Ballistic missile: Difference between revisions

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A '''ballistic missile''' is a [[guided missile]], usually of substantial range compared to cannon, that follows a generally parabolic trajectory, as adjusted by guidance and control mechanisms, from launching point to target.  In most cases, the trajectory is [[suborbital]], spending at least part of its flight in [[outer space]], but not going into orbit. The WWII German [[V-2]] was the first operational cruise missile; a number of subsequent types, such as the Soviet-built [[SS-1 SCUD]] and many national derivatives of it, are essentially V-2 clones.  
A '''ballistic missile''' is a [[guided missile]], usually of substantial range compared to cannon, that follows a generally parabolic trajectory, as adjusted by guidance and control mechanisms, from launching point to target.  In most cases, the trajectory is [[suborbital]], spending at least part of its flight in [[outer space]], but not going into orbit. The WWII German [[V-2]] was the first operational cruise missile; a number of subsequent types, such as the Soviet-built [[SS-1 SCUD]] and many national derivatives of it, are essentially V-2 clones.  
   
   
'''Ballistic''' conveys the idea that the basic energy is imparted, usually by a [[rocket motor]] or motors (i.e., multiple stages, during the initial [[boost phase]] rising to the edge of space.It then goes into a '''[[midcourse]]''' where it coasts ballistically subject to guidance. During the midcourse, several reentry vehicles can separate for fixed reentry (i.e., Multiple reentry vehicle (MRV), or they can be fired as multiple independently targetable reentry vehicles (MIRV) onto a final path by a [[atmospheric reentry#warheads|midcourse '''bus''']], which can align itself, essentially above the atmosphere, so reentry vehicles are on a specific trajectory.   
'''Ballistic''' conveys the idea that the basic energy is imparted, usually by a [[rocket motor]] or motors (i.e., multiple stages, during the initial [[boost phase]] rising to the edge of space.It then goes into a '''[[midcourse]]''' where it coasts ballistically subject to guidance. During the midcourse, several reentry vehicles can separate for fixed reentry (i.e., Multiple reentry vehicle (MRV), or they can be fired as multiple independently targetable reentry vehicles (MIRV) onto a final path by a [[atmospheric reentry#warheads|midcourse '''bus''']], which can align itself, essentially above the atmosphere, so reentry vehicles are on a specific trajectory.   


Guidance for the boost and midcourse phases are usually [[inertial guidance]], although some system also use [[celestial guidance]].
Guidance for the boost and midcourse phases are usually [[inertial guidance]], although some systems also use [[celestial guidance]].


Midcourse is followed by '''[[atmospheric reentry]]''', which can be affected by the aerodynamics of the reentry vehicle, the way in which it deals with the sometimes extreme heating of atmospherics, and other environmental affects near the target. Most reentry vehicles are essentially pure ballistic, although some advanced types have aerodynamic controls or internal weights that allow them to be '''maneuvering reentry vehicles''' (MARV).
Midcourse is followed by '''[[atmospheric reentry]]''', which can be affected by the aerodynamics of the reentry vehicle, the way in which it deals with the sometimes extreme heating of atmospherics, and other environmental affects near the target. Most reentry vehicles are essentially pure ballistic, although some advanced types have had aerodynamic controls or internal weights that allow them to be '''maneuvering reentry vehicles''' (MARV). As a result of arms control agreements, Soviet and U.S. land-based long-range missiles no longer have MIRVs, and MARVs were never deployed. U.S. Pershing II missiles were to have a MARV, and were a sufficient threat that not deploying them became an important "bargaining chip" in the [[Intermediate Range Forces]] (INF) treaty.


