This is a very interesting study, and this isn’t like a random guy, he’s an actual engineer that works on literal 5th gen aircraft and research for 6th ones.
And although this study isn’t supposed to represent the actual missiles it’s still very interesting and can be used for comparisons between missile classes.
Very interesting that from a sea level launch it tops out at M2.0, but i think it’s interesting knowing about weaknesses (and strengths) of the ramjet design.
I feel like that would actually be restricted by the throttle-able ramjet, there aren’t any sources that say the meteor is supposed to be Hypersonic, and the author states that in the simulation it’s modeled as a fixed thrust ramjet for comparison sake.
And the extra speed could just cause more drag causing loss in range anyway, meteor cruising along at M4+ is more than enough.
If the missile body even has the structural strength to go that far. I wouldn’t be surprised if it just falls apart in the hypersonic regime. Still interesting to think about how far the engine could push the missile if you disregard a couple things
This is why also in an environment with stealth aircraft the ramjet design might prove a detriment because you couldn’t take advantage of the full range (can’t get a track at 200km) and would be at a disadvantage if fighting at lower altitudes against solid propellant rocket missiles.
Makes sense they want an AESA on the Meteor and remote guidance trough the F-35 is considered to be the way forward.
I’ve seen 30g being mentioned somewhere on the Forum. But as far I’m aware there are a grand total of zero sources telling us anything concrete about it’s maneurvrability. You could try asking in the Fox-3 topic, maybe they have smth concrete