Electro-optical MASINT: Difference between revisions
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{{PropDel}}<br><br>{{subpages}} | {{PropDel}}<br><br>{{subpages}} | ||
'''Electro-optical MASINT''' is a subdiscipline of | '''Electro-optical MASINT''' is a subdiscipline of measurement and signature intelligence]] (MASINT), which has similarities to but complements imagery intelligence]] (IMINT). The basic model of IMINT is taking a photograph, perhaps using techniques that record information not visible to the unassisted human eye, but a picture nonetheless. It may take significant skill to interpret objects in that picture, but the interpretation still depends on visual metaphors such as shape, size, and shadow. | ||
Electro-optical MASINT helps validate the elements of that picture, so that, for example, the analyst can tell if an area of green is vegetation or camouflage paint. Electro-optical MASINT also generates information on phenomena that emit, absorb, or reflect electromagnetic energy in the | Electro-optical MASINT helps validate the elements of that picture, so that, for example, the analyst can tell if an area of green is vegetation or camouflage paint. Electro-optical MASINT also generates information on phenomena that emit, absorb, or reflect electromagnetic energy in the infrared]], visible light]], or ultraviolet]] spectra, phenomena where a "picture" is less important than the amount or type of energy reported. For example, a class of satellites, originally intended to give early warning of rocket launches based on the heat of their exhaust, reports energy wavelengths and strength as a function of location(s). There would be no value, in this specific context, to seeing a photograph of the flames coming out of the rocket. | ||
Subsequently, when the geometry between the rocket exhaust and the sensor permits a clear view of the exhaust, IMINT would give a visual or infrared picture of its shape, while electro-optical MASINT would give, either as a list of coordinates with characteristics, or a "false-color" image, the temperature distribution, and | Subsequently, when the geometry between the rocket exhaust and the sensor permits a clear view of the exhaust, IMINT would give a visual or infrared picture of its shape, while electro-optical MASINT would give, either as a list of coordinates with characteristics, or a "false-color" image, the temperature distribution, and spectrometry|spectrometric]] information on its composition. In other words, MASINT may give warning before characteristics visible to IMINT are clear, or it may help validate or understand the pictures taken by IMINT. | ||
MASINT techniques are not limited to the United States, but the U.S. distinguishes MASINT sensors from others more than do other nations. According to the | MASINT techniques are not limited to the United States, but the U.S. distinguishes MASINT sensors from others more than do other nations. According to the United States Department of Defense]], MASINT is technically derived intelligence (excluding traditional imagery IMINT]] and signals intelligence SIGINT]]) that – when collected, processed, and analyzed by dedicated MASINT systems – results in intelligence that detects, tracks, identifies, or describes the signatures (distinctive characteristics) of fixed or dynamic target sources. MASINT was recognized as a formal intelligence discipline in 1986.<ref name =IOSS-2>{{cite web | ||
| last = Interagency OPSEC Support Staff (IOSS) | | last = Interagency OPSEC Support Staff (IOSS) | ||
| title = Operations Security Intelligence Threat Handbook: Section 2, Intelligence Collection Activities and Disciplines | | title = Operations Security Intelligence Threat Handbook: Section 2, Intelligence Collection Activities and Disciplines | ||
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| publisher = Air Force Institute of Technology | url = http://www.afit.edu/cmsr/}}</ref> | | publisher = Air Force Institute of Technology | url = http://www.afit.edu/cmsr/}}</ref> | ||
MASINT collection technologies in this area use radar, lasers, staring arrays in the infrared and visual, to point sensors at the information of interest. As opposed to IMINT, MASINT electro-optical sensors do not create pictures. Instead, they would indicate the coordinates, intensity, and spectral characteristics of a light source, such as a | MASINT collection technologies in this area use radar, lasers, staring arrays in the infrared and visual, to point sensors at the information of interest. As opposed to IMINT, MASINT electro-optical sensors do not create pictures. Instead, they would indicate the coordinates, intensity, and spectral characteristics of a light source, such as a rocket]] engine, or a missile reentry vehicle]]. Electro-optical MASINT involves obtaining information from emitted or reflected energy, across the wavelengths of infrared]], visible]], and ultraviolet]] light]]. Electro-optical techniques include measurement of the radiant intensities, dynamic motion, and the materials composition of a target. These measurements put the target in spectral and spatial contexts. Sensors used in electro-optical MASINT include radiometers, spectrometers, non-literal imaging systems, lasers, or laser radar (LIDAR]]).<ref name=FM2-0Ch9>{{cite web | ||
