Lightweight tandem launch vehicle
The Cyclone-4 launch vehicle is used for efficient and highly accurate injection of a single or multiple spacecraft into circular, geostationary, and sun-synchronous orbits.
The launch vehicle burns hypergolic storable liquid propellants.
The Cyclone-4 is the newest and most powerful rocket in the Cyclone family. The Cyclone rockets that have been in operation since 1969 (Cyclone-2) and are widely recognized among the most reliable launchers in the world.
Basic Specifications
|
Number of stages |
3 |
|
Dimensions, mm Length Stage diameter Fairing diameter |
40190 3000 4000 |
|
Launch mass, tons |
198,25 |
|
Propellants Oxidizer Fuel |
NTO UDMH |
|
Thrust, ton-force Stage 1 Stage 2 Stage 3 |
313 102 8 |
|
Maximum payload capability, tons 500-km circular orbit Geostationary transfer orbit Sun-synchronous orbit |
5,275 1,6 3,7 |
|
Injection accuracy: 500-km circular orbit Altitude, km Inclination, deg Geostationary transfer orbit Apogee height, km Perigee height, km Inclination, deg Sun-synchronous orbit Altitude, km Inclination, deg |
± 5 ± (0,05…0,08)
± 100 ± 5 ± (0,05…0,08)
± 6-7 ± (0,05…0,08) |
|
Maximum g-load |
6,8 |
|
Payload fairing cleanliness class (FED STD 209E) |
100 000 |
Cyclone-4 Payload Capability into Circular Orbits
Cyclone-4 Payload Capability into GTO
Cyclone-4 Payload Capability into Sun-Synchronous Orbits
Payload Accommodation Area
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