I would like to ask a hypothetical question:
would it be possible to convert a quasi-ballistic missile or a hypersonic missile or some kind of ballistic missile that can definitely be controlled and is very fast into a super long-range air defense system?
The idea behind this would be to track a target, e.g. a bomber or a fighter jet in a distance of 1500km to 2000 km with an OTH radar or satellite and then let the missile or hypersonic missile shoot at the position. The missile would then have its own powerful active radar system that once in range could then detect and lock on to the target and track it, and once the enemy initiates jamming action the radar would automatically switch to passive mode and track the jammer.
(Similar to the phenix missile).
There are 2 cases here from my point of view:
1.) Optimal case: Hypersonic or quasi-ballistic missile is in communication with the radar almost during the whole flight and can be steered by the stationary radar or by the satellite constantly in the direction of the target because it delivers trajectory correction data which allow the missile to correct in the direction of the target with an accuracy of a few hundred meters or a few kilometers. Once in range of the missile's own radar, the missile will then switch to the target by its own tracking radar.
2) Hardship case: Rocket has no contact with the ground station after launch. In this case the missile would have to remember the last position and the direction of the target.. A hypersonic missile would need about 6 to 7 minutes for 1500km range. A target flying at 2000kmh would then be a maximum of 250km away from its original location. It would still with worst setup still in radar detection range of the Hypersonic missile when the Hypersonic Missile arrives close to the target.
Here there are at least 3 conditions wich came in my mind wich must be fulfilled now:
- the target must be in the radar cone of the active rocket radar after a certain flight phase.
- the missile must still be maneuverable enough to hit the target.
- the target must be distinguishable and identifiable among many other targets (potentially including civilian traffic).
I have made the following scenario calculation:
Assumption: Hypersonic missile:
Speed 15.000 km/h
Altitude FL: 10.000km
Altitude HR: 30.000km
Takes about 6 to 7 minutes for 1500km (Tehran - Tel Aviv)
The hypersonic missile radar:
The radar of the hypersonic missile can be designed very powerful. The hypersonic rocket will draw the electrical energy for this from the engine, which should provide more than enough energy.
In my opinion, the radar can also be set significantly higher in terms of its electrical performance than a comparable radar of a fighter jet. It can be supplied with so much energy that components would burn out after only e.g. 20 minutes. Basically, the radar only has to stay alive for a maximum of 8 or 10 minutes. For this reason, you can certainly be very generous with the dimensioning of the radar. In this way, ranges of 400km or 300km would certainly be feasible.
Now to the Scenario:
From Tehran, a hypersonic air defense missile (callsign: HR) is launched to intercept a plane flying over Tel Aviv. HR has a own radar with a detection range of 400 km and a 70-degree opening angle. Lockon Range is 200km.The radar constantly emits a cone-shaped signal that follows HR's flight path and can detect any object within its range.
The target, a Zionist Fighterplane callsign: FL, is flying at a speed of 2,000 km/h and an altitude of 10 km in a northwesterly direction from over Tel Aviv, which makes it almost 90 degree angle to HR's flight path. the greatest probability for FL to escape the radar beam cone before FL is within the radar beam area.
View attachment 918247
Red arrow is FL`s flight path in comparision to the radar beam angle of HR. It is probably the best position for FL to flee from radar beam.
FL is first detected by HR's radar after 4 minutes and 18 seconds from HR's launch, during which time FL had traveled a distance of 133.32 km from his original location. At this point, HR had traveled a distance of 1,125 km towards Tel Aviv.
To intercept FL, HR needs to make a turn with a radius of 300 km. If HR makes this turn at its maximum speed of 15,000 km/h, it would need to endure a force of 4.45 G. (8 tonnes HR weight). When in Range Radar can lock on target and go for the last hunt.
Assuming that the missile's guidance system is accurate and that FL's course and speed do not change, HR will reach FL's position and intercept it after round about 7 minutes from the launch. By that time, FL would have traveled a total distance of 210 km from its starting point.
This scenario highlights the strategic advantage of hypersonic air defense missiles in intercepting fast-moving targets. However, it also underscores the importance of maintaining a constantly evolving defense strategy that can adapt to changing threats and technologies.
It would be much easier to Intercept a target flying with Mach 0.98.
Most of the Planes, even fighter aircraft never fly with afterburner.
This scenario was calculated and simulated, The Speed, altidude and calculations should be correct. If somebody interested PN me I will send calculations.
With this calculation we theoretically proofed that:
1. the target must be in the radar cone of the active rocket radar after a certain flight phase.
Even if Target is detected one single time and an not be tracked after Hypersonic Air defence missile launch, when the Hypersonic missile arrives position, the target will still be in radar cone range
2. the missile must still be maneuverable enough to hit the target.
Yes: with a weight of 8 tonnes (Kinshal missile is about 7 tonnes) missile will pull maximum 5 G for a 300km turn radius. Hypersonic missiles can generally pull up to 15 G constiniously.
3. the target must be distinguishable and identifiable among many other targets (potentially including civilian traffic)
No specific solution Maybe combination with AI possible?
Any Ideas on that?