F35 - superfighter or lame duck?

In fact since you've purposely exaggerated just about every argument I've made about why what you're saying wouldn't work, I'll go ahead and clarify in this post and refer to it going forward. That way when you state what I "believe" it will be easier to set you straight.

1. I'm not saying there is only one or a limited number of Russian jets

2. I'm not saying Russians cannot use radars or IR sensors, they can use whatever they want

3. I'm not saying Russians only get one jammer, you can include as many as you want

4. I'm not saying unlimited USA jets in the skies

5. I'm not saying stealth is infallible

I'm sure you'll think of another straw man argument, and equally sure you're repeat these, but we'll just add to the list as you continue to make them up.

Just keep digging, cupcake. The hole just gets deeper.
 
You can stop this anytime you wish. I am NOT Monobreath. You can try and change the subject, red herring and more all you wish but I have the experience and you don't and can look back at the history of the United States Air Force without Google or any other help. I also have an extensive background in Military Air History that you don't have. So keep going. The more you dig, the deeper the hole. You may wish to just stop digging sometime.
Speaking of red herring, this is an entire post that neither addresses absolutely nothing in the thread other than implying I should believe you because you think you know a lot. I don't accept that, and I would hope you wouldn't either.

So, still waiting on the technical specs on why the SU-27s IR system is so much better than the IR system the uses to train with on aggressor squadron F-16s. You threw that out there as fact but sure lost interest quickly when asked to provide specifics. Should be an easy one you could try to pull off since you've clearly been unable to express how barrage jamming makes it a WVR fight despite the flailing with AMRAAMs going ballistic, standoff jamming used against fast moving air targets that you don't even know are in the sky, stealth fighters with massive situational awareness advantage deciding to broadcast their position by jamming radars that you said weren't even on, deception jammers being used in the same space as noise jamming, nose mounted IRST seeing an F-22 approaching from behind, and all the other hilarious notions you've dreamed up in this thread so far.
 
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Just keep digging, cupcake. The hole just gets deeper.
Hey man I had to make that post because you were leaning so much on making up straw man arguments. It'll save me some typing just being able to reference those points that clarify I don't believe any of those exaggerated positions you're attempted to attribute to me.
 
Just keep digging, cupcake. The hole just gets deeper.
Hey man I had to make that post because you were leaning so much on making up straw man arguments. It'll save me some typing just being able to reference those points that clarify I don't believe any of those exaggerated positions you're attempted to attribute to me.

Actually, you should be scared to know that most of what I posted would be a reality if it came to that. And that is exactly the reason it won't happen. It scares them as much as it scares me. So both sides claim that they would win and no one dies today.
 
You can stop this anytime you wish. I am NOT Monobreath. You can try and change the subject, red herring and more all you wish but I have the experience and you don't and can look back at the history of the United States Air Force without Google or any other help. I also have an extensive background in Military Air History that you don't have. So keep going. The more you dig, the deeper the hole. You may wish to just stop digging sometime.
Speaking of red herring, this is an entire post that neither addresses absolutely nothing in the thread other than implying I should believe you because you think you know a lot. I don't accept that, and I would hope you wouldn't either.

So, still waiting on the technical specs on why the SU-27s IR system is so much better than the IR system the uses to train with on aggressor squadron F-16s. You threw that out there as fact but sure lost interest quickly when asked to provide specifics. Should be an easy one you could try to pull off since you've clearly been unable to express how barrage jamming makes it a WVR fight despite the flailing with AMRAAMs going ballistic, standoff jamming used against fast moving air targets that you don't even know are in the sky, stealth fighters with massive situational awareness advantage deciding to broadcast their position by jamming radars that you said weren't even on, deception jammers being used in the same space as noise jamming, nose mounted IRST seeing an F-22 approaching from behind, and all the other hilarious notions you've dreamed up in this thread so far.

I will as soon as I get back from my next sooper secrit mission spying on Russian Military. But until then, you will just have to believe that the Russians/Soviets have had IRST for decades while the US has not. In fact, only about a handful of Guard F-15Cs and 16s have it installed today. And, yes, the agressor squadron of F-16s have it installed. As well as about 500 F-18E/F and Gs. And it works. The longer your Stealth bird stays in the air, the more fuel he burns and the less IR masking he can do through his fuel heat masking. And it will depend on the distance the Us fighter has to fly to get to the battle whether he has an effective fuel load that he can keep his rearward most tanks full or not. Even the F-22 can't mask his engine exhaust heat without the help of the fuel masking. Here is a very good article and a very recent one for the US Military Air about Ir defenses.

The Pentagon Has Figured Out How to Hunt Enemy Stealth Fighters
 
Spending so extraordinarily on this one system has cost dearly to alternatives that would be more advantageous, all in order to preserve the outdated thinking of backward-looking militarists.
 
Here is a very good article on IRST versus Radar.

Airborne IRST properties and performance



Airborne IRST properties and performance
Posted by Picard578 on June 16, 2015

Introduction

IRST is a sensory device which uses IR (infrared) radiation for detection and targeting purposes. IR radiation has wavelength of 0,75 to 1.000 microns (micrometers), longer than wavelengths of color red in the visible spectrum (visible spectrum ranges from 0,39 to 0,7 microns, with violet at 0,4 and red at 0,7 microns). It is given off by all objects above absolute zero, though objects that are below average temperature of their surroundings will absorb far more IR radiation than they will give out. Unlike FLIR which is a targeting device, IRST can be used for initial detection as well.

Infrared radiation is divided into near infrared (0,75 – 1,4 microns), shortwave infrared (1,4 – 3 microns), midwave infrared (3 – 8 microns), longwave infrared (8 – 15 microns) and far infrared (15 – 1.000 microns). These have different properties. For example, glass is opaque to LWIR band but transparent to SWIR band, and significantly degradess image in MWIR band. MWIR sensors are far better at penetrating fog and clouds than other wavelengths, while LWIR sensors have superior atmospheric performance. As a result, while SWIR sensors can use glass, MWIR and LWIR sensors have to use exotic materials such as germanium and sapphire. 5-7 micron band suffers 100% absorption by water particles.