| last = US Army | | last = US Army | ||
| title = Chapter 9: Measurement and Signals Intelligence | | title = Chapter 9: Measurement and Signals Intelligence | ||
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| url = https://atiam.train.army.mil/soldierPortal/atia/adlsc/view/public/10536-1/FM/2-0/chap9.htm3}}</ref> | | url = https://atiam.train.army.mil/soldierPortal/atia/adlsc/view/public/10536-1/FM/2-0/chap9.htm3}}</ref> | ||
Observation of foreign missile tests, for example, make extensive use of MASINT along with other disciplines. For example, electro-optical and radar tracking establish trajectory, speed, and other flight characteristics that can be used to validate the | Observation of foreign missile tests, for example, make extensive use of MASINT along with other disciplines. For example, electro-optical and radar tracking establish trajectory, speed, and other flight characteristics that can be used to validate the TELINT]] telemetry intelligence being received by SIGINT sensors. Electro-optical sensors, which guide radars, operate on aircraft, ground stations, and ships. | ||
The major subdisciplines of electro-optical MASINT are: | The major subdisciplines of electro-optical MASINT are: | ||
:* | :*#airborne electro-optical missile tracking MASINT|airborne electro-optical missile tracking MASINT]] | ||
:* | :*#electro-optical artillery detection MASINT|electro-optical artillery detection MASINT]] | ||
:* | :*#Short-range aircraft and missile tracking|Short-range aircraft and missile tracking]] | ||
:* | :*#Long-range missile tracking|Long-range missile tracking]] | ||
:* | :*infrared MASINT]] | ||
:* | :*#optical measurement of nuclear explosions MASINT|optical measurement of nuclear explosions MASINT]] | ||
:* | :*#LASER MASINT|LASER MASINT]] | ||
:* | :*spectroscopic MASINT]] | ||
==Airborne Electro-Optical Missile Tracking MASINT== | ==Airborne Electro-Optical Missile Tracking MASINT== | ||
U.S. | U.S. RC-135 COBRA BALL]] aircraft have MASINT sensors that are "...two linked electro-optical sensors -- the Real Time Optics System (RTOS) and the Large Aperture Tracker System (LATS). RTOS consists of an array of staring sensors encompassing a wide field of regard for target acquisition. LATS serves as an adjunct tracker. Due to its large aperture, it has significantly greater sensitivity and resolving power than the RTOS, but is otherwise similar.<ref name=COBRABALL>{{Citation | ||
| last = Pike | | last = Pike | ||
| first = John | | first = John | ||
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| url = http://www.globalsecurity.org/intell/systems/cobra_ball.htm}}</ref> | | url = http://www.globalsecurity.org/intell/systems/cobra_ball.htm}}</ref> | ||
<!-- | <!--Image:RC-135 Cobra Ball aircraft parked at Offutt.jpg|thumb|Two Cobra Ball aircraft on the flightline at Offutt Air Force Base]], Nebraska.]]--> | ||
There is a broader program to standardize the architecture of the various RC-135 aircraft, so that there will be greater commonality of parts, and some ability to switch missions: a COBRA BALL will be able to carry out some SIGINT missions of the | There is a broader program to standardize the architecture of the various RC-135 aircraft, so that there will be greater commonality of parts, and some ability to switch missions: a COBRA BALL will be able to carry out some SIGINT missions of the RC-135 RIVET JOINT#RC-135V/W Rivet Joint |RIVET JOINT]] RC-135. | ||
COBRA BALL | COBRA BALL MASINT#Cueing |cues]] the COBRA DANE ground radar and the COBRA JUDY ship-based radar. See Radar MASINT]]. This application is for technical intelligence]]; see #Long-range missile tracking|Long-range missile tracking]] for the use of these sensors in ballistic missile defense]]. | ||
==Electro-optical artillery detection MASINT== | ==Electro-optical artillery detection MASINT== | ||
Both electro-optical and radar sensors have been coupled with acoustic sensors in modern counter-artillery systems. Electro-optical sensors are directional and precise, so need to be cued by acoustic or other omnidirectional sensors. The original | Both electro-optical and radar sensors have been coupled with acoustic sensors in modern counter-artillery systems. Electro-optical sensors are directional and precise, so need to be cued by acoustic or other omnidirectional sensors. The original Canada|Canadian]] geophysical MASINT#Counterbattery and Countersniper Location and Ranging|sensors]], in the First World War]], used visual observation and plotting of flash, as well as geophysical MASINT| acoustic]] sensors. | ||
