T
Turko
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Hell no again we will be deprived quad packed G40.If Hisar-O RF only has 35km range and they intend to replace 'ESSM with it on the Istif-Class the dicussion need to be had why G40 was not greenlit in 2019.
Hell no again we will be deprived quad packed G40.If Hisar-O RF only has 35km range and they intend to replace 'ESSM with it on the Istif-Class the dicussion need to be had why G40 was not greenlit in 2019.
ATMACA doesn't fly supersonic which overheats IR seeker. The problem with IIR SAM is overheating burns sensors because supersonic speed.So from what you are saying can I deduce that the physically, the missile can reach longer ranges but due to it’s seeker head’s inadequacies, as it can’t see efficiently further than 25 km, and hence it has a shorter range?
For IR this is the case. Isn’t that it is why Imaging Infra Red seekers are used so that the target lock is secured with the image and flares don’t mean much?
Atmaca block 2 will use multi mode seeker ; RF and IIR seeker head. Why not use the same for Hisar, if this is the limiting factor?
It's one of the limitations. But rocket motor is more important. İssues with IIR at long ranges can be solved with datalink.So from what you are saying can I deduce that the physically, the missile can reach longer ranges but due to it’s seeker head’s inadequacies, as it can’t see efficiently further than 25 km, and hence it has a shorter range?
As range increases, dedicated pixel number for target decrease. It's like trying to digitaly zoom into a photo which taken long ranges from object. In lower pixels, a flare and aircraft will share the same size. At one point, both aircraft and flare will be in same pixel.For IR this is the case. Isn’t that it is why Imaging Infra Red seekers are used so that the target lock is secured with the image and flares don’t mean much?
Atmaca block 2 will use multi mode seeker ; RF and IIR seeker head. Why not use the same for Hisar, if this is the limiting factor?
I am sorry but, even a high-school student knows that aerodynamic structure and drag coefficient of a circular head is much lower than a conical one.It is the other way around. The pointed nosecone of a radar seeker has much less drag than the rounded seeker of an IIR missile. See the following link for example. Addition of a pointed nosecone to the Umkhonto ER is expected to increase its range by upto 10 km:
Mica NG missile uses IR and RF combined seeker head? Chinese are doing it with their a2a missiles?ATMACA doesn't fly supersonic which overheats IR seeker. The problem with IIR SAM is overheating burns sensors because supersonic speed.
No idea. Although David's Sling also has dual seeker, AFAIK Imaging IR seekers can't resist long time supersonic speed.Mica NG missile uses IR and RF combined seeker head? Chinese are doing it with their a2a missiles?
Isn’t that why the use detachable cone heads?No idea. Although David's Sling also has dual seeker, AFAIK Imaging IR seekers can't resist long time supersonic speed.
To be honest no clue but it sounds suspicious because detachable cone will effect on minumum range. Anyway HisarA+ great achievementIsn’t that why the use detachable cone heads?
Did we ever build a Hisar O variant that has different properties than the O+ variant ?
No, Mica uses a changeable seeker. You can use only RF or only IIR at the same time.Mica NG missile uses IR and RF combined seeker head? Chinese are doing it with their a2a missiles?
Which seems to confirm that no Hisar-O was previously built. The Hisar-O+ we are talking about is the only variant to be built and SSB calls it Hisar-O.
MSB calls it Hisar O
You are correct. It is one or other.No, Mica uses a changeable seeker. You can use only RF or only IIR at the same time.
I am sorry but, even a high-school student knows that aerodynamic structure and drag coefficient of a circular head is much lower than a conical one.
View attachment 25457
Below shape is the most aerodynamic shape there is. That is why all air and sea vehicles are optimised to approximate this shape.
The reason in your shared article , they have used detachable heads, is to protect the seeker head from heat due to air friction. By designing a more aerodynamic detachable head than it had previously they were probably able to increase range, which otherwise would have been 10 km shorter.
If lift is not required an aerofoil is the most aerodynamic shape and has the lowest drag coefficient.
View attachment 25458
Physics laws do not change because an article misinterpreted the speed gain with a newly designed cone head.
Just check out the drag coefficient values of various shapes below: The lowest is the aerofoil. That would give you the highest speed through fluids and air.
View attachment 25460
According to @TheInsider RF has a range of 35-40km!!
Do we have a definitive source for the range figure for the RF missile?
Also why RF has a longer range than IIR? Does the nose structure of a missile make such a big difference? If it does can someone explain how? Since a circular ball head has better aerodynamic properties and drag coefficient than a cone shaped head of same diameter, I would like to know what gives this extra range.
İ didn't get it.What should we understand according to picture? Maximum range Hisar O+ is 25km or 50km?
Hisar A+ & Hisar O+ class missiles are 4+ Mach speed missiles. So they should, in theory, be able to stop supersonic missiles as well as supersonic planes. The test pictures we see are with ”Simsek” . It is a subsonic turbojet propelled UAV/plane. Doesn’t any body here think that it should also be tested against supersonic missiles and planes.
RF 35-40 km
So Hisar O RF could reach 35-40 km range.
Can you elaborate please? Are you suggesting that drag coefficient changes with speed?High speed vs low -speed. It is different.
Banshee seems to be slower than Simsek target plane. (Half the speed of Simsek) . Which supersonic target is tested?View attachment 25471
View attachment 25472
Banshee with hot nose is used for IR missile testing. Simsek did also getting updated with hot nose etc.
It does get tested against supersonic threats. Also TAI recently developed supersonic target drone. Even if they were to release footage, it wouldn't be something with detail obviously. It would probably be low res footage, with supersonic missile flying straight. Two dots.