During entry, decoys and other [[penetration aid]]s can be released to hide the reentry vehicles carrying [[warhead]]s from [[ballistic missile defense]] (BMD).
During entry, decoys and other [[penetration aid]]s can be released to hide the reentry vehicles carrying [[warhead]]s from [[ballistic missile defense]] (BMD).
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|-
|-
| [[battlefield short range ballistic missile]] (BSRBM)
| [[battlefield short range ballistic missile]] (BSRBM)
| <150 km < 94 km miles
| <150 km                  
< 94 km miles
| U.S. [[MGM-52 Lance]], Soviet/Russian [[SS-21B SCARAB B]
| U.S. [[MGM-52 Lance]], Soviet/Russian [[SS-21B SCARAB B]
|-
|-
| [[short range ballistic missile]] (SRBM)
| [[short range ballistic missile]] (SRBM)
| 150-799 km 94-499 miles
| 150-799 km                
94-499 miles
| German [[V-2]], Israeli [[Jericho I]], Soviet/Russian [[SS-1 SCUD|SS-1A SCUD]], U.S. [[MGM-140B ATACMS Block 1A]]
| German [[V-2]], Israeli [[Jericho I]], Soviet/Russian [[SS-1 SCUD|SS-1A SCUD]], U.S. [[MGM-140B ATACMS Block 1A]]
|-
|-
| [[medium range ballistic missile]] (MRBM)
| [[medium range ballistic missile]] (MRBM)
| 800-2,399 km 500-1499 miles
| 800-2,399 km    
500-1499 miles
| Iranian [[Shahab-3]], Israeli [[Jericho II]], U.S. [[Jupiter (missile)|PGM-19 Jupiter]],Soviet [[SS-4 SANDAL]]
| Iranian [[Shahab-3]], Israeli [[Jericho II]], U.S. [[Jupiter (missile)|PGM-19 Jupiter]],Soviet [[SS-4 SANDAL]]
|-
|-
| [[intermediate range ballistic missile]] (IRBM)
| [[intermediate range ballistic missile]] (IRBM)
| 1,400-5,499 km 1,500-3,437 miles
| 1,400-5,499 km      
1,500-3,437 miles
| Soviet [[SS-5 SKEAN]], Chinese [[DF-4]], Soviet [[SS-20]],  
| Soviet [[SS-5 SKEAN]], Chinese [[DF-4]], Soviet [[SS-20]],  
|-
|-
| [[intercontinental ballistic missile]] (ICBM)
| [[intercontinental ballistic missile]] (ICBM)
| + 5,500 km + 3,438 miles
| + 5,500 km            
| U.S. [[LGM-30 Minuteman III]] and [[UGM-133 Trident D5]]*
Ru+ 3,438 miles
| Chinese [[DF-5]], Russian [[SS-18]], U.S. [[LGM-30 Minuteman III]] and [[UGM-133 Trident D5]]§
|}
|}
* Submarine launched
§  Submarine launched


==References==
==References==
{{reflist}}
{{reflist}}

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A ballistic missile is a guided missile, usually of substantial range compared to cannon, that follows a generally parabolic trajectory, as adjusted by guidance and control mechanisms, from launching point to target. In most cases, the trajectory is suborbital, spending at least part of its flight in outer space, but not going into orbit. The WWII German V-2 was the first operational cruise missile; a number of subsequent types, such as the Soviet-built SS-1 SCUD and many national derivatives of it, are essentially V-2 clones.

Ballistic conveys the idea that the basic energy is imparted, usually by a rocket motor or motors (i.e., multiple stages, during the initial boost phase rising to the edge of space.It then goes into a midcourse where it coasts ballistically subject to guidance. During the midcourse, several reentry vehicles can separate for fixed reentry (i.e., Multiple reentry vehicle (MRV), or they can be fired as multiple independently targetable reentry vehicles (MIRV) onto a final path by a midcourse bus, which can align itself, essentially above the atmosphere, so reentry vehicles are on a specific trajectory.

Guidance for the boost and midcourse phases are usually inertial guidance, although some systems also use celestial guidance.

Midcourse is followed by atmospheric reentry, which can be affected by the aerodynamics of the reentry vehicle, the way in which it deals with the sometimes extreme heating of atmospherics, and other environmental affects near the target. Most reentry vehicles are essentially pure ballistic, although some advanced types have had aerodynamic controls or internal weights that allow them to be maneuvering reentry vehicles (MARV). As a result of arms control agreements, Soviet and U.S. land-based long-range missiles no longer have MIRVs, and MARVs were never deployed. U.S. Pershing II missiles were to have a MARV, and were a sufficient threat that not deploying them became an important "bargaining chip" in the Intermediate Range Forces (INF) treaty.

During entry, decoys and other penetration aids can be released to hide the reentry vehicles carrying warheads from ballistic missile defense (BMD).

The Launching System

Early ballistic missiles were exposed to attack, on the surface, originally for up to several hours of fueling with cryogenic liquid propellants. Even a single bullet might significantly damage the missile before launch.

Survivability increased when the missiles could be fueled while underground, and then increased significantly when they started to use storable liquid propellants that did not require hours of preparation. Still, the storable propellants tended to be hypergolic, or igniting on contact; again, there was extreme vulnerability to physical damage. In one memorable case, on 19 September 1980, a U.S. UGM-27 Titan II missile crewman, working on a missile in an open silo at Little Rock Air Force Base in Arkansas, dropped a socket wrench weighing perhaps one pound, into the silo, where it hit the outer skin of the fueled rocket at approximately 6:30 PM. The crew treated the incident seriously, for the propellants are highly toxic aside from the other dangers. At approximately 3 AM the next morning, the rocket exploded, killing 1, injuring 23, and hurling a 9-megaton W53 warhead several hundred feet away. The nuclear weapon demonstrated its safeguards by not partially or fully detonating.[1]

Later, solid propellant missiles such as the LGM-30 Minuteman had a stable solid propellant. Reportedly, it could be launched 32 seconds after receiving a valid order, although it would take longer for that order to get from the National Command Authority to the launch crew. The problem remained, however, as missile warheads became more and more accurate, that land-based ICBMs were increasingly vulnerable, thus encouraging "use it or lose it" and ultimately being destabilizing.