===Purple Hawk=== | ===Purple Hawk=== | ||
Complementing | Complementing Radar MASINT#Counterartillery Radar |counter-mortar radar]] is the Israel|Israeli]] Purple Hawk mast-mounted electro-optical sensor, which detects mortars and provides perimeter security. The device, remotely operated via fiber optics or microwave, is intended to have a laser designator.<ref>{{Citation | ||
| author = Daniel W. Caldwell | | author = Daniel W. Caldwell | ||
| title = Radar planning, preparation and employment of 3-tiered coverage: LCMR, Q-36 and Q-37 | | title = Radar planning, preparation and employment of 3-tiered coverage: LCMR, Q-36 and Q-37 | ||
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}}</ref> RLS combines components from two existing systems, the Tactical Aircraft Directed Infra-Red Countermeasures (TADIRCM) and the UTAMS . The two-color infrared sensors were originally designed to detect surface-to-air missiles for TADIRCM. Other TADIRCM components also have been adapted to RLS, including the computer processors, inertial navigation units (INU), and detection and tracking algorithms. | }}</ref> RLS combines components from two existing systems, the Tactical Aircraft Directed Infra-Red Countermeasures (TADIRCM) and the UTAMS . The two-color infrared sensors were originally designed to detect surface-to-air missiles for TADIRCM. Other TADIRCM components also have been adapted to RLS, including the computer processors, inertial navigation units (INU), and detection and tracking algorithms. | ||
It is an excellent example of | It is an excellent example of MASINT#Cueing |automatic cueing]] of one sensor by another. Depending on the application, the sensitivity|sensitive]] but less selectivity|selective]] sensor is either acoustic or nonimaging electro-optical. The selective sensor is forward-looking infrared]] (FLIR). | ||
RLS uses two TADIRCM sensors, an INU, and a smaller field-of-view single-color (FLIR) camera on each tower. The INU, which contains a GPS receiver, allows the electro-optical sensors to align to the azimuth and elevation of any detected threat signature. | RLS uses two TADIRCM sensors, an INU, and a smaller field-of-view single-color (FLIR) camera on each tower. The INU, which contains a GPS receiver, allows the electro-optical sensors to align to the azimuth and elevation of any detected threat signature. | ||
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When a sensor measures a potential threat, the control station determines if it correlates with another measurement to give a threat signature. When a threat is recognized, RLS triangulates the optical signal and presents the Point of Origin (POO) on a map display. The nearest tower FLIR camera then is cued to the threat signature, giving the operator real-time video within 2 seconds of detection. When not in RLS mode, the FLIR cameras are available to the operator as surveillance cameras. | When a sensor measures a potential threat, the control station determines if it correlates with another measurement to give a threat signature. When a threat is recognized, RLS triangulates the optical signal and presents the Point of Origin (POO) on a map display. The nearest tower FLIR camera then is cued to the threat signature, giving the operator real-time video within 2 seconds of detection. When not in RLS mode, the FLIR cameras are available to the operator as surveillance cameras. | ||
<!-- | <!--Image:MASINT-UTAMStower.png | thumb |UTAMS-RLS tower head]]--> | ||
Mortar launches do not produce as strong an electro-optical signature as does a rocket, so RLS relies on acoustic signature cueing from an | Mortar launches do not produce as strong an electro-optical signature as does a rocket, so RLS relies on acoustic signature cueing from an Geophysical MASINT#UTAMS |Unattended Transient Acoustic Measurement and Signal Intelligence System (UTAMS)]]. There is an UTAMS array at the top of each of the three RLS towers. The tower heads can be rotated remotely. | ||
Each array consists of four microphones and processing equipment. Analyzing the time delays between an acoustic wavefront’s interaction with each microphone in the array UTAMS provides an azimuth of origin. The azimuth from each tower is reported to the UTAMS processor at the control station, and a POO is triangulated and displayed. The UTAMS subsystem can also detect and locate the point of impact (POI), but, due to the difference between the speeds of sound and light, it may take UTAMS as long as 30 seconds to determine the POO for a rocket launch 13 km away. This means UTAMS may detect a rocket POI prior to the POO, providing very little if any warning time. but the electro-optical component of RLS will detect the rocket POO earlier. | Each array consists of four microphones and processing equipment. Analyzing the time delays between an acoustic wavefront’s interaction with each microphone in the array UTAMS provides an azimuth of origin. The azimuth from each tower is reported to the UTAMS processor at the control station, and a POO is triangulated and displayed. The UTAMS subsystem can also detect and locate the point of impact (POI), but, due to the difference between the speeds of sound and light, it may take UTAMS as long as 30 seconds to determine the POO for a rocket launch 13 km away. This means UTAMS may detect a rocket POI prior to the POO, providing very little if any warning time. but the electro-optical component of RLS will detect the rocket POO earlier. | ||
