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As 34 Kormoran
As 34 Kormoran




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As 34 Kormoran Performance

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1 Performance
1.1 Engine
Solid-fuel rocket
1.2 Propulsion
Not Available
1.2.1 Propellant
solid-propellant rocket motor
1.3 Speed
S 125 Neva Pech..
Not Available
Rank: N/A (Overall)
Ugm 27 Polaris Performance
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1.4 Guidance System
Semi-active radar homing (R-4R)Infrared homing (R-4T)
1.5 Flight Ceiling
Not Available
1.5.1 Flight altitude
Not Available
1.6 Accuracy
Not Available
1.7 Range
Df 5 Performance
Not Available
Rank: N/A (Overall)
Hgm 25A Titan I Performance
1.8 Launch Platform
Tu-28, MiG-25P
1.8.1 Basing
Not Available

As 34 Kormoran Range

The performance of As 34 Kormoran during flight is majorly governed by the nature of propellant used and its physical parameters. Factors that affect the missile performance are its weight during launch, steering system, propellant used to provide thrust as well as the fabrication material. Generally, engines used for propulsion of missiles are rocket & jet engines. Since missiles need to deploy multiple engine stages, they use rocket engines for launching. Once the missile overcomes pull of gravity, jet engine is used for further flight. Engine used in As 34 Kormoran is Solid-fuel rocket. During the missile launch, the propellant provides the power needed to impart thrust. Either solid type of fuel or liquid propellant (for larger missiles) is used to run the rocket engine. The propellant used is solid-propellant rocket motor.

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