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Hi, I understand that the Meteor missile is a ducted rocket, but doesn't that mean during a turn, the air intake would be seriously limited, thus making the rocket less effective, and therefore less maneuverable?
1. Looking at the Meteor's layout, it looks like the ducts are configured so that at least one intake will always have clear airflow
2. Keep in mind that the Meteor will be traveling at very high speeds, so the sheer act of moving forward in the air, even in a turn, should be enough to force air into the intake.
Also, a missile isn't going to be moving at "near zero" speeds. It has to keep its forward inertia and kinetic energy, otherwise it simply falls out of the sky. Unlike an airplane, a missile doesn't generate lift.
4. The Meteor's flight profile is boost and coast, but even when coasting, it will be moving at very high speeds and getting plenty of airflow.
5. And, if I recall correctly, ramjets create "positive push," sucking air into their engines as they run. This force of suction would be helpful if normally generated airflow was blocked by a maneuver.
Also, a missile isn't going to be moving at "near zero" speeds. It has to keep its forward inertia and kinetic energy, otherwise it simply falls out of the sky. Unlike an airplane, a missile doesn't generate lift.
Actually IIRC a bunch of modern AAMs use a lifting body concept. It doesn't generate lift LIKE a plane, but it does generate lift.
4. The Meteor's flight profile is boost and coast, but even when coasting, it will be moving at very high speeds and getting plenty of airflow.
Plus it won't be making hard turns unless its in terminal guidance, and at that point the utility of a functioning engine (specifically one that fails during terminal guidance while the missile is still fast) may be somewhat questionable.
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