==Short-range aircraft and missile tracking== | ==Short-range aircraft and missile tracking== | ||
Infrared tracking has long been used for missile guidance, first with | Infrared tracking has long been used for missile guidance, first with air-to-air missile]]s such as the AIM-9 Sidewinder]], but also with MANPADS]] such as the 9K31 Strela-1]] (Western: SA-9 GASKIN]]). Pure infrared sensors, however, are vulnerable to being decoyed by hot flares. | ||
While newer infrared seekers use additional wavelengths and pattern recognition that can discriminate flares, another approach has been to add | While newer infrared seekers use additional wavelengths and pattern recognition that can discriminate flares, another approach has been to add ultraviolet]] sensors, or to replace them completely. For example, the FIM-92 Stinger]] short-range antiaircraft missile uses "dual-band" infrared and ultraviolet guidance. The AAR-54, a representative missile warning receiver]], primarily intended for use on aircraft, uses pure ultraviolet detection, although missile warning receivers increasingly use multiple electro-optical wavelengths, and may cue radar onto the missile track. | ||
==Long-range missile tracking== | ==Long-range missile tracking== | ||
Both aircraft and satellite based sensors can be used to track long-range missile launches, both for strategic warning of | Both aircraft and satellite based sensors can be used to track long-range missile launches, both for strategic warning of ICBM]] launch, and tactical warning and tracking of theater ballistic missile]]s. | ||
===Initial space-based=== | ===Initial space-based=== | ||
{{main|Defense Support Program}} | {{main|Defense Support Program}} | ||
The US, in 1970, launched the first of a series of space-based | The US, in 1970, launched the first of a series of space-based staring array]] sensors that detected and located infrared heat signatures, typically from rocket motors but also from other intense heat sources. Such signatures, which are associated with measurement of energy and location, are not pictures in the IMINT sense. Currently called the Satellite Early Warning System (SEWS), the program is the descendant of several generations of Defense Support Program]] (DSP) spacecraft,<ref name=Richelson1999>{{citation | ||
| title = America's Space Sentinels: DSP Satellites and National Security | | title = America's Space Sentinels: DSP Satellites and National Security | ||
| author = | | author = Jeffrey Richelson]] | ||
| publisher = University of Kansas Press | year = 1999}}</ref> which is operated by the | | publisher = University of Kansas Press | year = 1999}}</ref> which is operated by the Fourteenth Air Force]]. Originally, DSP was known by the classified name Program 949, and, after that became known, Program 647. | ||
The fUSSR/ | The fUSSR/Russia|Russian]] Prognoz spacecraft has been described, by US sources, as having similar capabilities to DSP.<ref name=IOSS3>{{citation | ||
| url = http://www.fas.org/irp/nsa/ioss/threat96/part03.htm | | url = http://www.fas.org/irp/nsa/ioss/threat96/part03.htm | ||
| title = Operations Security Intelligence Threat Handbook, Section 3, Adversary Foreign Intelligence Operations | | title = Operations Security Intelligence Threat Handbook, Section 3, Adversary Foreign Intelligence Operations | ||
Line 104: | Line 104: | ||
}}</ref> | }}</ref> | ||
Originally intended to detect the intense heat of an | Originally intended to detect the intense heat of an ICBM]] launch, this system proved useful at a theater level in 1990-1991. It detected the launch of Iraqi SS-1 SCUD]] missiles in time to give early warning to potential targets. | ||
===Air platforms=== | ===Air platforms=== | ||
First used for | First used for technical intelligence]], the RC-135 COBRA BALL]] system now has the potential to significantly assist theater-based ballistic missile defense]], by giving detailed tracking after launch. Similar sensors may be mounted on future unmanned aerial vehicle]]s. | ||
===Next-generation satellite platforms=== | ===Next-generation satellite platforms=== | ||
{{seealso|Space-Based Infrared System}} | {{seealso|Space-Based Infrared System}} | ||
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| url = http://www.st.northropgrumman.com/media/SiteFiles/mediagallery/factsheet/STSS2.pdf | | url = http://www.st.northropgrumman.com/media/SiteFiles/mediagallery/factsheet/STSS2.pdf | ||
