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*
(11.3°, 200 km circular) |
LEO Payload*
(53°, 200 km circular) |
LEO Payload*
(90°, 200 km circular) |
LEO Payload*
(98°,
200 km circular) |
GTO*)
(200 x 35786 km @ 11.3° incl) |
GEO*
(0° incl). |
| Avrora |
12,000
kg
26,450 lbm |
9,800
kg
21,600 lbm |
95,00
kg
20,940 lbm |
9,200
kg
20,275 lbm |
--- |
--- |
| Avrora / Korvet |
--- |
--- |
--- |
--- |
4,350
kg
9587 lbm |
2,100
kg
4,625 lbm |
* Performance values from
APSC website
Vehicle Overview
| |
Strap-On
Boosters
(4 Total) |
Stage
2
(Core) |
Stage
3
(Blok E) |
Stage
4
(Korvet) |
| Length |
64.3 ft
19.6 m |
--- |
--- |
--- |
| Diameter |
8.8 ft
2.7 m |
7.1 to 9.7 ft
2.15 to 2.95 m |
--- |
--- |
| Gross Mass |
94,200 lb
42,750 kg |
337,000
lb***
153,000 kg*** |
--- |
--- |
Propellant
Propellant Mass |
LOX / RP
86,400 lb
39,200 kg |
LOX /
RP
318,000 lb***
144,500 kg*** |
LOX / RP
--- |
LOX / RP
--- |
Engine**
Thrust
Isp |
RD-107A
223,000 lbf
991.7 kN
314 sec |
NK-33
339,000 lbf SL
1,505 kN SL
331 sec |
RD-0124
--- |
11D-58M
16,000 lbf
71,000 N
361 sec |
| Number of Engines |
1 (per strap-on) |
1 |
1 |
1 |
| Nominal Burn Time |
118 sec |
289*** |
--- |
--- |
** Note: Vacuum engine performance unless
otherwise specified.
*** Note: Estimated Values
|
