Ballistic missile

V-2 One modern pioneer ballistic missile was the A-4, commonly known as the V-2, developed by Nazi Germany in the 1930s and 1940s under the direction of Wernher von Braun. The first successful launch of a V-2 was on October 3, 1942, and it began operation on September 6, 1944, against Paris, followed by an attack on London two days later. By the end of World War II in Europe in May 1945, more than 3,000 V-2s had been launched. In addition to its use as a weapon, a vertically launched V-2 became the first human-made object to reach outer space on June 20, 1944. ICBM arms race The R-7 Semyorka was the first intercontinental ballistic missile, with the first fully successful tests being completed in 1958-1959. The advent of ICBM technology began an arms race between the United States and Soviet Union, which saw the continuous development of ballistic missiles that could reach further, carry a greater load, and avoid intercepts. Alongside this arms race was the space race, which accelerated rocketry innovations and therefore contributed to the advancement of ballistic missile technology indirectly. The Minuteman III was the first ICBM equipped with a Multiple Independently targetable Reentry Vehicle (MIRV) to enter service, in 1970. The need for multiple warheads is a countermeasure to minimise the effectiveness of missile defense systems. Use in war The largest ballistic missile attack in history took place on 1 October 2024 when the Iranian Revolutionary Guard launched about 200 missiles at Israel, a distance of about 1,500 kilometers. The missiles arrived about 15 minutes after launch. It is believed that Iran's Fattah-1 and Kheybar Shekan missiles were used, which both have a range of about 1,400 km. == 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 . A ballistic missile's trajectory consists of three parts or phases: the boost phase, the mid-course phase and the terminal phase. Special systems and capabilities are required to facilitate the successful passage from one phase to the other. The boost phase is the powered flight portion, beginning with the ignition of the engines and concluding with the end of powered flight. The powered flight portion can last from a few tenths of seconds to several minutes and can consist of multiple rocket stages. The last phase in the missile's trajectory is the terminal or re-entry phase, beginning with the re-entry of the missile into the Earth's atmosphere (if exoatmospheric) During the beginning of this phase, the missile's trajectory is still relatively well defined, though as the missile reaches the heavier layers of atmosphere it is increasingly influenced by gravity and aerodynamic drag, which can affect its landing. == Types ==

SLBM launched by ballistic missile submarine Ballistic missiles can be launched from fixed sites or mobile launchers, including vehicles (e.g., transporter erector launchers), aircraft, ships, and submarines. Ballistic missiles 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: • Tactical ballistic missile (TBM): Range less than • Short-range ballistic missile (SRBM): Range from • Medium-range ballistic missile (MRBM): Range from • Intermediate-range ballistic missile (IRBM): Range from • Intercontinental ballistic missile (ICBM): Range greater than 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 in comparison to conventional bomber aircraft. == Quasi-ballistic missiles ==

A quasi-ballistic missile is a category of SRBM that is largely ballistic but is fully guided and can perform maneuvers throughout the entirety of atmospheric flight to make unexpected changes in direction and range. Large guided MLRS rockets with range comparable to an SRBM are sometimes categorized as quasi-ballistic missiles. List of quasi-ballistic missiles ; • Long Range – Anti Ship Missile (under development) ; • LORA (active) ; • MGM-140 ATACMS (active) • Precision Strike Missile (active) == Hypersonic ballistic missile ==

Many ballistic missiles reach hypersonic speeds (i.e. Mach 5 and above) when they re-enter the atmosphere from space. However, in common military terminology, the term "hypersonic ballistic missile" is generally only given to those that can be maneuvered before hitting their target and do not follow a simple ballistic trajectory. == Throw-weight ==

Throw-weight is a measure of the effective weight of ballistic missile payloads. It is measured in kilograms or tonnes. Throw-weight equals the total weight of a missile's warheads, reentry vehicles, self-contained dispensing mechanisms, penetration aids, and any other components that are part of the delivered payload, and not of the rocket itself (such as the launch rocket booster and launch fuel). Throw-weight may refer to any type of warhead, but in normal modern usage, it refers almost exclusively to nuclear or thermonuclear payloads. It was once also a consideration in the design of naval ships and the number and size of their guns. Throw-weight was used as a criterion in classifying different types of missiles during Strategic Arms Limitation Talks between the Soviet Union and the United States. The term became politically controversial during debates over the arms control accord, as critics of the treaty alleged that Soviet missiles were able to carry larger payloads and so enabled the Soviets to maintain higher throw-weight than an American force with a roughly comparable number of lower-payload missiles. The missiles with the world's heaviest payloads are the Russian SS-18 and Chinese CSS-4 and , Russia was developing a new heavy-lift, liquid-propellant ICBM called the Sarmat. By reducing the payload weight, different trajectories can be selected, which can either increase the nominal range or decrease the total time in flight. A depressed trajectory is non-optimal, as a lower and flatter trajectory takes less time between launch and impact but has a lower throw-weight. The primary reasons to choose a depressed trajectory are to evade anti-ballistic missile systems by reducing the time available to shoot down the attacking vehicle (especially during the vulnerable burn-phase against space-based ABM systems) or a nuclear first-strike scenario. An alternate, non-military purpose for a depressed trajectory is in conjunction with the spaceplane concept with use of airbreathing jet engines, which requires the ballistic missile to remain low enough inside the atmosphere for air-breathing engines to function. In contrast, a "lofted" trajectory is frequently used for testing purposes, as it reduces the range of the missile (allowing for a controlled and observed impact), as well as signals a lack of hostile intention with the test. == Combat use ==

The following ballistic missiles have been used in combat: • Ghadr-110 • LORA • MGM-140 ATACMS • OTR-21 Tochka • Qaher-1/2M • Scud • V-2 • Zolfaghar • Kh-47M2 Kinzhal • Oreshnik == See also ==