Forest Green
ACCESS: Above Top Secret
- Joined
- 11 June 2019
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My thinking was a little bit of "operational experience" and a little bit of "precision weapon available"Why is it ominous? Because it is overkill for the air-defences available to opponents? IMHO, NATO isn't immune to using low threat combat environments to gain operational experience with new weapon types, nor is NATO immune to using up outdated weapon stocks against unsuitable targets. So, either explanation would work.
The Kh-55 is also one of the few precision weapons readily available.
There's quite a bit of volume taken up by an inlet duct. especially if you want stealth ducting. Call it engine diameter and length, if not twice that much volume.Circling back to the original design as discussed a page ago - what is the advantage of having the entire engine extend downward in a separate pod vice having a ventral air intake and leaving it internalized? I assume it's easier/cheaper to pod mount the entire outside the airframe in fixed design, and a lot of Iranian missiles seem to use that geometery (US UTAP-22 UAV is another example). But once you go to the trouble of internalizing the engine and using up the missile body's volume anyway, why not duck the intake to the engine rather than move the engine out of the missile? I'm sure there's some additional loss of volume for having an air duct, but compared to having the moving parts of shifting the engine outside the airframe, isn't worth just keeping it internal?
Chaff launchers?These are not infrared traps, but anti-radar ones