| title = Space Tracking and Surveillance System (STSS) | | title = Space Tracking and Surveillance System (STSS) | ||
| author = | | author = Northrop Grumman]]}}</ref> As opposed to DSP and SBIRS, which basically detect the point of origin]] (POO) of a launch and its general direction, STSS actually can track the missiles. | ||
It has been confusing to some that while SBIRS is, indeed, an intellicence system, it is also a fundamental part of modern | It has been confusing to some that while SBIRS is, indeed, an intellicence system, it is also a fundamental part of modern ballistic missile defense]], its funding is not included in the budget of the Missile Defense Agency]]. <ref>{{citation | ||
| http://www.slate.com/id/2243759?nav=wp | | http://www.slate.com/id/2243759?nav=wp | ||
| url = Watch What They Spend, Not What They Say" The Obama administration says missile defense isn't as important as it used to be. Its budget says otherwise. | | url = Watch What They Spend, Not What They Say" The Obama administration says missile defense isn't as important as it used to be. Its budget says otherwise. | ||
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==Optical Measurement of Nuclear Explosions== | ==Optical Measurement of Nuclear Explosions== | ||
There are several distinctive characteristics, in the range of visible light, from nuclear explosions. One of these is a characteristic "dual flash" measured by a | There are several distinctive characteristics, in the range of visible light, from nuclear explosions. One of these is a characteristic "dual flash" measured by a bhangmeter]]. This went into routine use on the Vela (satellite) |advanced Vela]] nuclear detection satellites, first launched in 1967. The earlier Velas only detected X-rays, gamma rays, and neutrons. | ||
The bhangmeter technique was used earlier, in 1961, aboard a modified US KC-135B aircraft monitoring the preannounced Soviet test of | The bhangmeter technique was used earlier, in 1961, aboard a modified US KC-135B aircraft monitoring the preannounced Soviet test of Tsar Bomba]], the largest nuclear explosion ever detonated.<ref>{{cite web | ||
| url = http://nuclearweaponarchive.org/Russia/TsarBomba.html | | url = http://nuclearweaponarchive.org/Russia/TsarBomba.html | ||
| title = Big Ivan, The Tsar Bomba (“King of Bombs”): The World's Largest Nuclear Weapon | | title = Big Ivan, The Tsar Bomba (“King of Bombs”): The World's Largest Nuclear Weapon | ||
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| last = Office of the Historian, Strategic Air Command | | last = Office of the Historian, Strategic Air Command | ||
| title = History of SAC Reconnaissance Operations, FY 1974 | | title = History of SAC Reconnaissance Operations, FY 1974 | ||
| url = http://www.gwu.edu/~nsarchiv/NSAEBB/NSAEBB184/FR29.pdf}}</ref> This operation is borderline with | | url = http://www.gwu.edu/~nsarchiv/NSAEBB/NSAEBB184/FR29.pdf}}</ref> This operation is borderline with Nuclear MASINT]]. | ||
Bhangmeters on Advanced Vela satellites detected the what is variously called the | Bhangmeters on Advanced Vela satellites detected the what is variously called the Vela Incident]] or South Atlantic Incident, on 22 September 1979. Different reports have claimed that it was, or was not, a nuclear test, and, if it was, probably involved South Africa]] and possibly Israel]]. France]] and Taiwan]] have also been suggested. Only one bhangmeter detected the characteristic double-flash, although US Navy hydrophone]]s suggest a low-yield blast. Other sensors were negative or equivocal, and no definitive explanation has yet been made public. | ||
==LASER MASINT== | ==LASER MASINT== |
Revision as of 07:27, 18 March 2024
This article may be deleted soon. | ||
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Electro-optical MASINT is a subdiscipline of measurement and signature intelligence]] (MASINT), which has similarities to but complements imagery intelligence]] (IMINT). The basic model of IMINT is taking a photograph, perhaps using techniques that record information not visible to the unassisted human eye, but a picture nonetheless. It may take significant skill to interpret objects in that picture, but the interpretation still depends on visual metaphors such as shape, size, and shadow. Electro-optical MASINT helps validate the elements of that picture, so that, for example, the analyst can tell if an area of green is vegetation or camouflage paint. Electro-optical MASINT also generates information on phenomena that emit, absorb, or reflect electromagnetic energy in the infrared]], visible light]], or ultraviolet]] spectra, phenomena where a "picture" is less important than the amount or type of energy reported. For example, a class of satellites, originally intended to give early warning of rocket launches