Ballistic missile: Difference between revisions

From Citizendium
Jump to navigation Jump to search
imported>Howard C. Berkowitz
m (Text replacement - "guided missile" to "guided missile")
 
(38 intermediate revisions by 5 users not shown)
Line 1: Line 1:
{{subpages}}
{{subpages}}
{{TOC|right}}
[[File:Polaris-a3.jpg|thumb|U.S. Navy Polaris ballistic missile on the pad in Cape Canaveral, Florida, U.S.A., circa 1964. CREDIT: Public domain]]
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, of much greater range than that of artillery, 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 World War II German [[V-2]] ballistic missile was the first used in warfare. Ballistic missiles have been a part of modern warfare, starting with the Germans bombing London during World War II, and have given human beings the opportunity to wage global nuclear war and create vast destruction from a distance. Starting in the early 1970s, their deployment became subject to a number of international treaties designed to limit the destruction of a nuclear war.
   
   
'''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''<ref name=MC>Midcourse guidance involves stabilizing the path, through air and space, after burnout of the boost engines and the end of increasing acceleration. Stabilization most often depends on small [[rocket motor]]s called ''thrusters'', but also may use gyroscopes, and aerodynamic fins while still in atmosphere.  Midcourse guidance for a high-altitude [[cruise missile]] or [[unmanned aerial vehicle]] usually depends on inputs from [[Global Navigation Satellite System]]s (e.g., GPS) or sometimes [[inertial navigational]], and adjusts its flight path with aerodynamic control surfaces and possibly adjustments to its engine power. Terrain-following cruise missiles may also use GPS or intertial guidance, but they also make significant use of [[radar]], minimally a radar altimeter for terrain avoidance, but often terrain contour mapping systems that match the ground radar image to a highly accurate digital map.</ref> where it coasts ballistically subject to guidance. During the midcourse, several reentry vehicles can separate for fixed reentry, 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 above the atmosphere so reentry vehicles are on a specific trajectory.  In many short-range ballistic missiles, the entire missile remains intact until the warhead detonates.


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).  


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.
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.
{{TOC|left}}


During entry, decoys and other [[penetration aid]]s can be released to hide the reentry vehicles carrying [[warhead]]s from [[ballistic missile defense]] (BMD).
In the early 21st-century, a new international arms race has developed involving the use of hypersonic glide vehicles, sometimes launched from ballistic missiles. A hypersonic glide vehicle is a type of warhead for ballistic missiles that can maneuver and glide at hypersonic speed, in other words, many times the speed of sound at velocities of Mach 5 and greater. It can be used in conjunction with ballistic missiles to significantly change their trajectories after launch, allowing a weapon that theoretically is harder to detect by defensive forces. As of 2024, countries developing and testing these weapons include China, India, France, Russia, North Korea, Japan, and the United States.
==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 [[nuclear weapon, W53|9-megaton W53 warhead]] several hundred feet away. The nuclear weapon demonstrated its safeguards by not partially or fully detonating.<ref name=ArkTitan>{{citation
==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. 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 warhead several hundred feet away. The nuclear weapon demonstrated its safeguards by not partially or fully detonating.<ref name=ArkTitan>{{citation
  | title = Titan II Missile Explosion
  | title = Titan II Missile Explosion
  | author = The Encyclopedia of Arkansas History and Culture
  | author = The Encyclopedia of Arkansas History and Culture
Line 19: Line 21:
}}</ref>
}}</ref>


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.
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 intercontinental ballistic missiles (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.
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.
==Guidance==
Guidance for the boost and midcourse phases is usually [[inertial navigation|inertial]], utilizing devices such as gyroscopes, although some systems also use celestial guidance.


==Payloads==
==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.
The total payload, or ''throw-weight'', of a missile includes both the actual destructive material of the ''warhead(s)'', but also ballistic missile penetration aids that confuse a defense as to which reentering objects are the truly dangerous [[warhead]]s.  Payload weight assigned to penetration aids has to be traded against weight allocated to guidance or to actual warheads; the optimal distribution was being researched from the very first days of ballistic missiles. If increased guidance system weight can make warhead delivery more accurate, smaller warheads can be used. <ref name=RAND-P-1839>{{citation
| title = Ballistic Missile Payload Allocation
| publisher = RAND Corporation
| author=Sidney I. Firstman
| id = P-1839
| url = http://www.dtic.mil/cgi-bin/GetTRDoc?AD=AD616405&Location=U2&doc=GetTRDoc.pdf
| date = 12 November 1959}}</ref>
 
===Warheads===
===Warheads===
[[Nuclear weapon|Nuclear warhead]]s 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.
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.
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.
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===
===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:<ref name=ACA>{{citation
| journal =Arms Control Today 
| date =November 2007
| title =Missile Nonproliferation and Missile Defense: Fitting Them Together
| first =Richard | last = Speier
|url=http://www.armscontrol.org/act/2007_11/Speier.asp?print}}</ref>
*'''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.
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).
==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. <ref name=Elert>{{citation
| first1 = Glenn | last1 =Elert | first2 =Alicia | last2 = White
| title = The Physics Factbook
| url =http://hypertextbook.com/facts/2003/AliciaWhite.shtml}}</ref>
{| class="wikitable"
|-
! Type ''(No longer in service)''
! 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-1 SCUD|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. [[Jupiter (missile)|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]], U.S. ''[[PGM-17 Thor]]''
|-
| [[intercontinental ballistic missile]] (ICBM)
| + 5,500 km             
Ru+ 3,438 miles
| Chinese [[DF-5]], Russian [[RT-2]] and [[RSM-52]]§, U.S. [[LGM-30 Minuteman III]] and [[UGM-133 Trident D5]]§
|}