IR bands are also associated with temperatures of bodies producing radiation. Visible light is associated with temperatures above 1.000 *C. Next come IR bands: 0,7-4 microns (1.000 – 400 *C); 5-25 microns (400 – -150 *C) and 25-350 microns (this is a civilian, not military, division). Bodies at room temperature have radiation peak at around 10 microns, while 3-5 micron band is used in civilian applications for its effectiveness in tropical conditions.

In civillian purposes, astronomers use IR telescopes to penetrate dusty regions of space that block off visible light. NASA also has an airborne IR system – SOFIA (Stratospheric Observatory for Infrared Astronomy) which is flown at altitudes of over 41.000 ft, allowing 85% of the entire IR spectrum to reach it. Its service ceilling is 45.000 ft.

First IRSTs were deployed in 1950s on F-101, F-102 and F-106 interceptors. They were also used in F-8E, F-4 (B and C models only) and Swedish J-35A and J-35F-2 (1965-1967). However, they were primitive and were slaved to the radar, as opposed to modern-day independent systems. Any IR radiation falling on the sensor would generate a blip; consequential high false alarm rate meant that IRST was typically only used for (manual) radar targeting.

In 1960s and 1970s, Soviets deployed IRST units on their MiG-23, MiG-31, Su-27 and MiG-29 fighters. This was intended to provide passive BVR surveillance capability to fighters, and also as a way of countering Western advantage in radar technology and countermeasures. In fact, MiG-23 and MiG-31 interceptors were able to track the SR-71 recon aircraft from large distance, possibly up to 100 kilometers. This was despite the fact that the system was rather primitive, and that MiG-31s own skin and canopy would reach temperatures of over 760 degrees Celsius during the intercepts. MiG-23 had an IRST capable of detecting the F-16 at 35-40 km head on and 60 km from the rear. Later developments of Su-27 and MiG-29 families all have internal IRST.

General IRST properties

Due to relatively shorter wavelength, IRST is more sensitive than radar to adverse weather conditions. Much of the infrared radiation is absorbed by water vapor, carbon dioxide, methane and ozone. However, there are two wavelength “windows” in which very little infrared radiation is absorbed by the atmosphere. These windows are at 3-5 and 8-12 microns. Both modern IRSTs and modern IR missile seekers typically operate in both bands. 3-5 mM band is optimized for detection of aircraft in afterburner, while 8-12 mM band is better suited for detection of subsonic or supercruising aircraft through aerodynamic heating of skin. More specifically, afterburner exhaust plume is more prominent in midwave than in logwave band, with most emissions being in 2-8 mM wavelength band, while emissions from nonafterburning plume are only useful in 4,15-4,2 mM band. Blackbody radiation from a warm object is most prominent in 10-15 mM band, and only objects above ~300 K give appreciable MWIR emissions (still inferior to to LWIR band). As a result, LWIR detectors have good sensitivity against targets at ambient temperatures.

Unlike other IR bands, these two bands are comparatively altitude-insensitive when it comes to detection performance, as it can be seen from an IR absorpion chart in the next section; they are also less affected by water content. Comparing both bands, 3-5 mM band is less affected by aerosoil while 8-12 mM band has longer detection range and is less affected by clouds. Consequently, up until appearance of dual-band systems, midwave band was preferred for ground attack while longwave band was preferred for air-to-air usage.

While IRSTs can detect even relatively cool targets through thin cloud cover, detection range is reduced (more than it is in case of radar), and thicker clouds can significantly degrade detection range. As a result, IRST is most useful for air superiority fighters, which typically operate at 30.000 ft and above – well above normal cloud cover and in relatively thin atmosphere.* ** Only clouds typically present at altitudes above 8 km (~26.000 ft) are those of cirrus variety, which are IR transparent. While dense cumulonimbus clouds can reach extreme heights (60.000-75.000 ft), it is very rare; vast majority does not reach above 20.000 ft. They are also very hazardous to aircraft (especially those of stealth variety), with frequent lightning discharges and large hailstones ranging from 0,5 to 5 cm in diameter, which can damage aircraft’s skin.





Due to its passive nature and shorter wavelength, IRST has major advantages over radar regarding ID capabilities and ground attack performance due to increased resolution. In particular, IRST has better ability to project image of the target (to either cockpit displays or HMD), thus giving a fighter aircraft ability to ID other aircraft at longer ranges than would be possible with radar NCTR modes. IRST also has beter capability for differentiating aircraft in formation than radar does due to better angular resolution – possibly up to 40 times more accurate than radar’s. Still, IRST might have a regular magnified optical sight added for help with identification in clear weather.

Type and location of IRST is indicative of aircraft’s mission. Air superiority fighters will have dual band or longwave system positioned in front of the canopy on upper nose surface, while ground attack aircraft will have a dual band or midwave system positioned below the nose. Dual band system is preferable in both cases as it helps eliminate clutter, though it is not as beneficial for ground attack aircraft as it is for air superiority fighters.

Major advantage over the radar is that it cannot be easily jammed. As a result, actual tracking and engagement range of IRST can be expected to be greater than that of radar, even if latter has a major advantage in initial detection range. Jamming IRST with an infrared laser is a possibility (in theory), but it is very difficult if not impossible to pull off against a maneuvering aircraft. Operating modes are similar to radar: multiple target track (permitting engagement of multiple targets; similar in nature to radar’s track while scan), single target track and slaved acquisition (where IRST is slaved to another sensor, such as radar or RWR).

