C 801 Anti Ship
C 801 Anti Ship


C 801 Anti Ship Performance

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1 Performance
1.1 Engine
1.2 Propulsion
Not Available
1.2.1 Propellant
solid rocket
1.3 Speed
S 125 Neva Pech..
Not Available
Rank: N/A (Overall)
Ugm 27 Polaris Performance
1.4 Guidance System
ARH / PRH / TV guidance / Infrared homing
1.5 Flight Ceiling
0.01-0.02 km
1.5.1 Flight altitude
8 20 m
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
Aerial, naval and land-based
1.8.1 Basing
Aerial, naval and land-based

C 801 Anti Ship Range

The performance of C 801 Anti Ship 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 C 801 Anti Ship is 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 rocket.

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