Multiple independently targetable reentry vehicle
A multiple independently targetable reentry vehicle is a missile payload containing several warheads, each capable of being aimed to hit a different target. The concept is almost invariably associated with intercontinental ballistic missiles carrying thermonuclear warheads, even if not strictly being limited to them. By contrast, a unitary warhead is a single warhead on a single missile. An intermediate case is the multiple reentry vehicle missile which carries several warheads which are dispersed but not individually aimed. Only China, France, Russia, United Kingdom, United States and Pakistan are currently confirmed to possess functional MIRV missile systems. India and Israel are known or suspected to be developing or possessing MIRVs.
The first true MIRV design was the Minuteman III, first successfully tested in 1968 and introduced into actual use in 1970. The Minuteman III held three smaller W62 warheads of about 170 kilotons each in place of the single 1.2 megaton W56 used in the earlier versions of this missile. From 1970–1975, the United States would remove approximately 550 earlier versions of the Minuteman ICBM in the Strategic Air Command's arsenal and replace them with the new Minuteman IIIs outfitted with a MIRV payload, increasing their overall effectiveness. The smaller power of the warhead was offset by increasing the accuracy of the system, allowing it to attack the same hard targets as the larger, less accurate, W56. The MMIII was introduced specifically to address the Soviet construction of an anti-ballistic missile system around Moscow; MIRV allowed the US to overwhelm any conceivable ABM system without increasing the size of their own missile fleet. The Soviets responded by adding MIRV to their R-36 design, first with three warheads in 1975, and eventually up to ten in later versions. While the United States phased out the use of MIRVs in 2014 to comply with New START, Russia continues to develop new missile designs using the technology.
The introduction of MIRV led to a major change in the strategic balance. Previously, with one warhead per missile, it was conceivable that one could build a defense that used missiles to attack individual warheads. Any increase in missile fleet by the enemy could be countered by a similar increase in interceptors. With MIRV, a single new enemy missile meant that multiple interceptors would have to be built, meaning that it was much less expensive to increase the attack than the defense. This cost-exchange ratio was so heavily biased towards the attacker that the concept of mutual assured destruction became the leading concept in strategic planning and ABM systems were severely limited in the 1972 Anti-Ballistic Missile Treaty in order to avoid a massive arms race.
Purpose
The military purpose of a MIRV is fourfold:- Enhance first-strike proficiency for strategic forces.
- Providing greater target damage for a given thermonuclear weapon payload. Several small and lower yield warheads cause much more target damage area than a single warhead alone. This in turn reduces the number of missiles and launch facilities required for a given destruction level - much the same as the purpose of a cluster munition.
- With single warhead missiles, one missile must be launched for each target. By contrast, with a MIRV warhead the post-boost stage can dispense the warheads against multiple targets across a broad area.
- Reduces the effectiveness of an anti-ballistic missile system that relies on intercepting individual warheads. While a MIRV attacking missile can have multiple warheads, interceptors may have only one warhead per missile. Thus, in both a military and an economic sense, MIRVs render ABM systems less effective, as the costs of maintaining a workable defense against MIRVs would greatly increase, requiring multiple defensive missiles for each offensive one. Decoy reentry vehicles can be used alongside actual warheads to minimize the chances of the actual warheads being intercepted before they reach their targets. A system that destroys the missile earlier in its trajectory is not affected by this but is more difficult, and thus more expensive to implement.
Mode of operation
In a MIRV, the main rocket motor pushes a "bus" into a free-flight suborbital ballistic flight path. After the boost phase the bus maneuvers using small on-board rocket motors and a computerised inertial guidance system. It takes up a ballistic trajectory that will deliver a reentry vehicle containing a warhead to a target, and then releases a warhead on that trajectory. It then maneuvers to a different trajectory, releasing another warhead, and repeats the process for all warheads.The precise technical details are closely guarded military secrets, to hinder any development of enemy counter-measures. The bus's on-board propellant limits the distances between targets of individual warheads to perhaps a few hundred kilometers. Some warheads may use small hypersonic airfoils during the descent to gain additional cross-range distance. Additionally, some buses can release decoys to confuse interception devices and radars, such as aluminized balloons or electronic noisemakers.
Accuracy is crucial, because doubling the accuracy decreases the needed warhead energy by a factor of four for radiation damage and by a factor of eight for blast damage. Navigation system accuracy and the available geophysical information limits the warhead target accuracy. Some writers believe that government-supported geophysical mapping initiatives and ocean satellite altitude systems such as Seasat may have a covert purpose to map mass concentrations and determine local gravity anomalies, in order to improve accuracies of ballistic missiles. Accuracy is expressed as circular error probable. This is simply the radius of the circle that the warhead has a 50 percent chance of falling into when aimed at the center. CEP is about 90–100 m for the Trident II and Peacekeeper missiles.
MRV
A multiple reentry vehicle payload for a ballistic missile deploys multiple warheads, also known as "bomblets", in a "shotgun" like pattern above a single target. The advantage of an MRV over a single warhead is the increased effectiveness due to the greater coverage, this increases the overall-damage produced within the center of the pattern making it far greater than the damage possible from any single warhead in the MRV cluster; this makes for an efficient area attack weapon and makes interception by anti-ballistic missiles unlikely due to the number of warheads being deployed at once.Improved warhead designs allow smaller warheads for a given yield, while better electronics and guidance systems allow greater accuracy. As a result, MIRV technology has proven more attractive than MRV for advanced nations. Multiple-warhead missiles require both a miniaturised physics package and a lower mass reentry vehicle, both of which are highly advanced technologies. As a result, single warhead missiles are more attractive for nations with less advanced or less productive nuclear technology. The United States first began development of an MRV payload which was first used on the Polaris A-3 SLBM and was first deployed for use in 1964 on the USS Daniel Webster. The Polaris A-3 carried 3 "bomblets" each having an approximate yield of 200 Kt. The Royal Navy also had MRV payloads with the Chevaline upgrade. The Soviet Union deployed MRVs on the R-27U SLBM and the R-36 Mod 4 ICBM. Refer to atmospheric reentry for more details.
MIRV-capable missiles
;:- DF-5C
- DF-5B
- DF-16
- DF-31A
- DF-31B
- DF-41
- JL-2
- JL-3
- M4
- M45
- M51
- Agni-V
- Agni-VI
- K-5
- Khorramshahr missile
- Qiam 1 used for the first time during Operation Martyr Soleimani
- Ghadr-110
- Jericho 3
- Ababeel carries 3 standard warheads of 500 kg each or 5 of 300 kg or 8 maximum Warheads weighing 185 kg
MIRV at the National Air and Space Museum
- RS-28 Sarmat
- R-36M2 "Satan"
- RSM-54 R-29RMU2 "Layner"
- RSM-56 R-30 "Bulava"
- RS-26 Rubezh
- RS-24 Yars
- RSD-10 Pioneer
- UR-100N
- RSM-54 R-29RMU "Sineva"
- RT-2UTTH "Topol M"
- R-36 "Scarp"
- MR-UR-100 Sotka
- UR-100
- UGM-133 Trident II
- LGM-30 Minuteman III
- UGM-73 Poseidon
- UGM-96 Trident I
- LGM-118 Peacekeeper
- UGM-133 Trident II