Being a passive sensor, IRST alone has issues with range finding. There are some workarounds. Obvious one is laser rangefinder, but being an active sensor it means that the target is warned of the impending attack (IRST still retains its passive surveillance advantage over the radar). Second one is triangulation, which can be done in several ways: datalinking two or more aircraft together, flying in a zig-zag / weaving pattern and measuring apparent target shift, or flying in straight line perpendicular to the target while doing the same. First two are usable against aircraft, while last one is only practical against ground-based targets. Target motion analysis can also be combined with atmospheric propagation model and/or apparent size of the target in order to provide a more accurate rangefinding, or these modes can be used as standalones. Radiance difference between target and the background is also a possibility. Doppler shift may be used to provide estimate of target’s speed relative to the fighters, which can be used to help with rangefinding; this is still questionable as it does not show up well at short distances, measurement may be impeded by the atmosphere, and is typically used by platforms and against targets with relatively predictable paths, which fighters are not. Exception is radar ranging, but in this case wavelength is already known beforehand to a great degree of precision. That being said, the only determinant for Doppler shift is relative speed of sensor compared to the object emitting radiation – and modern IR sensors used in astronomy can measure velocity of a star down to 1 meter per second (relative to Earth). For comparison, speed of sound at >=40.000 ft is 294,9 meters per second, and two closing fighters will be doing it at relative speeds between Mach 1,5 and 3,6. It is questionable wether Doppler shift is, or may, be used in airborne IRST.

It should be noted that while not knowing range of the target limits maximum engagement range, it does not preclude beyond visual range engagement, as missile can fly along the line of sight towards the target. This does create issues with end-game engagement, though a missile with active radar head is capable of pulling a lead, and even one with IR head might be capable of doing so albeit with less precision. Such engagement profile is in some ways superior to the classical one, as IRST’s greater angular precision will mean less possibility of a missile flying past the target without acquiring it.

Imaging IRST can also be used as a landing aid in no or poor visibility conditions (night, fog, rain etc.). While helpful for any aircraft, this is especially important for fighter and ground attack aircraft expected to operate from austere air strips.

It should be noted that IRSTs detection range is range at which probability of detection exceeds ~95% treshold, in clear-sky conditions. Actual range at which target is detected can be higher or lower. Also, heating of sensor due to friction during high-speed flight can degrade its performance somewhat.

While modern QWIP IRSTs offer the best performance, they have to be cooled to extremely low temperatures: 65 K is not uncommon. Quantum well is a potential well in which electrons are trapped. When excited, they can be ejected from the well, and produce current if external voltage is applied. QWIP photodetector / IRST can measure how much light comes from various sources by measuring the current. The longer the wavelength of light, the less energy the light has to give the electrons and the colder the detector must be to avoid excessive thermal excitations.

IRST can use scanning or staring array. Staring sensor uses one detecting element for each part of the image within field of view. This means that all detecting elements are simultaneously exposed to the image of the object, or a frame. Standard frame rate is 30 Hz, and dwell time is equal to the frame rate (1/30 of a second). Longer dwell time results in a more sensitive detector and less noise.

Scanning system can use a single element, which then sequentially scans the instantaneous field of view (determined by the aperture). Scanning system is typically a rotaring mirror. This system is cheaper than a staring array. Its output is serial as only IFOV is directed on the detector at any one time. Dwell time is determined by both frame rate and number of pixels in the image; a system with 30 Hz refresh rate and standard VGA monitor of 640×400 pixels has a dwell time of 1/7.680.000 od a second, which leads to increased noise in the system and reduced sensitivity.

(Note that a staring array still can be mounted in a turret which can scan the area in front of the aircraft).

*French Dassault Rafale has an optronics suite (IR+visual) and radar. Radar is considered primary air-to-ground sensor, while OSF is considered primary air-to-air sensor.

** F-35, a ground attack aircraft, will also typically fly at 30.000 ft during ingress/egress.

Counter-stealth performance

It is a general wisdom that IRST is of limited usefulness due to its sensitivity to adverse weather conditions. However, most modern stealth fighters (excepting the F-35 and J-31 tactical bombers) are intended to operate at high altitudes – above 50.000 ft – where ambient temperatures range from -30 to -60 degrees Celsius, which helps provide excellent contrast. Air at this altitude is also very dry, with 99,8% of the atmospheric water being below 45.000 ft. Combined with low air density and low aerosoil content, this means that there is very little atmospheric absorption of IR radiation. This applies especially to the longwave band, but detection capability is significantly improved in most bands as can be seen from the image below.



Stealth aircraft are designed to have certain IR signature reduction measures, but effectiveness of these is rather limited due to basic physics. To fly, aircraft has to overcome two basic forces: gravity and drag. Drag is created due to friction with air, compressibility effects and lift. To overcome gravity, aircraft needs lift. To generate lift, aircraft has to move forward and overcome drag. As a result, aircraft has to perform work – which creates heat. Indeed the largest IR sources on the fighter aircraft are its engines. Jet engines work by burning fuel in order to heat up huge quantities of air, which is then propelled out of the rear in order to push the aircraft forward. This leads to significant heat – engine itself is very hot (especially turbines), as is the exhaust nozzle. Engine heats up airframe surrounding it, which can be detected. Exhaust plume is also very hot, though much of the radiation is typically absorbed by the atmosphere (this depends on the altitude – refer to the image before this paragraph).

Other than the engines themselves and their exhaust, there are other sources of IR radiation. Any moving objects have to push the air out of the way. If object is fast – for example, an aircraft flying at high subsonic or supersonic speeds – air cannot move out of the way quickly enough. This leads to compression of the air in front of the aircraft, which in turn leads to heating of said air. At Mach 1,7, a supercruising fighter generates shock cones with stagnation temperature of 87 degrees Celsius; shock cone forms above Mach 0,8 and at around Mach 1 it achieves temperature of -13 degrees Celsius. Shock cone also increases frontal area presented to the sensor about 10 times (its diameter depends largely on aircraft’s wing span). As the air moves out of the way for the aircraft, it also creates significant friction with the aircraft itself, leading to heating of the aircraft’s skin. In a jet fighter, hottest parts of the airframe other than the engine nozzles are tip of the nose, front of the canopy, as well as leading edges (of wings, tail(s) and air intakes).



