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Features
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Ballistic Missile
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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 |