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Dude I keep hearing you yapping about Mian Channu, what Mian Channu, this?Recall the main incident in Mian Channu, which revealed deficiencies in Pakistan's Chinese-origin air defense system. It relies on outdated semi-active radar guidance that is ineffective against modern high-speed projectiles
That's all he can Bragg about to save face. There's hq9B and P to content with now. Let see if they dare another "mishap"Dude I keep hearing you yapping about Mian Channu, what Mian Channu, this?
Pretty sure Pakistan, India, China, and US agreed that this is a ****-up![]()
2022 India–Pakistan missile incident - Wikipedia
en.wikipedia.org
Also, semi-active radar guidance is not outdated, especially not against high-speed projectiles with significant altitudes, like an airbreathing supersonic AShM like BrahMos. When trying to intercept high-velocity targets the missile's seeker head has to account for large relative angular velocity, which if you have to use an active radar seeker would mean you have to choose between having a fixed forward radar aperture, narrow FoV, thus a possible drop in intercept rate, or have an actuating aperture, which reduces your aperture size on top of having extra weight far from a missile's CG, degrading flight performance and maximum range.
A semi-active seeker is typically lighter by quite a long shot and has wide angles of reception, and while yes this makes the missile vulnerable to ground noise and low return targets, when we are talking about conspicuous high-speed projectiles they specifically have high-velocity differential compared to the background and give pronounced radar returns.
And guess which navy relies on said conspicuous high-speed projectiles.
Although this may not be the appropriate thread for the discussion, since you requested it, I'm posting it here. I have conducted a detailed analysis of the intercepted capabilities of the LRSAM and HQ16FE against various flight profiles of the BrahMos missile.Dude I keep hearing you yapping about Mian Channu, what Mian Channu, this?
Pretty sure Pakistan, India, China, and US agreed that this is a ****-up![]()
2022 India–Pakistan missile incident - Wikipedia
en.wikipedia.org
Also, semi-active radar guidance is not outdated, especially not against high-speed projectiles with significant altitudes, like an airbreathing supersonic AShM like BrahMos. When trying to intercept high-velocity targets the missile's seeker head has to account for large relative angular velocity, which if you have to use an active radar seeker would mean you have to choose between having a fixed forward radar aperture, narrow FoV, thus a possible drop in intercept rate, or have an actuating aperture, which reduces your aperture size on top of having extra weight far from a missile's CG, degrading flight performance and maximum range.
A semi-active seeker is typically lighter by quite a long shot and has wide angles of reception, and while yes this makes the missile vulnerable to ground noise and low return targets, when we are talking about conspicuous high-speed projectiles that specifically have high-velocity differential compared to the background and give pronounced radar returns, well...
And guess which navy relies on said conspicuous high-speed projectiles.
defencepk.com
Wtf even is this?Although this may not be the appropriate thread for the discussion, since you requested it, I'm posting it here. I have conducted a detailed analysis of the intercepted capabilities of the LRSAM and HQ16FE against various flight profiles of the BrahMos missile.
800+km range BrahMos missile successfully test fired by Indian Navy
Given Parameters: HQ-9 speed (v_hq9) = 1225 m/s BrahMos speed (v_brahmos) = 1020 m/s Maximum altitude for interception (h_max) = 30000 m Initial distance between the 052D (defender) and the target = 10.9 km = 10900 m Time taken for BrahMos to reach h_max: Time_brahmos = h_max / v_brahmos =...defencepk.com
When in fact the Jiangkai II/Tughril class frigates guide its HHQ-16 missiles with a completely different set of systems (in Tughril's case SR2410C UHF surveillance + Type 517 VHF supplementary against sea-skim/low observable + MR-90 illumination). There's a reason why HHQ-16 had an extra "H" in front of HQ-16, or did that just fly over your head?

You're right that the HQ-16FE guidance radar is just one part of a broader system. On ships, other radars like the SR2410C and Type 517 support it. However, the specific limitations of the HQ-16FE radar's elevation coverage (0° to 80°) are still important to note.Wtf even is this?
You took the show board of the Guidance Radar of a Ground-Based HQ-16FE, assuming that it is somehow the only radar operating in an HQ-16 battery even when the show board itself is specifically labelled (3) HQ-16FE Guidance Radar, as in, the third part out of many of an entire system
When in fact the Jiangkai II/Tughril class frigates guide its HHQ-16 missiles with a completely different set of systems (in Tughril's case SR2410C UHF surveillance + Type 517 VHF supplementary against sea-skim/low observable + MR-90 illumination). There's a reason why HHQ-16 had an extra "H" in front of HQ-16, or did that just fly over your head?
Steep-Dive Trajectory:Not only that, do you even know how Soviet-Russian AShM flight profiles work? You mentioned the "steep-dive" trajectory exploiting the top blindspot, how does the BrahMos arrive dead atop its target, does it teleport above the target with yoga magik, or I dunno, perhaps it has to either climb or cruise to them?
Do you know why Soviet AShMs like to have steep-dive trajectories instead of remaining full-stage sea-skim? It's because of this:
View attachment 43462
Figure out for yourself what an AShM have to go through to cripple a carrier in different trajectories.
I'm glad that you found it helpful/entertaining, on top of being "cold" and "logical" because I sure felt like throwing some personal attacks after this@Harbyharb . While many will advise you not to engage in these debates, i for one learned a great deal from your engagement. Masterclass! Load of technical information, no personal attacks and no rose colored glasses. Just cold hard fact with logical conclusions. Maybe my favorite series of posts since the new forum opened. Thanks for the illuminating info. Bravo!
NO.You're right that the HQ-16FE guidance radar is just one part of a broader system. On ships, other radars like the SR2410C and Type 517 support it. However, the specific limitations of the HQ-16FE radar's elevation coverage (0° to 80°) are still important to note.

And, well, just perhaps, that the BrahMos, can I dunno, get shot while flying at a high altitude before being dead atop its target?Steep-Dive Trajectory:
- The BrahMos missile can climb to a high altitude and then dive almost vertically onto the target. This isn’t “teleporting”; it’s part of its flight profile.
This not Indian navy thread, stick to the topicThe Indian Navy's frontline SAM is the Barak 8, which is already installed on P15A/B guided missile destroyers and INS Vikrant. Now, 7 more P17A frigates sailing in the waters of the IOR are also slated to be equipped with this modern SAM. Meanwhile, our domestically developed VL-SRSAM will be fitted on future vessels, including the 6 Next Generation Missile Vessels contracted by the Indian government. The Shivalik-class vessels are scheduled to receive these VL-SRSAMs as part of their MLU. Recently, these ships have been observed conducting BrahMos missile test firings. In parallel, the Indian Army and Indian Air Force are actively integrating Barak 8 MRSAM squadrons, complemented by the Akash SAM featuring an active radar seeker.

Recall the main incident in Mian Channu, which revealed deficiencies in Pakistan's Chinese-origin air defense system. It relies on outdated semi-active radar guidance that is ineffective against modern high-speed projectiles
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