porky_kicker
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I don't want to waste my time explainingI really don't want to waste my time explaining how different are between the subsystems of air-to-air missile and cruise missile.
So let’s talk about a simple question: how to provide consistent navigation signal.
If you shoot the Brahmos NG from 300km away, the missile will fly 260km before the onboard radar starts working (the maximum distance of missile seeker detection-40km), Even if we use the speed of 3.5 Mach which is around 1200m/s, the missile will need 216.66666 seconds to cross this journey. In the meantime, the enemy AWACS or transporter will move around 38.69km distance at 643km/s cruising speed. So, it is highly likely the enemy is already outside the detecting range of the missile seeker. So, the missile will need external navigation signal to keep itself in the right direction. But the question is who should guide the missile: the fighter jet or your own AWACS. No matter who is doing this job, they will be very vulnerable within this 216 seconds. (In order to provide stable and consistent guiding signal, they can't make extreme maneuver).
So brahmos NG in air to air ( if implemented ) will solve the your navigational corrundrum the same way the Chinese solved theirs with regard to claimed 300-400 km range PL 15.
As regards to vulnerability of launch platform or awacs I guess the problem will be solved more or less the same way you Chinese will do with regard to PL 15
Capish ? Lolzzzzz