As mentioned before, MiG-31 would heat up to 760 degrees Celsius during intercepts due to aerodynamic heating alone. Airframe temperature due to friction can reach -29 degrees Celsius at Mach 0,8, 54,4 degrees Celsius at Mach 1,6, 83,3 degrees Celsius at Mach 1,8 and 116,8 degrees Celsius at Mach 2,0. F-22 has two pitot tubes – one at each side of the nose – which are heated to 270* C during flight operations to prevent them from icing at high altitude. Avionics have to be cooled – especially radar. Heat exhaust is typically located at fighter’s upper surface – just behind the cockpit in Gripen, and about one canopy length behind it for the F-22. F-35 is in even worse situation since it uses fuel as a coolant, and said fuel completely surrounds its engine. This has the effect of increasing its IR signature as well as the possibility of bursting into flames if hit.

These temperatures can be compared to the ambient air (Standard US Atmosphere). F-22 achieves maximum cruise speed of Mach 1,72 at ~38.000 ft without afterburner, and maximum speed of Mach 2,0 at between 38.000 and 58.000 ft with afterburner. Above cca 53.000 ft it requires afterburner to fly, and can achieve maximum altitude of ~64.000 ft, where it is limited to maximum speed of Mach 1,6-1,8. Ambient temperature is -44,4 *C at 30.000 ft, -54,2 *C at 35.000 ft, -56,5 *C at 40.000 ft to 60.000 ft, and -55,2 *C at 70.000 ft. That is to say, difference between shock cone of a M 1,7 F-22 and ambient air will be around 130-145 * C, while temperature difference between airframe and ambient air will be cca 111 * C at Mach 1,6 and cca 172 * C at Mach 2,0. At Mach 1 difference will be 31-44 * C between shock cone and the ambient air; difference in temperature between airframe and ambient air will be 15-27 * C at Mach 0,8.

IRST sensor of Dassault Rafale’s OSF can, at 20.000 ft, detect a subsonic fighter-sized target at 80 km from the front and 130 km from the rear. At low altitude, range from the rear is 110 km, which would indicate frontal range of 68 km. F-22 achieves supercruise speed of Mach 1,72-1,75 at 38.000 ft. Assuming similar increase in range between 20.000 and 40.000 ft, OSF should be able to detect the subsonic F-22 at distance of 90-95 km from the front and 145-155 km from the rear. If F-22 is supercruising at Mach 1,70 and 40.000 ft (about the limit of its supercruise performance at that altitude), range increases to 270-285 km from the front and 435-465 km from the rear.

While fighter’s IR signature can be reduced by reducing speed, such course of action also has the effect of reducing one’s own weapons range, as well as making a rear-quarter surprise more likely. In either case, fighter will get detected by modern QWIP IRST before it reaches missile effective range (10-40 km for AIM-120D at most, and can be as low as 2 km).

It is possible to apply IR absorbent paints to a fighter in order to reduce IR emissions from systems inside it. This, at best, does not have any impact on aerodynamic heating. Some IR absorbent paints cause more friction than would otherwise be the case, increasing aerodynamic heating. RAM coatings also can increase friction. While it is not a significant factor in MWIR band, LWIR detectors can detect aircraft by detecting sunshine reflections from its surfaces, such as canopy.

Modern IRST systems can even detect missile launch from its nose cone heating – this is in fact a significant advantage for IR MAWS, as UV MAWS cannot detect missiles that have spent fuel. They are also sensitive enough for planets, birds, and (in air-to-ground) barbecue grills to be sources of clutter.

Note that even if an object is at the exact same temperature as its environment, it still emits blackbody radiation, most of it at longer wavelengths.

Tactical impact

Unlike radar, IRST is primarily a passive system. This allows a fighter aircraft, or a fighter group, to detect and track the enemy without latter being aware of their presence, thus gaining a significant initial advantage in the OODA loop. Even when the enemy is aware of the fighter’s presence, he has no way of knowing wether he has been detected, or is being targeted, until a significant shift in fighters’ posture (such as painting target with a rangefinder or shifting flight path or formation). For comparison, just turning on the radar warns the aircraft in very large area of scanning fighter’s presence – and said area is far larger than one covered by the radar. Not only does it give away fighter’s presence, but if the enemy has good enough listening equipment, it is possible to triangulate location and even identify the target through its unique radar signals. Even radio communications and datalinks can serve the same purpose.

If the enemy is using radar, it is possible to use data from radar warner to generate a bearing, after which IRST can be used in a “stare” mode – continuous track, during which photon impacts are combined over prolonged timeframe to detect a target at greater distances than would normally be possible. This mode is also present in radar systems, and like IRST, radar also has to be cued by other sensors to make use of it. But while using radar in such a manner basically guarantees than the enemy with a competent RWR will detect radar transmissions, IRST is undetectable. Even a short radar burst can allow the passive fighter to generate such bearing, albeit it will somewhat limit the precision.

If radars are jammed, or more likely turned off for fear of detection, first indication of IRST-equipped fighter’s presence that the enemy aircraft will get may be alarm from a missile warning system (or radar warning system if missile is using an active seeker), thus allowing only a short time for defensive reaction. (Simulated trials of ECR-90 have shown that its airborne detection range could be cut to less than 9 kilometers by jamming). If both sides have IRST, it comes down to sensor quality and IR signature differences.

Aircraft equipped with IRST, and using IR MAWS, can remain completely silent during the mission. If the enemy has no IRST, then he will have to turn on his own radar(s), allowing the passive aircraft excellent situational awareness, well beyond what using radar in addition to IRST would allow. Further, active usage of radar will allow geolocation of radar emitters, allowing the passive fighter to use IRST to engage such targets with high precision – thus gaining a “see first, strike first” capability. IRST-equipped aircraft is also not vulnerable to anti-radiation missiles. (Note that such missiles are not very hard to make, with basically all air-to-air engagement radars being in X band).

