shiv wrote:wen wrote:
And thats why the USA is quite serious to this threat to the degree they adjust quite some of their projects to meet this threat (e.g. downsizing DDG1000 whilst increase DDG51 orders, develop super-long ranged unmanned air-carrier based bombers, etc).
Sir - you are citing the US's reaction as "proof" that nonsense works? if a woman adjusts her blouse when I am nearby it does not mean that I am about to fondle her breasts.
You have yourself stated that guidance is done in space. Space is more than 75 km up. Your missile will miss by several kilometers. Unless you can tell it where the carrier is in the last 5 seconds of its flight.
Now tell me if your missile will travel 75 km in 5 seconds? At Mach 45? Yes Forty-five times the speed of sound. Only. Did your teachers never discover that you are a liar? Is this the sort of stuff they teach in China? You are making me laugh. Your countrymen are losing face because of your stupidity.
You have no idea:
You are talking about the so-called "black-window".
It is not the case the warhead will automatically enter the black-window when it enter the atomophere, it depends on many factors:
1) Aerodynamic frame: the aeroydynamic frame of warheads are highly-low resistance one, thus much less heat is generated, comparing with other type of much larger and much "fatter" re-entry vehicles. thus less black-windows.
Actually, without the requirement of terminal trajectory adjustment/active seeking, nuclear warhead actually want this black-window for stealth puprose, and it requires the nuclear warhead to be designed in a special way and to adding special coating material to improve the fricitions to generate sufficient heat (which is a necessary condition of creating such black window) to creat this ionization layer around the warhead to absorb radar waves.
2)The black-window is not always on, usually this is only occurs somewhere around the ionosphere of the atomosphere, at most 30km-80km above the earth (the American Pershing II's terminal trajectory correction is: pass the atomosphere to as low as 30 km above earth than switch the active seeking radar on, and do the correction then).
So thats at most ~50km, and if we assuming:
(1)AShBM recived the last signaling update about the carrier's current location through satellite/long-range unmaned scout aircraft/OTH radar before retry this ionization phase (assuming to be 80km above earth) and correcting its trajectory accordingly.
(2)The re-entry trajectory is at 45 degree to the surface (earth).
(3)It opens its terminal active seeker at 30 km above earth.
(4)The speed of the missile is Mach 10, or ~10000 km/hour.
(5) The aircraft-carrier travels at its maximum speed (60km/hour) to some random direction.
Then:
(a) It takes 25 sec for the AShBM to passing the ionization phase.
(b) During the 25 sec, the maximum displacement the AC can achieve, is merely 416 meter, or roughly an unit lenght of the heavy carrier.
(c) Considering the measurment errors of satellite/unmanned scout aircraft/OTH radar etc, the total error is assuming to be 5000 meter away from hitting the AC.
(d) It takes 15 sec for a Mach 10 missile from now to hit the AC.
(e) During which time the AC can at most, travel a futher 250 meter, which is less than its length, to some random direction.
(d) Thats a totally 5250 meter to correct.
(g) To correct the trajectory within the terminal phase (<30km above earth), based on the above assumptions, it only takes, on average, way lower than <10 g-load's terminal phase maneuver to correting the measurement errors and the error introduced through the air-carrier's futher displacement, and 10-g-load maneuver is nothing for a warhead, most of the combat aircraft can do near 10-g-load, and modern A-A missiles can do 100 g-load maneuvers.
Therefore, we can see, based on the above assumpitons, the primary source of error should be the measurement errors, whether the Aircraft-Carrier trying to escape at full speed doesnt really matter much, since comparing to a 10-mach AShBM, 60km/hour AC can be almost treating as a static target.
The AC is simply too big and too slow to escape the AShBM.