The AIM-120 'AMRAAM' - History, Design, Performance & Discussion

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Regarding your statements about my “napkin math” and the AIM-120’s thrust profile, the sustainer is essential to reach higher speeds and then maintain them for whatever time it can. At lower altitudes the booster will not be reaching mach 4 as the R-77s can. This is reflected in the relevant charts.

So no, this doesn’t contradict my earlier “assumptions”. The boost-sustain profile does allow for you to sustain the speeds of the initial boost, but at a certain point drag is much reduced and the sustainer can actually allow for higher top speeds. For the AIM-120 it seems that the top speed of mach 4 is only achievable in the same manner as the R-27ER’s top speed is only achievable. (At very high altitude and initial launch speeds). The R-77 is still the winner here, having a similar thrust profile to the AIM-120C-5 and lower drag grid fins for such high supersonic speeds.

Yes, you’re correct the R-77 is more similar to the AIM-7M in size but with much reduced electronics size, different warhead, tail guidance section instead of wings. It has more modern higher ISP propellant and a better burn profile. Now let me remind you that the AIM-7M has 100km range.

The R-77 is far from the second coming of Jesus, I think that could be quite an offensive statement to some… The R-77 is not better at lower altitudes where the aircraft would be unable to launch above mach 1.3 because wave drag could significantly impact the performance of the missile immediately. This is evident by the fact that it has some 33% less range than R-27ER at 1km altitude seemingly. The AIM-120A wouldn’t be any better, but as altitude increases the R-77’s advantages stack on.

You’ve read my assessments wrong, I think the AIM-120A in a 1v1 BVR situation would not be the breadwinner for engaging an aircraft equipped with the R-27ER. The R-27ER can out-range the AIM-120A and still give the launcher time to evade the AMRAAM. That is all. The fact that you can go full cold and turn around to launch another AMRAAM as the target gets closer kind of nullifies the advantages of the R-27ER. I think it’s a fair match-up and we should see the AIM-120A soon. In fact, I’d advocate for letting the AIM-120A come to the game and give Russia no fox-3 at all until a few updates (6-9 months) later.

Yes the export company overclaims the range of their missile. In no real world situation will it ever hit any target at 75km. No modern airforce is that idiotic that they’d allow such a thing to happen. The missile would be wasted with little to no remaining energy. Unlike the R-77 which seemingly has plenty of energy at the altitudes where it can hit 100km but fails to due to battery life.

They abandoned the R-27ER. It’s still used in training, but when you have massive stocks of things you tend to continue using them as necessary. There was a Harrier equipped with an AIM-120A/B in 2022. I seriously doubt them engaging anything in Syria requires the advantages of the R-77. Using the cheaper old missile stock would be wise.

Lattice fins are well studied, what I’ve claimed is true. The fact that they’d moved to conventional tailfins likely suggests that the missile wants better drag near the end of a lofting trajectory and supports the theory that earlier R-77s did not loft, whereas the newer models likely use such trajectory shaping. For a missile that looks at almost doubling the range of the original R-77 and in a similar sized package… this would be more ideal to move to conventional fins. Grid-fins would be better suited for what I’d call the “brute force missile” designs of Soviet era Russia such as the R-27ER or early R-77.

Also,
If they were to think the legacy style tailfins were better than the grid-fins they’d likely also replace the export models grid fins but they didn’t. They didn’t replace the grid-fins on the ramjet proposal model either.

You could have asked for the book but you didn’t. Instead you just used the fact that I failed to properly cite it as ammo to attack me for whatever reason because… behold… my napkin math was right. The R-77 is a 100km range missile by all means.

TL;DR
The R-77 is a 100km range missile, bar the export RVV-AE which we still do not have solid data to go off of imo. The grid fins are advantageous for a missile that lacks a lofting trajectory and no public knowledge really suggests it has any kind of loft. It looks like Russia was looking more for time to target than peak range. The new R-77M has traditional fins as it is a similar sized missile looking to reach nearly double the range of the original R-77. This requires lofting, and the older style fins do not suffer wave drag between 0.8 and 1.3 mach. At final approach at such ranges the missile can be expected to drop to those speeds and they don’t want it falling out of the air.

It’s not official Vympel’s catalogue. It’s “Bastion” magazine from 2001.

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And this chart originally is from this book from 1993.

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This is the second time @MiG-23M lied or about a source’s provenance and it seems completely pointless to continue arguing with someone when they’ve demonstrated that they’re not debating in good faith.

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You know very well what you did. Handing these sources off to me as legitimate and then turning around to paint me as guilty like this.

This also doesn’t change the fact that all of the graphs in the second book match the real primary source manual diagrams and charts for range on the remaining missiles. It’s highly likely that the R-77’s is accurate as well.

@Aetreus The argument stemmed from the fact that the R-77 outperforms the early AMRAAM’s, AIM-120A/B. I made the point that the first AIM-120 that would properly compete is the AIM-120C-5. This has not changed, and whether the R-77s max range is 80 or 100km doesn’t change that fact either. That will only really determine if the AIM-120C-5 will compete with, or beat it outright.