IRSTs shortcomings can be compensated for by using datalinks to network the fighter with other assets, such as other IRST-equipped fighters and radar-equipped AWACS. As a result, radar is not the primary onboard sensor any more, and is not actually even required.

Using datalink from AWACS (though AWACS is unlikely to survive for long in a shooting war) or ground radars, fighter can then approach the enemy from side or rear, in order to prevent detection by enemy’s own radar and maximize IRSTs detection range. Once target is acquired on IRST, fighter can pursue engagement completely independently. Of course, if enemy fighter uses its own radar, no AWACS is required. It should be noted that most, possibly all, fighter aircraft today lack the datalink capable of transferring amount of data necessary for a firing solution. Even if such datalink is deployed, it will be easy to jam. As a result, fighters have to rely on onboard sensors to create a firing solution (when Rafale shot down a target at 6 o’clock, shot was done with onboard sensors and within visual range; F-35 may have a similar capability).

Large radar-based fighters – such as the F-15, F-22, Flanker variants – can act as AWACS of sorts, providing radar image to smaller IRST-only fighters, which can then use such image to achieve optimal position for a surprise attack. This in turn will allow IRST-equipped fighters to focus the IRST and achieve detection ranges larger than could normally be achieved. Even if radars are jammed, radar-based fighters should be able to roughly tell positions of enemy fighters, unless DRFM, active cancellation or standoff jamming is used. Using IRST to generate a firing solution, and then launching an IR BVRAAM or ramjet RF BVRAAM (or, ideally, a ramjet IR BVRAAM, though such missile does not exist in Western inventory) at a surprised opponent will allow far higher kill probabilities than using an obvious radar for firing solution.

Still, using an AWACS with a huge IRST plus extensive ESM arrays might allow the same tactics without a drawback of warning the enemy that he has been detected, and without suffering vulnerability to decoys and jamming that radar has. Additional advantage of such system is that its effectiveness will not be significantly degraded even against VLO targets. On the other hand, while bad weather degrades IRSTs performance, it also degrades performance of stealth coatings (assuming that stealth fighters can safely enter storm clouds), thus combining radar AWACS with IRST-equipped fighters does make some sense, as does using both types of AWACS.

IRST is the best solution for engaging stealthy aircraft and cruise missiles. As it can be seen from the previous section, is impossible to significantly reduce IR signature of a high-speed, highly maneuverable aircraft, and even low-performance aircraft that do have very extensive IR signature reduction measures are still detectable at large distances by new QWIP imaging IRSTs. Even against “legacy” aircraft its is a better choice than radar, as radar cannot separate valid contacts from decoys except at very short range – especially if it is being jammed. As a result, only IRST-equipped fighters can effectively engage modern fighters at beyond visual range.

IRST can be used as a relatively cheap way of turning an old, possibly even WVR-only, platform into one capable of BVR combat. With PIRATE + MICA IR combination, even an old F-86 would gain a capability to shoot down enemy fighters from beyond visual range (that being said, issues of low cruise speed, deficient acceleration by today’s standards and no defense suite at all would remain, and would mean that even against the F-35, F-86 would not achieve positive kill/loss ratio).

Analytic simulations indicate that an IRST-equipped aircraft will have 230% better exchange ratio than a non-IRST equipped aircraft against a “legacy” target, and 370% better against a LO target.

Specific IRST systems

PIRATE

PIRATE is used by Eurofighter Typhoon, and it entered service in 2007. Its lead contractor is Selex ES. Selex holds the bulk of Western experience in IRST systems, and is also a sole supplier of the Skyward G IRST. Thales, another member of the Eurofirst consortium, also has extensive experience in the area.

PIRATE is a dual-band system (3-5 and 8-10 microns), combining long range detection capability of the longwave IRST with high resolution and all-weather performance of midwave one. It can track more than 200 targets, and has 140* field of regard in azimuth, with -15* depression angle. Sensor head weights 48 kg, with 60 kg (?) total weight.

Detection range against a subsonic fighter-sized target is 90 km from the front and 145 km from the rear. It has an ID range of 40 km, and can track a maximum of 200 targets. It is stated to be capable of passive ranging. Its ability to provide infrared image (which can be shown on cockpit displays and HMD) can, aside for ID purposes, also be used to help with flight operation in low visibility conditions.

(Note that range figures for Western IRSTs are most likely measured/estimated against Su-27, a massive aircraft with no IR signature reduction measures.)

Skyward G

Skyward G is a new IRST intended for use in Gripen E/F, and represents a technological improvement (in both hardware and software) over older PIRATE IRST it is based on. It is a staring imaging IRST. It is also smaller, with sensor head weighting 30 kg. Like PIRATE, it is a dual-band system covering midwave and longwave infrared bands, and can provide IR image on pilot’s helmet. Scan coverage is 160* in azimuth and 60* in elevation.

Skyward is stated to be capable of detecting all aircraft flying faster than 300-400 kts from skin friction alone – irrespective of any exhaust plume or engine IR signature reduction measures. Range for such detection is unstated.

OSF

OSF is an optical sensors suite used by Dassault Rafale. It consists of an IRST sensor and a video camera. Like PIRATE, its IR sensor is dual-band, using 3-5 and 8-12 micron bands.

Detection range against a subsonic fighter-sized target is 80 km from the front and 130 km from the rear (at 20.000 ft; 110 km at low altitude). Optical camera has ID range of 45 km, while IRST has an ID range of 40 (?) km. It was reported to have locked on a turboprop Transall through thin cloud cover.

EOTS

EOTS is a staring IR sensor. Unlike above IRST systems, it is primarily intended for ground attack, as a replacement for various IR targeting pods. As a result, it is a single-channel midwave IR system, limiting its detection performance against nonafterburning targets and in air-to-air role but providing all-weather performance. It weights 200 lbs / 90,7 kg.