based on the heat of their exhaust, reports energy wavelengths and strength as a function of location(s). There would be no value, in this specific context, to seeing a photograph of the flames coming out of the rocket. Subsequently, when the geometry between the rocket exhaust and the sensor permits a clear view of the exhaust, IMINT would give a visual or infrared picture of its shape, while electro-optical MASINT would give, either as a list of coordinates with characteristics, or a "false-color" image, the temperature distribution, and spectrometry|spectrometric]] information on its composition. In other words, MASINT may give warning before characteristics visible to IMINT are clear, or it may help validate or understand the pictures taken by IMINT. MASINT techniques are not limited to the United States, but the U.S. distinguishes MASINT sensors from others more than do other nations. According to the United States Department of Defense]], MASINT is technically derived intelligence (excluding traditional imagery IMINT]] and signals intelligence SIGINT]]) that – when collected, processed, and analyzed by dedicated MASINT systems – results in intelligence that detects, tracks, identifies, or describes the signatures (distinctive characteristics) of fixed or dynamic target sources. MASINT was recognized as a formal intelligence discipline in 1986.[1] Another way to describe MASINT is "a "non-literal" discipline. It feeds on a target's unintended emissive byproducts, the "trails" of thermal energy, chemical or radio frequency emission that an object leaves in its wake. These trails form distinct signatures, which can be exploited as reliable discriminators to characterize specific events or disclose hidden targets"[2] As with many branches of MASINT, specific techniques may overlap with the six major conceptual disciplines of MASINT defined by the Center for MASINT Studies and Research, which divides MASINT into Electro-optical, Nuclear, Geophysical, Radar, Materials, and Radiofrequency disciplines.[3] MASINT collection technologies in this area use radar, lasers, staring arrays in the infrared and visual, to point sensors at the information of interest. As opposed to IMINT, MASINT electro-optical sensors do not create pictures. Instead, they would indicate the coordinates, intensity, and spectral characteristics of a light source, such as a rocket]] engine, or a missile reentry vehicle]]. Electro-optical MASINT involves obtaining information from emitted or reflected energy, across the wavelengths of infrared]], visible]], and ultraviolet]] light]]. Electro-optical techniques include measurement of the radiant intensities, dynamic motion, and the materials composition of a target. These measurements put the target in spectral and spatial contexts. Sensors used in electro-optical MASINT include radiometers, spectrometers, non-literal imaging systems, lasers, or laser radar (LIDAR]]).[4] Observation of foreign missile tests, for example, make extensive use of MASINT along with other disciplines. For example, electro-optical and radar tracking establish trajectory, speed, and other flight characteristics that can be used to validate the TELINT]] telemetry intelligence being received by SIGINT sensors. Electro-optical sensors, which guide radars, operate on aircraft, ground stations, and ships. The major subdisciplines of electro-optical MASINT are:
Airborne Electro-Optical Missile Tracking MASINTU.S. RC-135 COBRA BALL]] aircraft have MASINT sensors that are "...two linked electro-optical sensors -- the Real Time Optics System (RTOS) and the Large Aperture Tracker System (LATS). RTOS consists of an array of staring sensors encompassing a wide field of regard for target acquisition. LATS serves as an adjunct tracker. Due to its large aperture, it has significantly greater sensitivity and resolving power than the RTOS, but is otherwise similar.[5] There is a broader program to standardize the architecture of the various RC-135 aircraft, so that there will be greater commonality of parts, and some ability to switch missions: a COBRA BALL will be able to carry out some SIGINT missions of the RC-135 RIVET JOINT#RC-135V/W Rivet Joint |RIVET JOINT]] RC-135. COBRA BALL MASINT#Cueing |cues]] the COBRA DANE ground radar and the COBRA JUDY ship-based radar. See Radar MASINT]]. This application is for technical intelligence]]; see #Long-range missile tracking|Long-range missile tracking]] for the use of these sensors in ballistic missile defense]]. Electro-optical artillery detection MASINTBoth electro-optical and radar sensors have been coupled with acoustic sensors in modern counter-artillery systems. Electro-optical sensors are directional and precise, so need to be cued by acoustic or other omnidirectional sensors. The original Canada|Canadian]] geophysical MASINT#Counterbattery and Countersniper Location and Ranging|sensors]], in the First World War]], used visual observation and plotting of flash, as well as geophysical MASINT| acoustic]] sensors. Purple HawkComplementing Radar MASINT#Counterartillery Radar |counter-mortar radar]] is the Israel|Israeli]] Purple Hawk mast-mounted electro-optical sensor, which detects mortars and provides perimeter security. The device, remotely operated via fiber optics or microwave, is intended to have a laser designator.