And @MythicPi if you still want to try and prove the AIM-120A/B is comparable to the R-77 I’d be happy to see you use napkin math or the same methods and reason as I have used to find the range of the missile. If you want to stick to your guns and not be a hypocrite about this you can go ahead and find any reasonable source to suggest the AIM-120A has more range than the AIM-7F/M barring guidance time and lofting.

Yeah no point in arguing anymore, I’ve just muted him.

Back on topic for the AIM-120, ill dig around and see if theres anything more I can find besides the source I already posted. Since it came from a mod, Gaijins already got eyeballs on that one, and beyond the fact that it indicates the AIM-120A matches the AIM-7M range and exceeds its envelope to the sides with conventional guidance, and exceeds its range with command inertial guidance, it doesnt give us any hard numbers beyond “better than AIM-7M”.

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Pointless muting someone who runs the thread and has more knowledge / information on the topic. I’ve already passed most public sources to the mods on the topic. In fact, they approached me for further information in the first place.

When you discover what I’ve said is true don’t be afraid to post it and admit as much.

I’m not painting anybody here. I only discuss misisles here and free to constructive dialogue. What’s wrong with showing that source you posted isn’t official and quite old, possibly outdated and perhaps not converging with reality?

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You had these sources, you knew that the RVV-AE is the export model yet failed to provide the information and when you did share it with others it was misrepresented. When someone posts it as it was shown to them you only take the time to correct them after it was posted here?

Yes let’s remain constructive and instead of attacking “napkin math” we can continue to make inferences on the performance of missiles without relying on arbitrary and inaccurate statements from the governments who produce them. The AIM-120 is clearly >20 miles maximum launch range, just the same as the R-77 is clearly capable of more than 80km. It would be considered dishonest imo to state that 80km is even the effective range of either weapon anyhow.

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I’m working on a working AIM-120A/B model in war thunder using the public data.
I don’t have real thrust figures, but using the burn times discovered and ISP of the HTPB propellants I’ve found a thrust that correlates. Adjusting the drag model to be between two missiles larger and smaller than the size of the AIM-120 has yielded the following results, and I’ll compare against R-27ER.

Co-altitude 10,500m target and launch aircraft.
Both locked at 1,200 km/h. Launch at 60km.

AIM-120A hits in 79s.

R-27ER hits in 52s.

This leaves approximately 27 seconds for the R-27ER launching aircraft to defend in this particular scenario. Honestly, I think the AIM-120A could come to the game very soon and it would be matched against the Russian aircraft equipped with R-27ER. (Albeit some AMRAAM slinging aircraft simply have more missiles).

Also take my testbed model of the AIM-120 with a huge pinch of salt. I’m working on estimates here, although at least well founded ones. The ISP, thrust etc could be way off since I’m guesstimating the thrust based on known propellant weight and burn time.

Note;
I tested the missile with an infeasibly low drag coefficient as well
(same CxK as AIM-7F albeit much smaller “caliber”)
Time to target dropped to ~69 seconds. This is still 17 seconds later than the R-27ER for a 60km launch in these conditions.

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Testing again, I found that the R-77 beats the AIM-120A/B test model to target as well. The time to target is approximately ~65s to the AIM-120’s best case scenario of 69s (and more realistic time to target of 79s).

Excuse the AIM-120C model, looking for an R-77 model to insert currently but wanted to share the results sooner.

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I found a source which states more clearly the fact that the AIM-120 uses instability to improve energy conservation and range as well as maneuverability.

Particular section;
In Russian
In English

https://www.gosniias.ru/index-e.htm#5

This is a “source” the same way “it came to me in a dream” is a source. A Russian state funded research institute commenting on a western missile is about as reliable as that Indian defense blog from a few days ago

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I did not include in in the OP of the thread for a reason, rather just shared something public that states something interesting about the missile. They also cited a number of sources for their information at the bottom of the page.

Its also just an erroneous understanding of what his source states, seeing as it specifies “the feature is a method of minimizing energy consumption by the drive” and speeks of the hinge moment.

This is literally just talking about how the missile minimizes how much effort the fins actuators (or drives) must work…

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This makes sense, I’m looking for more information on the “high-angle off-boresight capability” of the AIM-120C variants stated in various sources.

AIM-120C-7 initially seems to use the +5 motor from the AIM-120C-5, but later replaces the “SCAS” (shortened control actuator section) with “VCAS” (value control actuator section) and also received a replacement rocket motor from the firm “NAMMO”.

From what i understand , the C7 initial upgrade was new software to improve the resolution and interference immunity of the WGSN.
Later from lot27+ the use of a more modern oand compact element base (VCAS?) made it possible to increase the length of the engine bay and so more propelant = more range (120km vs 105km Max range)
The NAMMO remplacement motor was only a motor that could be use in cold temperature (ie Norway) because the initial one wasn’t working well for higth altitude cold air shot. I don’t think the motor was better in way than the atk one in performance.

NAMMO motor seems to have been offered at some point but only to those with VCAS modification which is why I presume it has higher performance similar to the lot27+ motors made by Orbital ATK but could be wrong. I also see no reason NAMMO couldn’t have helped produce both motors as well.

This has been a very interesting thread to read

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It is there and I did testing of it with a friend immediately after release, it works on F-14A Early at least with at least 2 missiles.