It is also obsolete when compared to modern IR pods used by US Navy (in particular, newest versions of Sniper and Litening pods), being more than a decade old as of 2015. In fact, it is basically an internal version of Sniper XR pod which entered service in 2006, and has low resolution and detection range when compared to the Legion pod. From Sniper XR demo, it appears that identification range is 24 kilometers against fighter aircraft, though the aircraft in question was on the ground, and 45 kilometers against an airborne business jet, showing ID performance at most comparable to PIRATE. This suggests lower maximum detection range as PIRATE likely uses midwave channel for identification, but also has longer-ranged longwave channel. That being said, actual detection range performance may be better than suggested here. Its configuration also allows it quicker scan speeds than with traditional IRSTs.

OLS-27

OLS-27 is used on Su-27 fighter, and has a maximum range of 70 km.

OLS-30

OLS-30 is used on Su-30 fighters. Maximum detection range might be as high as 90 km, and weights 200 kg.

OLS-35

OLS-35 is a scanning array IRST used on Su-35 fighters. Detection range is 50 km head on and 90 km from the rear against a subsonic fighter-sized target. It can track 4 targets. Sensor head weights 60 kg.

OLS-50

OLS-50 is IRST for T-50/PAK FA fighter. It is the first QWIP system deployed on Russian fighters, which suggests far higher detection range than earlier systems as well as the ability to identify targets.

IRST-21

IRST-21 is a podded system in use with US military. It has field of regard of +-70 degrees (140 degrees) in both azimuth and elevation, and total weight of 67-83 kg. Like other Western IRST systems (and presumably most Russian systems listed), it is capable of generating weapons-quality tracks.

Conclusion

While historically IRST had major performance issues, modern IRST systems, especially Western ones, have mostly solved these issues. As a result, IRST can be expected to become a primary sensor in any air war between competent opponents, for the same reasons as those that led to night vision googles being used for night fighting in place of flashlights.

While US Department of Defense has a very long history of being “late to the party” when it comes to introducing simple, yet effective (even transformative) systems*, US military is currently taking baby steps to rectifying its lag in development and application of airborne IR sensors. This can be clearly seen from the F-35s inbuilt IRST (though that decision was only made on insistence of US Navy, which was also the first service to introduce the Legion pod, and generally has better understanding of passive IR systems than USAF**), and procurement of IR pods for the F-15C, F-16 and F-18 fleets. Legion pod procured is capable of generating weapons track. US Navy is also the service that initiated development of AIM-9X Block III, which is basically a BVR missile, with a range of 42 km.

One of reasons why United States have not put funds into developing IRST, and are even now using almost exclusively systems geared for air-to-ground performance that happen to have air-to-air option, is that IRST was seen as a threat to the AWACS program, and later on also to stealth fighters. Both of these were high-budget programs that USAF could not allow to disappear. With average price of 1 million USD per unit, it would take only 3,2 billion USD to equip the entire US inventory of tactical aircraft with modern IRST systems. Allowing it to threaten the multi-billion AWACS or stealth aircraft programmes was simply unacceptable.*** For this reason, USAF is still acting as if IR sensors have not advanced past Vietnam-era sensors with their range, weather and targeting limitations. Same reason is also likely behind the decision to retire the IRST-equipped F-14 just before the F-22 started entering service (F-14s were retired in mid-2006, while the F-22 started entering service in 2007).

This might be changing as USAF agressors are starting to use IR sensors during Red Flag exercises. US’ Northrop Grumman has also signed a deal with SELEX which will bring Europe’s more advanced IRST technology to United States. This will help overcome US technological lag in field of IR systems when compared to Europe.

* Examples are assault rifles, carrier catapults, IR sensors, helmet mounted sights, HOBS IR missiles.

** US Navy was also the first service to deploy IR Sidewinder missile in 1956. US Air Force deployed a Falcon missile the same year, but it had both IR and RF variant, and unlike Sidewinder, it was primarily intended for bomber self-defense and not for usage on fighters. Even though it was later deployed on fighter aircraft as well, USN Sidewinder proved superior and became preeminent US IR air-to-air missile.

*** E-3 Sentry program cost is 26,73 billion USD, F-22 program cost is 79,48 billion USD and F-35 program cost is estimated at 323 billion USD, though it is likely to be higher.
 
Actually, you should be scared to know that most of what I posted would be a reality if it came to that. And that is exactly the reason it won't happen. It scares them as much as it scares me. So both sides claim that they would win and no one dies today.
Another post that does nothing to support your argument. We'll file this one right with the "I know more so I'm right" type posts you've already made.
 
Actually, you should be scared to know that most of what I posted would be a reality if it came to that. And that is exactly the reason it won't happen. It scares them as much as it scares me. So both sides claim that they would win and no one dies today.
Another post that does nothing to support your argument. We'll file this one right with the "I know more so I'm right" type posts you've already made.

Just keep digging. You always wanted an all expense paid vacation to China.
 
I will as soon as I get back from my next sooper secrit mission spying on Russian Military. But until then, you will just have to believe that the Russians/Soviets have had IRST for decades while the US has not.
Just as I thought, you clearly have no idea what the performance/specs on those two IR systems are when you claim the Russian one is better. You were just making stuff up and hoping I'd believe you.

Regarding your claim that Soviets have had IRST for decades while the US has not:

GyZ93UH.jpg


pi3qm1h.jpg


DG6mfL2.jpg



And, yes, the agressor squadron of F-16s have it installed.
I told you this, so I'm not sure why you're now telling me this. Point was the F-22 has dominated against aggressor F-16s with IRST and Typhoons with IRST. The German pilots said the only chance they had was when an exercise was purposely arranged to commence WVR, otherwise they had no chance since they couldn't find the F-22s and would get shot down without even knowing they were being targeted.

That is exactly waht would happen in this ridiculous scenario you have where there is some big plane trying to employ standoff jamming against other planes that it doesn't even know are in the air or where they are.... it would get shot down.
 
