Avimimus
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That's right. It's not a very interesting consideration in air combat though as aircraft are fairly soft targets. The US ballistics tests I quoted above show the percentage of vulnerable area of the target aircraft in the test to the different weapons, and explosive shell capable of damaging the aircraft structure have a clear advantage here, so I'd say optimizing for penetration would not be a good strategy.
Thanks for the detailed reply.
A couple of additional observations:
- Passing through aircraft skin induces yaw in bullets, which tends to reduce penetration by two or three millimetres. When one considers armoured seats, components, and fuel tanks may protect key components (pilot, engines) when fired on from the rear, and the strength of structural elements like spars... differences in penetration can actually have a significant effect. Of course this is most significant for the smallest calibre weapons (but does make them less effective overall compared to heavier weapons).
- Filling weight (for incendiary or explosive mixtures) differs significantly within the heavy machinegun range. So the difference between an Browning's M1 and an M23 means that the post-war round will have significantly better terminal effects. The same goes for the UB/UBS/UBT and MG-131 - both of which benefitted from considerably larger fillings. I think this impacts these medium calibre weapons the most (as they are the ones which have round volumes which are just beginning to carry meaningful bursting charges, but also vary the most in the ratio of steel to filling - as any amount of filling is relatively marginal and slight thicker walls can render the filling trivial).
So there is an argument for slightly reducing the firepower of rifle calibre weapons, and incorporating more variation in the firepower of heavy machine guns.
I suppose one would do the latter (adjust for filling weight) through using a non-linear equation that treats variation in filling as being relatively significant on the low end, but the differences being less significant in the high end (perhaps ignoring the effects of shrapnel and apply a square/cube function to treat the rounds as purely blast/volume based)?
You're right againIt's fairly complicated though, as the influence depends on further factors such as (already pointed out by you) the velocity of the shooting platform as well as of the targeted platform, as well as the flight altitude. I ran the numbers for a selection of weapons for which I had the data, and it turned out that the higher-velocity, machine-gun type weapons mostly relying on kinetic energy for effect lost power downrange quicker than the lower-velocity cannon, as the chemical energy of the shell contents remained unaffected.
So, it's sort of conservative to use muzzle energy in as far as not to underestimate the smaller calibres.
Regards,
Henning (HoHun)
This might be a reason why the transition to lower velocity higher volume rounds was common in the post-WWII era (e.g. NS-23/NR-23, N-37 are both favouring lower velocity but heavier rounds). Similarly, the abandonment of the 0.60.
There is also the probabilistic factor - how conservative are pilots in pulling the trigger, how long a burst can they fire, what area is covered by that burst. Looking at the Bf-110 in its primary characteristics (airspeed, firepower per second, turn time) it should have been competitive - it is only when one considers that it was a larger target (with a lower roll rate perhaps) that we see why it failed. So, I think the full picture involves the probability of hitting a target multiple times with an average skill pilot in a typical combat situation - and that might give a bit of an edge back to heavy machine guns or lighter cannons (higher combined rate of fire, higher muzzle velocity). That is very difficult to include in a calculation though! Will reply to the Col. Coats discussion later.