shehbazi2001
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While this topic is complex and lengthy, I have just tried to present some basics only. Purpose is just to initiate a healthy discussion on the topic and learn from one another.
Using easy examples, there are two types of heat-seeking missiles. One that "smell" or "feel" the aircraft and others that "see" an aircraft. The former are ordinary IR seeker missiles and latter are Imaging Infra Red seeker missiles.
Imaging IR seekers are those that actually "see" the thermal image of the aircraft. For early heat-seekers, aircraft was a dot in the sky. The Imaging Infra Red seekers are identified by their transparent glass domes at the nose. AIM-9X, ASRAAM, IRIS-T, MICA-IR all have transparent glass seekers.
The ideal seeker would be a dual-band Imaging Infra-Red seeker. It needs to be verified, but MICA seems to be doing it.
The seeker of FIM-92B Stinger MANPADS (Man Portable Air Defence System) used a dual-band seeker using both Infra-Red and Ultra-Violet bands, almost 30 years ago. FIM-92C was a reprogrammable microprocessor equipped (software) Stinger.
As the flares are mostly in Infra-Red spectrum, they are useless against a seeker who also seeks ultra-violet radiation. Block-II Advanced Stinger uses an Imaging Infra-red seeker.
Almost all the Imaging IR seekers use image-processing techniques and thus microprocessors and thus software for it. Getting this software is extremely important. As the imaging seeker sees the whole aircraft, it can be programed to hit the hottest engine part or less hotter fuselage, according to the tactics developed by the air force.
All missiles have impact fuses and now its important to see what other fuses are installed. For air to air, the proximity fuse is most important after the impact fuse because either the missile shall hit the target or it shall miss it by a small margin. Therefore its necessary to initiate the warhead on hitting the target and when its nearly missing the target. Fuse is the thing that explodes the warhead.
AIM-9L Lima has laser-proximity fuse, which is jam resistant. ASRAAM also uses laser proximity fuse, which is plus point. MICA uses RF (radio frequency) proximity fuse, which "seems" a disadvantage to me. However, PAF can demand to install a laser-proximity fuse from the manufacturer as it should not be difficult.
Lock-On After Launch (LOAL) is important for those fighters that carry missiles internally like F-22 or F-35. The seeker of missile is not out in the air to feel the heat or IR radiation. LOAL is useful also for submarines carrying such missiles.
Also LOAL is required for backward firing of missiles ie firing it straight and then the missile turns 180 degree to the rear and achieves a lock upon seeing the target. I dont know if PAF is interested in LOAL capability.
Warhead of MICA seems to be the most advanced one, using "Focused Splinters". When an ordinary warhead explodes, it distributes its explosive energy (destructive power or blast power) equally in all directions. This is not desired. We want the explosive energy to be directed towards the target.
MICA's warhead seems to be doing it. If MICA misses the target by a little margin to the right side, the proximity fuse shall initiate the warhead and warhead shall explode, sending its splinters towards the aircraft (left side of the missile). This is directed-energy warhead technology. I think this was first used in anti-tank missiles, with top-attack anti-armour warheads. The warhead concentrates most of its energy in direct downward direction to damage the tank or other armoured vehicle to the maximum, without diving on it.
Thrust-Vector Control (TVC) is another feature of the new missiles. ASRAAM, Python-4 and Python-5 are not using TVC. Pythons use complex aerodynamic controls for achieving good turn rates but ASRAAM is neither using complex aerodynamic surfaces nor TVC, casting doubts on its maneuverability (turning performance). MICA, IRIS-T, R-73 use TVC.
IRIS-T is said to pull 60g and MICA 50g and Python-4 is siad to pull 70g. But I
think that the measure of turning performance (both aircraft and missiles) is not so simple. Its not just pulling so much gs. Minimum turn radius is also not sufficient.
Important thing is time, tightest turn in shortest time is what we need to look. If an aircraft or missile makes a more tight turn but takes longer than his opponent, who pulls a less tight turn more quickly, then there is no use of this tightest turn. Tighest and fastest turn is what is required. Thats why we talk of corner speed, the speed at which turning performance is maximum.
Now comes the solid rocket motor. In early missiles, the rocket motor burn times were short and the missile would fly unpowered towards its target at max range and become energy-less, easy to dodge. Now the energy of rocket-motor is better managed to give it more energy at "end game". This is achieved through dual-thrust rocket motors, meaning that thrust of rocket is not the same during the flight, the thrust is increased slowly as the missile nears the target and then drops off.
AIM-9B followed 1 micron radiation, which is the hottest zone of an aircraft. AIM-9L follows 4 micron radiation, which is not the hottest region of aircraft and is more the fuselage. The more hot an object, the smaller would be the radiation wavelength. The smaller the wavelength, the higher the frequency.
wavelengths of typical flares????? if the wavelengths of the current flares are near 4 microns.....they can possibly fool the incoming Lima.... Therefore the flare systems used by PAF aircraft must be tailored according to the seekers of the Indian or other threatening force's heat-seeking missiles. We also need to see what Mr Mike (AIM-9M) is upto, if PAF is getting it.
Still many things remain like arming of the warhead, navigation techniques used, ranges, minimum launch speed restrictions (all heat-seeking missiles cant be fired from helicopters because of minimum launch speed restrictions), further filters for ECCM, maximum speed and its effect, inter-operatability with Sidewinder rails, seeker cooling systems, range of Proximity Fuse and its effect??? etc etc.