Just keep digging. You always wanted an all expense paid vacation to China.
Nonsensical post that doesn't help your argument that barrage jamming can force a WVR fight.

I already posted the reason that IRST is being installed on the US Fighters. And have shown that a Fighter above the Weather flying at near or above mach stands out like a sore thumb for about the same distance as it would for Radar. The F-22 super cruising at Mach 1.8 at 50K is going to be extremely hot. And the Russian IRST will be able to start picking them up at about 100 miles using their own IRST. You seem to want to leave out the other variables and Monobreath your way around this. My one post shows how this is done and why the US is working so hard to get their own IRST on as many fighters as possible. Remember, the next generation of SU-35 will have radar as good as the US front line fighters. And they can link up. In fact, when they get the SU-35 using the Aesa Radar, the Russians are very good at linking and if you have X number of IRST birds that can link at different angles they can get a launch solution for a IR Missile and that missile will have the same range as it's Radar Counterpart. All both sides need to do is to shorten the radars ability to lockon or jam X band completely to stop the incoming Amraam missiles from going active. They just need to do this long enough to let it get close enough for IR to do it's job. And believe me, the SU series will be tracking your missile through IR all the way which means, the dirty jammer can disengage and pull back out of harms way. The SU series fighters all have the ability to block or spoof or...... in X band.

Now, read my other post that explains it fully. I didn't write the explanation. Someone a lot smarter than either of us did though.

And stop digging. Or are you craving Chop Suey so much you just can't help yourself.
 
So, in your opinion, it could be a serious mess.
I'm going to have to read a lot more, but it looks dodgy on the surface.
Those jerks want their planes to look like sports cars and cover a range of fighting abilitys that are impossible to build. I know for a Fact that the USAF hated the A 10 it is a rough looking aircraft, but it shamed them because it is the best close support ac that they have had since WWII. Its called the Thunderbolt and you never want to be on the working end of it. They have updated and rebuilt it because it does the close support missions better than anything they have. Wish we had them in Nam. Its not fast, is not pretty, but it can hang around in the area and blast the hell out of anything you want. It does not make a pass and fly 5 miles to turn around for another pass. I you go to the military channel you can see how it works. The ground pounders love the Hog.
 
Just keep digging. You always wanted an all expense paid vacation to China.
Nonsensical post that doesn't help your argument that barrage jamming can force a WVR fight.

I already posted the reason that IRST is being installed on the US Fighters. And have shown that a Fighter above the Weather flying at near or above mach stands out like a sore thumb for about the same distance as it would for Radar. The F-22 super cruising at Mach 1.8 at 50K is going to be extremely hot. And the Russian IRST will be able to start picking them up at about 100 miles using their own IRST. You seem to want to leave out the other variables and Monobreath your way around this. My one post shows how this is done and why the US is working so hard to get their own IRST on as many fighters as possible. Remember, the next generation of SU-35 will have radar as good as the US front line fighters. And they can link up. In fact, when they get the SU-35 using the Aesa Radar, the Russians are very good at linking and if you have X number of IRST birds that can link at different angles they can get a launch solution for a IR Missile and that missile will have the same range as it's Radar Counterpart. All both sides need to do is to shorten the radars ability to lockon or jam X band completely to stop the incoming Amraam missiles from going active. They just need to do this long enough to let it get close enough for IR to do it's job. And believe me, the SU series will be tracking your missile through IR all the way which means, the dirty jammer can disengage and pull back out of harms way. The SU series fighters all have the ability to block or spoof or...... in X band.

Now, read my other post that explains it fully. I didn't write the explanation. Someone a lot smarter than either of us did though.

And stop digging. Or are you craving Chop Suey so much you just can't help yourself.
I bet a A10 can fly in at 50 foot hit the target and leave without getting hit.
 
But even so, at some point, the signals you are jamming will overpower the jamming signal the closer your birds get to the source. At that point, the 4th gens can be fired on first. And then the 5th gens can be fired on even closer. You may even have to use a fighter like the F-35 to do a short burst to blind a site that is stronger than the rest that has accomplished a lockon and maybe fire solution for a few minutes while it's being taken out. Not all sites will have the same range, power or capability. And neither will all Aircraft. But the EC-135 and EC-130 will be allowing the Fighters and Bombers to get a bit closer. Meanwhile, the Russians will be doing exactly the same thing with their IL birds. Then we are going to add in the Command Posts of both sides with extremely powerful radar that is just outside of launch range of the enemies attack missiles.

I'm sure hoping that this convo has stopped short of discussing classified tactical info.. That is all. I haven't read thru it all. But I'm seeing some pretty specific information being done in a public forum here.

Just sayin'....
 
I already posted the reason that IRST is being installed on the US Fighters. And have shown that a Fighter above the Weather flying at near or above mach stands out like a sore thumb for about the same distance as it would for Radar. The F-22 super cruising at Mach 1.8 at 50K is going to be extremely hot. And the Russian IRST will be able to start picking them up at about 100 miles using their own IRST.
You posted an amateur blog by someone who has never flown a fighter aircraft. That doesn't show anything, other than you desperately googled and decided it's a "good article" because you like it's conclusions.

Still waiting for your technical analysis to back up what you said about Russian IRST sensors being superior to those used by aggressor squadron, given you thought US hasn't had them for decades I'm even more skeptical that you know anything about them. Here I'll even give you a hand, this is the IRST system used on Flankers, specs given are for the latest one:

FmP5JDW

zKRtGSU.jpg


Hilariously, you're saying 100 miles but their own marketing material indicates a max detection range of 55 miles and that's from rear aspect of target under optimal atmospheric conditions. Frontal aspect max detection range is 21 miles, again under optimal conditions.


