Vympel R-27 'ALAMO' - History, Design, Performance & Discussion

The ability to maneuver in both single and multi plane is present, simply watch it being launched just as with the AIM-54. They pitch in “X” configuration upwards towards targets off the rail.

Of course having the capability to maneuver in X & + configuration as needed is a bonus, just like with HAWK, AIM-9, AIM-54, or practically any other missile. This is not such a big deal irl.

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so r27 had dual plane G values till now? damn, so that should also mean r24 should pull less g? what about magic 2 with dual plane? i swear it pulls like 50g even tho the statcard says like 35g, how much will it pull with dual plane, like 70g?

I don’t see why this would apply to the r24.
Granted I haven’t actually looked at the r24 manual but r27 is a completely new set of fins and such.

It’s actually modelled off the magic 1 maneuverability. Ik, insane. There’s a chart floating out there that corresponds g pull to speed, I bet @DirectSupport can post it in here if you want to see it. Magic 2 should actually be much more maneuverable than what it is rn which is ridiculous.
Rn magic 1 and 2 have same maneuverability.

@MythicPi what you think, think it’s worth writing up a report for this? I don’t think it’s exactly fair that the r27 gets to have its dual plane modeled when so many other missiles would benefit from it (especially the hawk/fakour 90 on the Iranian tomcats)

Pretty sure gaijin will just say something like “this proves the R-27 always operates in dual plane, so we will not change its modelling in-game” and slap it with a fat “Not a Bug”, but its worth a shot anyways imo.

Still not sure why gaijin refuses to give missiles their max dual plane maneuverability in-game tbh. Seems really silly imo, but thats just another chapter in the book of dumb that is gaijins modelling decisions.

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That’s not what was said, the case has been made that it has a 35G limit in single AND dual plane. Just like the HAWK can do 20G single AND dual plane.

The limit is lower than the potential maximum overload, so it is a structural issue limited by guidance logic.

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On a side note, the R-23 and R-24 are severely underperforming in low speed maneuverability and turn radius.