[6] Rocket Launch SpotterA newer U.S. system couples an electro-optical and an acoustic system to produce the Rocket Artillery Launch Spotter (RLS).[7] RLS combines components from two existing systems, the Tactical Aircraft Directed Infra-Red Countermeasures (TADIRCM) and the UTAMS . The two-color infrared sensors were originally designed to detect surface-to-air missiles for TADIRCM. Other TADIRCM components also have been adapted to RLS, including the computer processors, inertial navigation units (INU), and detection and tracking algorithms. It is an excellent example of MASINT#Cueing |automatic cueing]] of one sensor by another. Depending on the application, the sensitivity|sensitive]] but less selectivity|selective]] sensor is either acoustic or nonimaging electro-optical. The selective sensor is forward-looking infrared]] (FLIR). RLS uses two TADIRCM sensors, an INU, and a smaller field-of-view single-color (FLIR) camera on each tower. The INU, which contains a GPS receiver, allows the electro-optical sensors to align to the azimuth and elevation of any detected threat signature. The basic system mode is for rocket detection, since a rocket launch gives a bright flare. In basic operation, RLS has electro-optical systems on three towers, separated by 2 to 3 kilometers, to give omnidirectional coverage. The tower equipment connects to the control stations using a wireless network. When a sensor measures a potential threat, the control station determines if it correlates with another measurement to give a threat signature. When a threat is recognized, RLS triangulates the optical signal and presents the Point of Origin (POO) on a map display. The nearest tower FLIR camera then is cued to the threat signature, giving the operator real-time video within 2 seconds of detection. When not in RLS mode, the FLIR cameras are available to the operator as surveillance cameras. Mortar launches do not produce as strong an electro-optical signature as does a rocket, so RLS relies on acoustic signature cueing from an Geophysical MASINT#UTAMS |Unattended Transient Acoustic Measurement and Signal Intelligence System (UTAMS)]]. There is an UTAMS array at the top of each of the three RLS towers. The tower heads can be rotated remotely. Each array consists of four microphones and processing equipment. Analyzing the time delays between an acoustic wavefront’s interaction with each microphone in the array UTAMS provides an azimuth of origin. The azimuth from each tower is reported to the UTAMS processor at the control station, and a POO is triangulated and displayed. The UTAMS subsystem can also detect and locate the point of impact (POI), but, due to the difference between the speeds of sound and light, it may take UTAMS as long as 30 seconds to determine the POO for a rocket launch 13 km away. This means UTAMS may detect a rocket POI prior to the POO, providing very little if any warning time. but the electro-optical component of RLS will detect the rocket POO earlier. Short-range aircraft and missile trackingInfrared tracking has long been used for missile guidance, first with air-to-air missile]]s such as the AIM-9 Sidewinder]], but also with MANPADS]] such as the 9K31 Strela-1]] (Western: SA-9 GASKIN]]). Pure infrared sensors, however, are vulnerable to being decoyed by hot flares. While newer infrared seekers use additional wavelengths and pattern recognition that can discriminate flares, another approach has been to add ultraviolet]] sensors, or to replace them completely. For example, the FIM-92 Stinger]] short-range antiaircraft missile uses "dual-band" infrared and ultraviolet guidance. The AAR-54, a representative missile warning receiver]], primarily intended for use on aircraft, uses pure ultraviolet detection, although missile warning receivers increasingly use multiple electro-optical wavelengths, and may cue radar onto the missile track. Long-range missile trackingBoth aircraft and satellite based sensors can be used to track long-range missile launches, both for strategic warning of ICBM]] launch, and tactical warning and tracking of theater ballistic missile]]s. Initial space-basedThe US, in 1970, launched the first of a series of space-based staring array]] sensors that detected and located infrared heat signatures, typically from rocket motors but also from other intense heat sources. Such signatures, which are associated with measurement of energy and location, are not pictures in the IMINT sense. Currently called the Satellite Early Warning System (SEWS), the program is the descendant of several generations of Defense Support Program]] (DSP) spacecraft,[8] which is operated by the Fourteenth Air Force]]. Originally, DSP was known by the classified name Program 949, and, after that became known, Program 647. The fUSSR/Russia|Russian]] Prognoz spacecraft has been described, by US sources, as having similar capabilities to DSP.