launch Price |
Launch Mass |
| Kosmos 3M |
3300
lbm
1500 kg |
1700 lbm
775 kg |
US
$12 M |
240 klbm
109,000 kg |
* Performance provided
by AIAA "International Reference Guide to Space Launch
Systems" 3rd edition.
Vehicle Configuration (Note: engine performance values have been estimated)
| |
Stage 1 |
Stage 2 |
| Length |
73 ft
22.4 m |
19.7 ft
6.0 m |
| Diameter |
7.9 ft
2.4 m |
7.9 ft
2.4 m |
| Gross Mass |
192,550
lbm
87,200 kg |
44,390
lbm
20,135 kg |
Propellant
Propellant Mass |
Nitric
Acid + 27% N2O4 /
UDMH
180,560 lbm
81,900 kg |
Nitric
Acid + 27% N2O4 /
UDMH
41,225 lbm
18,700 kg |
Engine**
Thrust
Isp |
RD-216/11D614
392 klbf
1745 kN
291.3 sec |
11D49
35,300 lbf
157 kN
289 sec |
| Number of Engines |
1 |
1 |
| Nominal Burn Time |
130 sec |
500 sec |
** Note: Vacuum engine
performance unless otherwise specified.
|