Further discussion can be continued in the thread.
Using easy examples, there are two types of heat-seeking missiles. One that "smell" or "feel" the aircraft and others that "see" an aircraft. The former are ordinary IR seeker missiles and latter are Imaging Infra Red seeker missiles.
Imaging IR seekers are those that actually "see" the thermal image of the aircraft. For early heat-seekers, aircraft was a dot in the sky. The Imaging Infra Red seekers are identified by their transparent glass domes at the nose. AIM-9X, ASRAAM, IRIS-T, MICA-IR all have transparent glass seekers.
The ideal seeker would be a dual-band Imaging Infra-Red seeker. It needs to be verified, but MICA seems to be doing it.
The seeker of FIM-92B Stinger MANPADS (Man Portable Air Defence System) used a dual-band seeker using both Infra-Red and Ultra-Violet bands, almost 30 years ago. FIM-92C was a reprogrammable microprocessor equipped (software) Stinger.
As the flares are mostly in Infra-Red spectrum, they are useless against a seeker who also seeks ultra-violet radiation. Block-II Advanced Stinger uses an Imaging Infra-red seeker.
Almost all the Imaging IR seekers use image-processing techniques and thus microprocessors and thus software for it. Getting this software is extremely important. As the imaging seeker sees the whole aircraft, it can be programed to hit the hottest engine part or less hotter fuselage, according to the tactics developed by the air force.
All missiles have impact fuses and now its important to see what other fuses are installed. For air to air, the proximity fuse is most important after the impact fuse because either the missile shall hit the target or it shall miss it by a small margin. Therefore its necessary to initiate the warhead on hitting the target and when its nearly missing the target. Fuse is the thing that explodes the warhead.
AIM-9L Lima has laser-proximity fuse, which is jam resistant. ASRAAM also uses laser proximity fuse, which is plus point. MICA uses RF (radio frequency) proximity fuse, which "seems" a disadvantage to me. However, PAF can demand to install a laser-proximity fuse from the manufacturer as it should not be difficult.
Lock-On After Launch (LOAL) is important for those fighters that carry missiles internally like F-22 or F-35. The seeker of missile is not out in the air to feel the heat or IR radiation. LOAL is useful also for submarines carrying such missiles.
Also LOAL is required for backward firing of missiles ie firing it straight and then the missile turns 180 degree to the rear and achieves a lock upon seeing the target. I dont know if PAF is interested in LOAL capability.
Warhead of MICA seems to be the most advanced one, using "Focused Splinters". When an ordinary warhead explodes, it distributes its explosive energy (destructive power or blast power) equally in all directions. This is not desired. We want the explosive energy to be directed towards the target.
MICA's warhead seems to be doing it. If MICA misses the target by a little margin to the right side, the proximity fuse shall initiate the warhead and warhead shall explode, sending its splinters towards the aircraft (left side of the missile). This is directed-energy warhead technology. I think this was first used in anti-tank missiles, with top-attack anti-armour warheads. The warhead concentrates most of its energy in direct downward direction to damage the tank or other armoured vehicle to the maximum, without diving on it.
Thrust-Vector Control (TVC) is another feature of the new missiles. ASRAAM, Python-4 and Python-5 are not using TVC. Pythons use complex aerodynamic controls for achieving good turn rates but ASRAAM is neither using complex aerodynamic surfaces nor TVC, casting doubts on its maneuverability (turning performance). MICA, IRIS-T, R-73 use TVC.
IRIS-T is said to pull 60g and MICA 50g and Python-4 is siad to pull 70g. But I
think that the measure of turning performance (both aircraft and missiles) is not so simple. Its not just pulling so much gs. Minimum turn radius is also not sufficient.
Important thing is time, tightest turn in shortest time is what we need to look. If an aircraft or missile makes a more tight turn but takes longer than his opponent, who pulls a less tight turn more quickly, then there is no use of this tightest turn. Tighest and fastest turn is what is required. Thats why we talk of corner speed, the speed at which turning performance is maximum.
Now comes the solid rocket motor. In early missiles, the rocket motor burn times were short and the missile would fly unpowered towards its target at max range and become energy-less, easy to dodge. Now the energy of rocket-motor is better managed to give it more energy at "end game". This is achieved through dual-thrust rocket motors, meaning that thrust of rocket is not the same during the flight, the thrust is increased slowly as the missile nears the target and then drops off.
AIM-9B followed 1 micron radiation, which is the hottest zone of an aircraft. AIM-9L follows 4 micron radiation, which is not the hottest region of aircraft and is more the fuselage. The more hot an object, the smaller would be the radiation wavelength. The smaller the wavelength, the higher the frequency.
wavelengths of typical flares????? if the wavelengths of the current flares are near 4 microns.....they can possibly fool the incoming Lima.... Therefore the flare systems used by PAF aircraft must be tailored according to the seekers of the Indian or other threatening force's heat-seeking missiles. We also need to see what Mr Mike (AIM-9M) is upto, if PAF is getting it.
Still many things remain like arming of the warhead, navigation techniques used, ranges, minimum launch speed restrictions (all heat-seeking missiles cant be fired from helicopters because of minimum launch speed restrictions), further filters for ECCM, maximum speed and its effect, inter-operatability with Sidewinder rails, seeker cooling systems, range of Proximity Fuse and its effect??? etc etc.
Further discussion can be continued in the thread.