It sometimes is difficult to draw the line between penetration aids and warheads. Indeed, the real warheads may be configured to resemble a decoy, and vice versa. <ref name=GarwinPBS>{{citation
| url = http://www.pbs.org/wgbh/pages/frontline/shows/missile/interviews/garwin.html
| journal = PBS Frontline
| title = Missile Wars: Interview, Richard Garwin
}}</ref>


§  Submarine launched
== Historical deployment and use==
[[File:8k63 na pu.jpg|thumb|Soviet R-12 missile of type deployed to Cuba during the Cold War]]
Ballistic missiles were first used as weapons during World War II, by the German forces, who bombed London from a distance with V-2 ballistic missiles armed with conventional high explosives. Later, ballistic missiles were often armed with nuclear warheads, but to date these have never used in battle. The Cuban missile crisis of 1962 was over the deployment of Soviet R-12 Dvina intermediate-range nuclear ballistic missiles staged in Cuba within striking range of the continental United States. High-explosive warhead Scud ballistic missiles were used in the Iran–Iraq war of the 1980s, by both Iran and Iraq, and also in the U.S.-led Gulf War conflict of early 1991, by Iraq against Coalition Forces, Israel, and Saudi Arabia.


==References==
==References==
{{reflist}}
{{reflist|2}}[[Category:Suggestion Bot Tag]]

Latest revision as of 13:42, 3 October 2024

This article is a stub and thus not approved.
Main Article
Discussion
Related Articles  [?]
Bibliography  [?]
External Links  [?]
Citable Version  [?]
 
This editable Main Article is under development and subject to a disclaimer.
U.S. Navy Polaris ballistic missile on the pad in Cape Canaveral, Florida, U.S.A., circa 1964. CREDIT: Public domain

A ballistic missile is a guided missile, of much greater range than that of artillery, 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 World War II German V-2 ballistic missile was the first used in warfare. Ballistic missiles have been a part of modern warfare, starting with the Germans bombing London during World War II, and have given human beings the opportunity to wage global nuclear war and create vast destruction from a distance. Starting in the early 1970s, their deployment became subject to a number of international treaties designed to limit the destruction of a nuclear war.

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[1] where it coasts ballistically subject to guidance. During the midcourse, several reentry vehicles can separate for fixed reentry, or they can be fired as multiple independently-targetable reentry vehicles (MIRV) onto a final path by a midcourse bus, which can align itself above the atmosphere so reentry vehicles are on a specific trajectory. In many short-range ballistic missiles, the entire missile remains intact until the warhead detonates.

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.

In the early 21st-century, a new international arms race has developed involving the use of hypersonic glide vehicles, sometimes launched from ballistic missiles. A hypersonic glide vehicle is a type of warhead for ballistic missiles that can maneuver and glide at hypersonic speed, in other words, many times the speed of sound at velocities of Mach 5 and greater. It can be used in conjunction with ballistic missiles to significantly change their trajectories after launch, allowing a weapon that theoretically is harder to detect by defensive forces. As of 2024, countries developing and testing these weapons include China, India, France, Russia, North Korea, Japan, and the United States.

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. 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 warhead several hundred feet away. The nuclear weapon demonstrated its safeguards by not partially or fully detonating.[2]

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 intercontinental ballistic missiles (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.

Guidance

Guidance for the boost and midcourse phases is usually inertial, utilizing devices such as gyroscopes, although some systems also use celestial guidance.

Payloads

The total payload, or throw-weight, of a missile includes both the actual destructive material of the warhead(s), but also ballistic missile penetration aids that confuse a defense as to which reentering objects are the truly dangerous warheads. Payload weight assigned to penetration aids has to be traded against weight allocated to guidance or to actual warheads; the optimal distribution was being researched from the very first days of ballistic missiles. If increased guidance system weight can make warhead delivery more accurate, smaller warheads can be used. [3]

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. Indeed, the real warheads may be configured to resemble a decoy, and vice versa. [4]

Historical deployment and use

Soviet R-12 missile of type deployed to Cuba during the Cold War

Ballistic missiles were first used as weapons during World War II, by the German forces, who bombed London from a distance with V-2 ballistic missiles armed with conventional high explosives. Later, ballistic missiles were often armed with nuclear warheads, but to date these have never used in battle. The Cuban missile crisis of 1962 was over the deployment of Soviet R-12 Dvina intermediate-range nuclear ballistic missiles staged in Cuba within striking range of the continental United States. High-explosive warhead Scud ballistic missiles were used in the Iran–Iraq war of the 1980s, by both Iran and Iraq, and also in the U.S.-led Gulf War conflict of early 1991, by Iraq against Coalition Forces, Israel, and Saudi Arabia.

References

  1. Midcourse guidance involves stabilizing the path, through air and space, after burnout of the boost engines and the end of increasing acceleration. Stabilization most often depends on small rocket motors called thrusters, but also may use gyroscopes, and aerodynamic fins while still in atmosphere. Midcourse guidance for a high-altitude cruise missile or unmanned aerial vehicle usually depends on inputs from Global Navigation Satellite Systems (e.g., GPS) or sometimes inertial navigational, and adjusts its flight path with aerodynamic control surfaces and possibly adjustments to its engine power. Terrain-following cruise missiles may also use GPS or intertial guidance, but they also make significant use of radar, minimally a radar altimeter for terrain avoidance, but often terrain contour mapping systems that match the ground radar image to a highly accurate digital map.
  2. The Encyclopedia of Arkansas History and Culture, Titan II Missile Explosion
  3. Sidney I. Firstman (12 November 1959), Ballistic Missile Payload Allocation, RAND Corporation, P-1839
  4. "Missile Wars: Interview, Richard Garwin", PBS Frontline