All both sides need to do is to shorten the radars ability to lockon or jam X band completely to stop the incoming Amraam missiles from going active. They just need to do this long enough to let it get close enough for IR to do it's job.
Why and how would they be trying to close on F-22s that they don't even know are there? Answer = they wouldn't. They are flying blind, while broadcasting their position to F-22s from hundreds of miles away by emitting strong RF. Massive holes in your logic, and you just keep repeating them.


Now, read my other post that explains it fully. I didn't write the explanation. Someone a lot smarter than either of us did though.
That author is am amateur blogger, do you anything about him? Do you think he's a fighter pilot or has actually worked in development of these weapon systems?


And stop digging. Or are you craving Chop Suey so much you just can't help yourself.
I have no idea what this means.
 
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I bet a A10 can fly in at 50 foot hit the target and leave without getting hit.
History disagrees, they stopped using them in contested airspace during the Gulf War after they kept getting shot down.


I'm sure hoping that this convo has stopped short of discussing classified tactical info.. That is all. I haven't read thru it all. But I'm seeing some pretty specific information being done in a public forum here.

Just sayin'....
Don't worry, there is nothing classified being presented here. The defense blogs that Darryl googles up when he can't figure things out aren't classified either.
 
But even so, at some point, the signals you are jamming will overpower the jamming signal the closer your birds get to the source. At that point, the 4th gens can be fired on first. And then the 5th gens can be fired on even closer. You may even have to use a fighter like the F-35 to do a short burst to blind a site that is stronger than the rest that has accomplished a lockon and maybe fire solution for a few minutes while it's being taken out. Not all sites will have the same range, power or capability. And neither will all Aircraft. But the EC-135 and EC-130 will be allowing the Fighters and Bombers to get a bit closer. Meanwhile, the Russians will be doing exactly the same thing with their IL birds. Then we are going to add in the Command Posts of both sides with extremely powerful radar that is just outside of launch range of the enemies attack missiles.

I'm sure hoping that this convo has stopped short of discussing classified tactical info.. That is all. I haven't read thru it all. But I'm seeing some pretty specific information being done in a public forum here.

Just sayin'....

None of this is classified. Tactics and capabilities that are known on both sides are of public record. But there is so much that we don't know and can only speculate. I, for one, will not speculate.
 
I already posted the reason that IRST is being installed on the US Fighters. And have shown that a Fighter above the Weather flying at near or above mach stands out like a sore thumb for about the same distance as it would for Radar. The F-22 super cruising at Mach 1.8 at 50K is going to be extremely hot. And the Russian IRST will be able to start picking them up at about 100 miles using their own IRST.
You posted an amateur blog by someone who has never flown a fighter aircraft. That doesn't show anything, other than you desperately googled and decided it's a "good article" because you like it's conclusions.

Still waiting for your technical analysis to back up what you said about Russian IRST sensors being superior to those used by aggressor squadron, given you thought US hasn't had them for decades I'm even more skeptical that you know anything about them. Here I'll even give you a hand, this is the IRST system used on Flankers, specs given are for the latest one:

FmP5JDW

zKRtGSU.jpg


Hilariously, you're saying 100 miles but their own marketing material indicates a max detection range of 55 miles and that's from rear aspect of target under optimal atmospheric conditions. Frontal aspect max detection range is 21 miles, again under optimal conditions.


All both sides need to do is to shorten the radars ability to lockon or jam X band completely to stop the incoming Amraam missiles from going active. They just need to do this long enough to let it get close enough for IR to do it's job.
Why and how would they be trying to close on F-22s that they don't even know are there? Answer = they wouldn't. They are flying blind, while broadcasting their position to F-22s from hundreds of miles away by emitting strong RF. Massive holes in your logic, and you just keep repeating them.


Now, read my other post that explains it fully. I didn't write the explanation. Someone a lot smarter than either of us did though.
That author is am amateur blogger, do you anything about him? Do you think he's a fighter pilot or has actually worked in development of these weapon systems?


And stop digging. Or are you craving Chop Suey so much you just can't help yourself.
I have no idea what this means.


There you go again. You are requiring the Russians to fly with the Radar On while the US flies with it's Radar off. How Monobreath of you.
 
I already posted the reason that IRST is being installed on the US Fighters. And have shown that a Fighter above the Weather flying at near or above mach stands out like a sore thumb for about the same distance as it would for Radar. The F-22 super cruising at Mach 1.8 at 50K is going to be extremely hot. And the Russian IRST will be able to start picking them up at about 100 miles using their own IRST.
You posted an amateur blog by someone who has never flown a fighter aircraft. That doesn't show anything, other than you desperately googled and decided it's a "good article" because you like it's conclusions.

Still waiting for your technical analysis to back up what you said about Russian IRST sensors being superior to those used by aggressor squadron, given you thought US hasn't had them for decades I'm even more skeptical that you know anything about them. Here I'll even give you a hand, this is the IRST system used on Flankers, specs given are for the latest one:

FmP5JDW

zKRtGSU.jpg


Hilariously, you're saying 100 miles but their own marketing material indicates a max detection range of 55 miles and that's from rear aspect of target under optimal atmospheric conditions. Frontal aspect max detection range is 21 miles, again under optimal conditions.


All both sides need to do is to shorten the radars ability to lockon or jam X band completely to stop the incoming Amraam missiles from going active. They just need to do this long enough to let it get close enough for IR to do it's job.
Why and how would they be trying to close on F-22s that they don't even know are there? Answer = they wouldn't. They are flying blind, while broadcasting their position to F-22s from hundreds of miles away by emitting strong RF. Massive holes in your logic, and you just keep repeating them.


Now, read my other post that explains it fully. I didn't write the explanation. Someone a lot smarter than either of us did though.
That author is am amateur blogger, do you anything about him? Do you think he's a fighter pilot or has actually worked in development of these weapon systems?


And stop digging. Or are you craving Chop Suey so much you just can't help yourself.
I have no idea what this means.

His information is sound. The only way you can dispute it is to try and discredit the author. That tells me that you are quite busy digging that hole.
 

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