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Cyclone-3

Cyclone-3 launch vehicle, developed Yuzhnoye State Design company and built by Yuzhniy machine building plant, continues the series of Cyclone launchers. The third stage of Cyclone-3 was designed to take the shape of an ampoule, fitted with Yuzhnoye engine and made to have two ignitions in zero gravity. This feature expands capability of spacecraft injection to a greater extent.
Spacecraft launch is done from Plesetsk range (Russian Federation). Cyclone-3 launcher can inject spacecraft with a mass of up to 4000 kg into low and middle circular and elliptical orbits.
Cyclone03 launch vehicle is a transport system comprising highly reliable, flight-proven technologies. It features the best flight and operational characteristics traditionally peculiar to the launchers of Cyclone series.

Cyclone-3 LV performance (SC mass, orbit altitude and inclination)
at SC launching into circular and elliptic orbits.

Lift-off mass (at SC of 3.6t), t189

Payload envelope

Propellants for all stages:
oxidizeramil
fuelgeptil
Mass budget (without SC):
- full mass, t:
first stage127,5
second stage53,3
third stage4,6
- propellant mass:
first stage0,95
second stage0,92
third stage0,7
Thrust, tf:
first stage303,2
second stage101,5
third stage7,96
SC injection accuracy for Íęđ=600 ęě
orbit altitude, km15
revolution period, s5,0
inclination, ang. min3
Inclinations of orbits73,5;
82,5;

Launch service of the Cyclone-3 LV is characterized by optimal combination of reliability and cost.

Launch statistics Cyclone-3
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