[9] Originally intended to detect the intense heat of an ICBM]] launch, this system proved useful at a theater level in 1990-1991. It detected the launch of Iraqi SS-1 SCUD]] missiles in time to give early warning to potential targets. Air platformsFirst used for technical intelligence]], the RC-135 COBRA BALL]] system now has the potential to significantly assist theater-based ballistic missile defense]], by giving detailed tracking after launch. Similar sensors may be mounted on future unmanned aerial vehicle]]s. Next-generation satellite platforms
DSP is to be succeeded by the Space-Based Infrared System (SBIRS). DSP and SBIRS give worldwide coverage, but are really optimized for ICBMs. SBIRS High continues to be the name for the part of this system that operates from geosynchronous orbit, but the names of the low earth orbit components keep changing. A lower-altitude constellation can give faster warning of short-range ballistic missile launches, important at the theater level. The U.S. system for this purpose has gone through several redirections and name changes, including SBIRS-Low, BRILLIANT EYES, and now Space Tracking and Surveillance System (STSS). [10] As opposed to DSP and SBIRS, which basically detect the point of origin]] (POO) of a launch and its general direction, STSS actually can track the missiles. It has been confusing to some that while SBIRS is, indeed, an intellicence system, it is also a fundamental part of modern ballistic missile defense]], its funding is not included in the budget of the Missile Defense Agency]]. [11] Optical Measurement of Nuclear ExplosionsThere are several distinctive characteristics, in the range of visible light, from nuclear explosions. One of these is a characteristic "dual flash" measured by a bhangmeter]]. This went into routine use on the Vela (satellite) |advanced Vela]] nuclear detection satellites, first launched in 1967. The earlier Velas only detected X-rays, gamma rays, and neutrons. The bhangmeter technique was used earlier, in 1961, aboard a modified US KC-135B aircraft monitoring the preannounced Soviet test of Tsar Bomba]], the largest nuclear explosion ever detonated.[12] The US test monitoring, which carried both broadband electromagnetic and optical sensors including a bhangmeter, was named SPEEDLIGHT. As part of Operation BURNING LIGHT, one MASINT system photographed the nuclear clouds of French atmospheric nuclear tests to measure their density and opacity.[13] [14] This operation is borderline with Nuclear MASINT]]. Bhangmeters on Advanced Vela satellites detected the what is variously called the Vela Incident]] or South Atlantic Incident, on 22 September 1979. Different reports have claimed that it was, or was not, a nuclear test, and, if it was, probably involved South Africa]] and possibly Israel]]. France]] and Taiwan]] have also been suggested. Only one bhangmeter detected the characteristic double-flash, although US Navy hydrophone]]s suggest a low-yield blast. Other sensors were negative or equivocal, and no definitive explanation has yet been made public. LASER MASINTThis discipline includes both measuring the performance of lasers of interest, and using lasers as part of MASINT sensors. With respect to foreign lasers, focus of the collection is on laser detection, laser threat warning, and precise measurement of the frequencies, power levels, wave propagation, determination of power source, and other technical and operating characteristics associated with laser systems strategic and tactical weapons, range finders, and illuminators. [4] In addition to passive measurements of other lasers, the MASINT system can use active lasers (LIDAR) for distance measurements, but also for destructive remote sensing that provides energized material for spectroscopy. Close-in lasers could do chemical (i.e., materials MASINT) analysis of samples vaporized by lasers. Laser systems are largely at a proof of concept level.[15] One promising area is a synthetic imaging system that would be able to create images through forest canopy, but the current capability is much less than existing SAR or EO systems. A more promising approach would image through obscurations such as dust, cloud, and haze, particularly in urban environments. The laser illuminator would send a pulse, and the receiver would capture only the first photons to return, minimizing scattering and blooming. Use of LIDAR for precision elevation and mapping is much closer, and again chiefly in urban situations. References
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