Strela  
Initial Operational Capability (IOC):
Total Production: ?
Origin: Russia
Parent System: Strela
Initial Operational Capability (IOC):
Total Production: ?
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Description: The Strela is a three-stage light space launch vehicle based on the RS-18/SS-19 Stiletto intercontinental ballistic missile. These launchers that can lift off from underground silos at Baikonur and Svobodny Cosmodromes and are stored inside launch-transport canisters. The Strela launch vehicle retains the same mechanisms and instruments section provided to the RS-18 missile. That section is placed between the two rocket stages and the payload fairing. The Strela launch vehicle can be fitted with two different payload fairings known as Ascent Unit 1 and the larger Ascent Unit 2. The liquid propellant consists of high-boiling components of hypergolic propellant with unsymmetrical dimethyl hydrazine as fuel and nitrogen tetroxide as oxidizer. The Strela launch vehicle features inertial autonomous control system that can place a payload of 750 kg into a circular orbit at an altitude of 1,500 km, 1,220 kg into a circular orbit of 800 km, and 1,400 kg into a circular orbit of 500 km.

Strela Specifications

Number of Stages: 3
Dimensions
Height: 29.2 meter (1,150 inch)
Rocket Diameter: 2.50 meter
Percent
Reliability: 97 %
Weight
Max Lift-off Weight: 105 ton (231,481 pound)
Payload to LEO: 1,400 kilogram (3,086 pound)
Payload to SSO: 750 kilogram
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

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