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Ракеты в DCS


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Posted
58 minutes ago, TaxDollarsAtWork said:

Then why did one of your sources say this

 

 

"

Buyers of Russian aircraft may soon be left without the R-73 melee missiles, which "catch up" with the enemy aircraft due to the infrared homing head. These missiles work on the "fire and forget" principle and remain one of the most formidable weapons of destruction of aircraft. The most recent modifications of the rocket (RMD-2) have an all-aspect multi-site seeker with a dual-band cooled photodetector, the sensitivity of which is twice as high as the basic version. These devices, which are called MK-80 "Mayak", have been produced by the Kiev plant "Arsenal" since Soviet times. "

I've seen the dual band on some sites refereed to as the "MK-80M"

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Posted
2 часа назад, TotenDead сказал:

Да, занятно, конечно, что тебя так задело, что я тебе указал на оффтоп, что ты мне 20 баллов накинул -_-

Могу еще

1 час назад, TaxDollarsAtWork сказал:

Then why did one of your sources say this

 

 

"

Покупатели российских самолетов могут в ближайшее время остаться без ракет ближнего боя Р-73, которые «догоняют» самолет противника за счет инфракрасной головки самонаведения. Эти ракеты работают по принципу «пустил и забыл» и остаются одним из самых грозных средств поражения авиатехники. Самые свежие модификации ракеты (РМД-2) имеют всеракурсную многоплощадочную головку самонаведения с двухдиапазонным охлаждаемым фотоприемником, чувствительность которого вдвое выше базовой версии. Эти устройства, которые называются МК-80 «Маяк», еще с советских времен производит киевский завод «Арсенал»."

This is a misinterpretation by journalists. MK-80 seeker has one spectrum range.

Единственный урок, который можно извлечь из истории, состоит в том, что люди не извлекают из истории никаких уроков. (С) Джордж Бернард Шоу

Posted (edited)
On 6/18/2021 at 10:39 AM, Маэстро said:

Hello, I'm not in charge of development plans.


Regarding R-27ER range... we already say that unfortunatley chart quality is not very good. There is no any chace to perfectly match this charts with any realistic drag and thrust values. Say, if we adjust missile to match chart at 5km rear hemisphere it wont match all other points! Current drag values for 27ER/ET is good compromise to be close to all chart  points at a time.

Here another one chart with new/old 27ER performance comparison. As you may see  missile achive official numbers at least at 10km altitude
 

27ER comparison.png


It still underperforms in 2/3 areas, and im not sure this even includes the energy reserve (if its not factored in, its still all 3 areas), hardly a good compromise. A good compromise would be the adjustments GGTharos suggested, it would match 1km and 5km. At 10km, i guarantee you that with battery life and the 150+ m/s energy reserve factored in, you would end up not far from the current value.

A different question, you did have this chart - why did the missile underperform in all 3 areas for this many years?

Edited by Max1mus
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When ED reworks russian missiles:
 


(April 2021 update)

Posted
7 minutes ago, Max1mus said:

It still underperforms in 2/3 areas, and im not sure this even includes the energy reserve (if its not factored in, its still all 3 areas), hardly a good compromise. A good compromise would be the adjustments GGTharos suggested, it would match 1km and 5km. At 10km, i guarantee you that with battery life and the 150+ m/s energy reserve factored in, you would end up not far from the current value.

A different question, you did have this chart - why did the missile underperform in all 3 areas for this many years?

 

 

This tuning has to do with the old FM.  The new FM should be able to better match all the ranges, but it's not so easy - the old FM simply cannot though, and IMHO it has a lot to do with the way the drag cure is represented.

Old FM is not possible to match anything but one of the ranges, all others will be off.  Matching 1km should bring yo close to the 5km but you cannot tune 1km AND 5km (or 10km).  You can only tune one of them.

 

It has been requested a long time ago to tune for the low altitude with old FM, ED never did this.  They may or may not now, and either way only the new FM can bring a clearer view and resolution to this problem as a whole.

 

You can basically ignore/forget the 150m/s and 2-3g stuff when it comes to this.  You cannot simultaneously tune all of this in the old FM - you can try and maybe get close, but it just doesn't contain enough information for this.

If you look at the new FM, it's basically simulating 10x the variables just for the FM, along with new systems like the autopilot and actuator controls etc.

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Posted
12 minutes ago, GGTharos said:

You can basically ignore/forget the 150m/s and 2-3g stuff when it comes to this.


Why? It literally proves that "possible launch" means the missile must be able to overshoot the target with a significant amount of extra energy.

When ED reworks russian missiles:
 


(April 2021 update)

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Posted
25 минут назад, Max1mus сказал:

A different question, you did have this chart - why did the missile underperform in all 3 areas for this many years?

 

Because we did not take into account the speed required to proximity fuse work, 150 m/s. 

Единственный урок, который можно извлечь из истории, состоит в том, что люди не извлекают из истории никаких уроков. (С) Джордж Бернард Шоу

Posted
1 minute ago, Chizh said:

Because we did not take into account the speed required to proximity fuse work, 150 m/s. 


Do the markings posted by Maestro respect that required speed, or is that just pure kinematic ability?

When ED reworks russian missiles:
 


(April 2021 update)

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Posted
1 минуту назад, Max1mus сказал:


Why? It literally proves that "possible launch" means the missile must be able to overshoot the target with a significant amount of extra energy.

R-27 can do it now. It has a good amount of energy on the target.

