later I realized it could make sense to look upwhat's discussed in this page I think boils down to minimal range of an SM-2
now I used google, didn't find it: sources to various extent boast about its maximal range though LOL
anyone?
Faster launch rate is the most obvious answer.Why the PLAN would hot launch their HHQ-16 when the PLA cold launches their HQ-16 is beyond me. You would think they would try to be compatible.
Any combination of dual-packing, triple-packing, quad-packing, or even more are possible with the UVLS. The UVLS is not limited by the CCL method of venting exhaust.So now I am thinking, hypothetically, what if the next generation 054 frigate uses U-VLS instead? Of course the HHQ-16 can more than fit in, but the system of which how it will fit, is going to be based on the CCL (Concentric Canister Launcher) concept. The HHQ-16 canister would have to fit into a larger canister. Due to the hemispherical end cap, both canisters appear preferably cylindrical, which would be convenient for the current HHQ-16, this being the most simple CCL design. Do note that by going CCL, the VLS does need to be bigger in diameter than if it were hot launched, which is where the U-VLS steps in. Note that this does not mean that other CCL designs have to be cylindrical designs, or cylinder in cylinder, you have to be creative in designing the end cap so it would route the gas flow to any space between the missile inner canisters.
Well, I think there's hardly anyone who would use SM-2's a primary weapon in the terminal phase of anti-ship missile interception and we all can agree on that I assume?
In size they are similar, but in range they are vastly different. The SM-2 is probably >3 times the range of the HHQ-16.SM-2 is 700-750kg, closest analogue is HQ-16.
Highest figure for booster-less (600 kg weight) variant of sm-2 i found was 118 km of range. HQ16 is usually credited with 40-50 ranges. We know new russian buk-3 missiles are credited with 70 km range.
We also have this recent image of peculiar missile, possibly hq16c. Weight wise, there is no reason for it or some future variant of hq16 not to at least match highest sm-2 range. If electronics can be made smaller than in sm-2, which they very well could be since the said range was claimed for 1980s variant of the missile, there is no reason same or better autopilot using same or better trajectory and rocket motor being same size or larger could not achieve AT LEAST the same range.
But, as said, sm-2 was not the only self defense missile. sea sparrow was used for close defense, against incoming sea skimmers. If it wasn't more effective at those ranges, USN would not have put it in its VLS alongside sm-2.
Since we've no evidence of a smaller missile serving alongside hq16, it is plausible hq16 is designed to be as effective at intercepting missiles as it can be. But perhaps at a cost of other roles, possibly medium range anti aircraft role.