Various schemes of making the ICBMs more survivable through mobility, perhaps on special railroads within a military base, proved impractical. It made more sense to move the missiles to submarines, especially when submarine-launched missiles had sufficient range to launch from well-guarded waters.

Payloads

The total payload, or throw-weight, of a missile includes both the actual destructive material of the warhead(s), but also penetration aids that confuse a defense as to which reentering objects are the truly dangerous warheads.

Warheads

Nuclear warheads have been most common for longer-range ballistic missiles. Some short range missiles may have high explosive or cluster bomblet warheads, but, unless the reentry vehicle is extremely accurate, may be psychological weapons.

Some chemical warheads, often as bomblets, have been demonstrated. Biological warheads are rumored but not confirmed; they may have been destroyed.

The reentry speed of an ICBM is so great that the reentry vehicle can be filled with concrete for a fixed target, or metal rods for an area target; the kinetic energy of the warhead is so great that a conventional explosive filling would add no appreciable energy.

Penetration aids

Confusing the defense can have effects on two levels. If the target nation has ballistic missile defense, penetration aids will make the problem of intercepting the true warheads much more difficult. Devices flying along with the missile, to increase the difficulty of identifying the true warheads, are called penetration aids. Penetration aid technology is difficult, and harder for a nation to achieve that to acquire the missiles or technology limited by the Missile Technology Control Regime (MCTR).

It sometimes is difficult to draw the line between penetration aids and warheads. The three basic ways in which penetration aids work are:[2]

  • Saturation: presenting a large number of (real) targets for defensive interceptors, as with conventional submunitions, or multiple reentry vehicles (MRV), whether the latter simply be separate, independently targetable from midcourse (MIRV) or maneuverable in the atmosphere (MARV);
  • Concealment: obscuring a re-entry vehicle (RV), as with stealth or jamming, or mixing the RV with other objects, as with chaff or decoys;
  • Evasion: maneuvering the RV to avoid interception, as with terminal guidance and aerodynamic controls. Again, this technology is blurred between warhead and penetration aid. Variations on evasion include techniques that would require significant space technology, such as (in violation of treaties) leaving reentry vehicles in orbit; fractional orbital bombardment systems (FOBS) which fly against the Earth's direction of rotation; or depressed trajectory ballistic missiles, typically fired from submarines, that do not rise to the altitude at which warning radar will detect or track them.

Whether or not to confuse the defense of a nation without BMD is more of a challenge. Especially if the nation has its own nuclear-armed ballistic missiles, it may be dangerously destabilizing for the target country not to understand the nature of the attack directed at it. For example, if an attack is limited, intended for psychological effect (i.e., "we are really serious") and perhaps not even targeting a populated area or military base, the target nation is more prone to wait to counterattack.

If, however, the attack may be a large-scale disarming counterforce attack, the target may decide, with respect to its own land-based ballistic missiles, it faces a choice of "use it or lose it", and may launch an even more destructive response to the attacker.

Range bands

Ballistic missiles historically have differentiated by their range. There are major leaps in technology between short-range missiles of the V-1/SCUD type, to intermediate range, to intercontinental range. [3]

Type Range Examples
battlefield short range ballistic missile (BSRBM) <150 km

< 94 km miles

U.S. MGM-52 Lance, Soviet/Russian [[SS-21B SCARAB B]
short range ballistic missile (SRBM) 150-799 km

94-499 miles

German V-2, Israeli Jericho I, Soviet/Russian SS-1A SCUD, U.S. MGM-140B ATACMS Block 1A
medium range ballistic missile (MRBM) 800-2,399 km

500-1499 miles

Iranian Shahab-3, Israeli Jericho II, U.S. PGM-19 Jupiter,Soviet SS-4 SANDAL
intermediate range ballistic missile (IRBM) 1,400-5,499 km

1,500-3,437 miles

Soviet SS-5 SKEAN, Chinese DF-4, Soviet SS-20,
intercontinental ballistic missile (ICBM) + 5,500 km

Ru+ 3,438 miles

Chinese DF-5, Russian SS-18, U.S. LGM-30 Minuteman III and UGM-133 Trident D5§

§ Submarine launched

References

  1. The Encyclopedia of Arkansas History and Culture, Titan II Missile Explosion
  2. Speier, Richard (November 2007), "Missile Nonproliferation and Missile Defense: Fitting Them Together", Arms Control Today
  3. Elert, Glenn & Alicia White, The Physics Factbook