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Единственный урок, который можно извлечь из истории, состоит в том, что люди не извлекают из истории никаких уроков. (С) Джордж Бернард Шоу

Posted (edited)
12 minutes ago, Chizh said:

R-27 can do it now. It has a good amount of energy on the target.

marks.png

What i am asking about is these markings. They compare the old and new missile capabilities. Is that kinematic ability MINUS >150 m/s or ability to destroy the target in DCS?

PS: No, it cannot. Ive given you tracks showing the missile fall behind the target well within the declared range. I dont know what else to say.

Edited by Max1mus

When ED reworks russian missiles:
 


(April 2021 update)

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Posted

OK, I'll see it in a week when I return from vacation to Moscow.

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Единственный урок, который можно извлечь из истории, состоит в том, что люди не извлекают из истории никаких уроков. (С) Джордж Бернард Шоу

Posted (edited)
On 5/12/2021 at 7:26 PM, Chizh said:

Еще раз. И для GG тоже.

у старых AIM-9 было очень заметное ограничение на угол целеуказания. Даже у ракет 9L/M этот угол составляет +-28 градусов, против 45 градусов поворота координатора на сопровождении.

ТТХ ракет ВВ НАТО из Т-О МиГ-29.jpg


In DCS, the AIM-7M has significantly less range than the R-530D, especially at the 0.5km mark. And the DCS gap between a non-lofted AIM-120B(A) and the AIM-7 is also bigger than described in this document.

Edited by Max1mus

When ED reworks russian missiles:
 


(April 2021 update)

Posted
1 minute ago, Max1mus said:

non-lofted AIM-120B(A)

Just a note, but as far as I can tell the whole AIM-120A cant loft thing appears to be a myth. I was under that impression as well, but after doing some digging, I simply cant find any sources supporting this claim. For example, weapons manuals for the F-16 mention the loft steering cues without making any distinction between the 120A and B, same with the F-18 weapons manual.

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Posted
2 hours ago, dundun92 said:

Just a note, but as far as I can tell the whole AIM-120A cant loft thing appears to be a myth. I was under that impression as well, but after doing some digging, I simply cant find any sources supporting this claim. For example, weapons manuals for the F-16 mention the loft steering cues without making any distinction between the 120A and B, same with the F-18 weapons manual.

The early 90's F15 weapons manual also makes mention of lofted steering cues for the amraam.

Posted (edited)

Then the russians were either horribly wrong with their estimations on lofting missiles, or something is up with non-draggy missiles at very high altitudes in DCS. But the range relationship in that document between 530, 7M and 120 is not represented in DCS. The difference between 7M and 530 is even reversed.

The fact that the AIM-9M outspeeds and outranges the AIM-7MH at altitudes like 40.000ft adds more questions.


@Jack1nthecrack Check Maestros post from a few pages ago (last page?) He did the testing and marked the points on the chart. I couldnt find the original posts so i will just re-post them:

ER_falls_behind (1).trk - 1000m in ZPS, around 9.6km (less than on the graph). Missile even falls behind.
I skipped 5000m, but the differences there are also extreme
10.000m_not_enough_energy_fast.trk - 10000m. Missile hits, but with not enough energy reserve, and the launch distance also seems to be a bit within the chart range.
10.000m_battery_life.trk -  10000m This one shows how close the ER is to running out of battery life up there (i shot slightly further here and it already ran out). A bit less drag - and it would not be limited by energy, but by electronics (it might barely already be). This could very well explain the smaller gap between fast and slow speed at high altitude, which from what i understood, is the reason why some in ED do not believe the graphs.

Edited by Max1mus
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When ED reworks russian missiles:
 


(April 2021 update)

Posted (edited)
36 minutes ago, Max1mus said:

The fact that the AIM-9M outspeeds and outranges the AIM-7MH at altitudes like 40.000ft adds more questions.

 

It's really not that surprising.  The sidewinder's rocket motor is all-boost and at a higher acceleration than even the AIM-7s own boost stage. 

As a projectile, the AIM-9M has the ability to gain a lot of speed (well over M3) and is limited by available power.

 

At high altitude the AIM-7's sustain stage plays a role, but not quite as large ... think of it this way.

10g for ~ 3.5 sec + 2g for ~ 11 sec

vs

14g for ~5sec.

 

The sustain motor won't get you quite to the same peak as a boost motor for the simple reason that it's going to get a bigger acceleration fraction eaten up by air resistance.  You would certainly get the lines to cross on a graph at some point, but not with these two missiles at high altitude.

Edited by GGTharos

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Posted

We have flyout graphs for the AIM-9.   No amount of mentioning 'wobbly movements' or anything else like that makes any sense.  Compare to those graphs and see if its different.

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Posted

Just a quick comment @tavarish palkovnik, I'm reasonably certain that you're good up to 17 degrees of AoA for mid-body wing controlled missiles of this era 🙂

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Posted

All right, Cy function to get down a bit and to have Cn with 17 deg at time when needed.

Fact is that obtaining of horizontal flight is with reasonable angles much under 12 or 17 so increased or reduced Cy will not affect a lot induced Delta Cx and by that velocity in function of time.

Posted (edited)

And by the way, rocket having such wings near to the center of gravity usually and by purpose doesn’t do high angle of attack compared to others. I doubt is it even 10 in this particular case.

Edited by tavarish palkovnik
Posted

I agree with you, just stating some numbers I have read about other similar missiles.

 

For canard controlled missiles you get higher AoA available, and even more for tail-controlled.  I doubt that in any case they can exceed 30 (although the R-77 is rumored to be controllable at 150 which is weird)

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Reminder: SAM = Speed Bump :D

I used to play flight sims like you, but then I took a slammer to the knee - Yoda

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