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|
Features |
Ballistic Missile |
Cruise Missile |
| Flight Path | Follows a parabolic trajectory; most of its flight is outside the atmosphere. | Flies within the Earth’s atmosphere, following a relatively straight or guided path. |
| Propulsion | Powered during the initial phase of launch; relies on gravity and momentum for most of the flight. | Powered throughout its flight using jet engines or turbojets. |
| Speed | Typically faster; can reach hypersonic speeds. | Slower compared to ballistic missiles; subsonic or supersonic speeds. |
| Guidance System | Primarily inertial guidance; less manoeuvrable in the mid-course phase. | Highly manoeuvrable with advanced guidance systems like GPS or terrain-following radar. |
| Range | Generally long-range, capable of intercontinental distances (ICBMs). | Typically medium to short-range, though some have long-range capabilities. |
| Accuracy | Less accurate compared to cruise missiles; used for large-scale destruction. | High precision; designed for targeted strikes. |
| Payload Type | Can carry nuclear, conventional, or other payloads; often used for strategic missions. | Can carry conventional or nuclear payloads; suited for tactical missions. |
| Detection | Easier to detect during the boost phase due to heat and smoke trails. | Harder to detect due to low altitude flight and terrain hugging capabilities. |
| Examples | Prithvi I, Prithvi II, Agni I, Agni II and Dhanush missiles | BrahMos Missile |