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Ballistic Missiles

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Ballistic Missiles

A ballistic missile is a missile that follows a ballistic flightpath with the objective of delivering one or more warheads to a predetermined target. Shorter range ballistic missiles stay within the Earth's atmosphere, while longer range ones are designed to spend some of their flight time above the atmosphere and are thus considered sub-orbital.

History

The first ballistic missile was the A-4,[1] commonly known as the V-2 rocket, developed by Nazi Germany in the 1930s and 1940s under direction of T.J. Gertner and Wernher von Braun. The first successful launch of a V-2 was on October 3, 1942, and began operation on September 6, 1944, against Paris, followed by an attack on London two days later. By the end of World War II, May 1945, over 3,000 V-2s had been launched.

The R-7 Semyorka was the first ICBM, while the SM-65 Atlas was the first American ICBM.

A total of 30 nations have deployed operational ballistic missiles. Development continues, with around 100 ballistic missile flight tests (not including those of the US) in 2007, mostly by China, Iran and the Russian Federation. In 2010 the US and Russian governments signed a treaty to reduce their inventory of intercontinental ballistic missiles (ICBMs) over a seven-year period (to 2017) to 1550 units each.[2]


Flight

A ballistic missile trajectory consists of three parts: the powered flight portion, the free-flight portion which constitutes most of the flight time, and the re-entry phase where the missile re-enters the Earth's atmosphere.

Ballistic missiles can be launched from fixed sites or mobile launchers, including vehicles (transporter erector launchers, TELs), aircraft, ships and submarines. The powered flight portion can last from a few tens of seconds to several minutes and can consist of multiple rocket stages.

When in space and no more thrust is provided, the missile enters free-flight. In order to cover large distances, ballistic missiles are usually launched into a high sub-orbital spaceflight; for intercontinental missiles the highest altitude (apogee) reached during free-flight is about 1200 km.

The re-entry stage begins at an altitude where atmospheric drag plays a significant part in missile trajectory, and lasts until missile impact.

Missile types

Ballistic missiles can vary widely in range and use, and are often divided into categories based on range. Various schemes are used by different countries to categorize the ranges of ballistic missiles:

Short- and medium-range missiles are often collectively referred to as theater or tactical ballistic missiles (TBMs). Long- and medium-range ballistic missiles are generally designed to deliver nuclear weapons because their payload is too limited for conventional explosives to be cost-effective (though the U.S. is evaluating the idea of a conventionally armed ICBM for near-instant global air strike capability despite the high costs).

The flight phases are like those for ICBMs, except with no exoatmospheric phase for missiles with ranges less than about 350 km.

Quasi ballistic missiles

A quasi ballistic missile (also called a semi ballistic missile) is a category of missile that has a low trajectory and/or is largely ballistic but can perform maneuvers in flight or make unexpected changes in direction and range.

At a lower trajectory than a ballistic missile, a quasi ballistic missile can maintain higher speed, thus allowing its target less time to react to the attack, at the cost of reduced range.

The Russian Iskander is a quasi ballistic missile.[3] The Russian Iskander-M cruises at hypersonic speed of 2,100–2,600 m/s (Mach 6 - 7) at a height of 50 km. The Iskander-M weighs 4,615 kg carries a warhead of 710 – 800 kg, has a range of 480 km and achieves a CEP of 5 – 7 meters. During flight it can maneuver at different altitudes and trajectories to evade anti-ballistic missiles.[4][5]

China & Iran have recently developed anti-ship ballistic missile;

 China
  • DF-21D
 Iran
  • Khalij Fars

Comparable systems

See also

References

Further reading

Bate, Mueller, White (1971). Fundamentals of Astrodynamics. Dover Publications, New York. ISBN 0-486-60061-0

External links

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