So what is 3M22 Tsirkon (SS-N-33)? I have some thoughts based on written Russian sources, published test footage, and conversations with Ukrainian colleagues.
Is Tsirkon a “hypersonic (anti-ship) cruise missile? The answer is “yesn’t”👇🏻
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While renders from the past decade depict it as a rocket-assisted scramjet vehicle, similar to X-51 Waverider, this is not accurate to the system that has been fielded.
I suspect that they potentially depict an earlier Tsirkon concept that was abandoned or not pursued.
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Since the first live fire test in 2020, all published images and video have indicated a design substantially different design.
Rather than a scramjet vehicle, Tsirkon bore a striking resemblance to 3M55 Oniks (third image), Russia’s existing supersonic ASCM system.
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Oniks employs a rocket-assisted ramjet. At launch, a solid rocket motor aft of the ramjet’s combustion chamber accelerates the missile to the ramjet’s operating velocity and is then ejected.
Oniks’ ramjet can sustain cruising at ~2.5M at sea-level out to 600 km.
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Like Oniks, Tsirkon has an inlet cover with an Attitude Control System that executes a pitchover program to the target azimuth. Whereas Oniks’ ACS pitches it 90 degrees, Tsirkon’s ACS makes a small correction. The rest is completed with control surfaces or thrust vectoring.
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Test footage further indicates that, like Oniks, Tsirkon has an axially symmetric airframe with an annular inlet.
Tsirkon’s booster also lofts it to a dramatically greater apogee than Oniks before completing the pitchover program and transition to cruise phase.
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Additional test footage shows Tsirkon executing a shallow dive toward its target in terminal phase. This would be a very shallow, although not unheard of, descent angle for (aero)ballistic missiles.
So Tsirkon isn’t really an (aero)ballistic or sea-skimming missile.
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With Russian claims for velocity (1.66 km/s, ~4.8M) and cruising altitude (25-30 km), we can derive a few conclusions.
Tsirkon likely performs a high supersonic (4-5M) cruise at high altitude, then executes a shallow low hypersonic (5-6M) dive to low altitude in terminal.
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This profile is somewhat similar to the approach taken by the Soviet vintage Kh-22 supersonic anti-ship missile.
The primary distinction, aside from greater cruising altitude/velocity and terminal velocity, would be a much longer (and thus shallower) dive during terminal.
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Overall, Tsirkon bears a large degree of similarity to Oniks. Both Russian media and Ukrainian technical assessments indicate that Tsirkon is likely a deeply evolved derivative of Oniks.
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The Russians likely heavily iterated on Oniks’ rocket-assisted ramjet propulsion to enable it to deliver the performance needed to operate in high supersonic and low hypersonic flight regimes.
Russian media reports of aluminum nanoparticle additive fuel are one example.
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Tsirkon differs dramatically from Oniks in airframe construction and Thermal Protection System however.
Its airframe appears to make much greater use of composites for both structural and thermal performance.
12|20
Operating in high supersonic and low hypersonic regimes places much greater aerothermal loads on the vehicle.
In particular, the Russians likely faced serious engineering challenges developing a thermally refractory yet radio transparent material for the seeker radome.
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My overall assessment of Tsirkon is that it straddles the line between a high-performance supersonic cruise missile and a hypersonic cruise missile.
If a HCM is strictly defined as a vehicle that experiences hypersonic flow in most or all of flight, then it is not a HCM.
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Alternatively, if you define a HCM as a vehicle using scramjet propulsion, I believe that Tsirkon fails that criteria as well.
I do not see any compelling evidence that Tsirkon employs a scramjet as opposed to a high-performance ramjet.
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As a corollary, I’d like to touch on defense against hypersonic threats.
The 25 APR raid tentatively demonstrated Patriot’s ability to defeat low-end hypersonic threats with PAC-3 MSE and MPQ-65. It also, as usual, deflated much public Russian marketing about Tsirkon.
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That said, even low-end hypersonic threats are very stressing to currently fielded Air and Missile Defense (AMD) systems.
Only one of two missiles was intercepted. And none of the at least three Tsirkons employed against Kyiv from DEC 2023 to FEB 2024 were intercepted.
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Alongside Kh-32, Tsirkon has the greatest terminal velocity of any Russian missile system employed in Ukraine, 50-100% greater than Iskander-M/Kinzhal.
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While PAC-3 MSE is certified against faster threats, such as MRBMs, Tsirkon’s relatively low altitude in terminal will seriously stress MPQ-65’s sensor envelope.
This will erode PAC-3 MSE’s Pk and shrink Patriot’s defended footprint.
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Finally, the employment of Tsirkon not only highlights Ukraine’s need for sustained and sophisticated AMD assets.
It reinforces the urgency with which the U.S. and allies must continue to field new AMD capabilities to defeat Russian and Chinese hypersonic threats.
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As soon as I post lmao. After brief consultation with @Link_Plumeria, this looks to be similarly dimensioned to Yakhont’s warhead. Yakhont being the MTCR-compliant export version of Oniks.
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@Link_Plumeria There are a number of unique and interesting features of Tsirkon that I didn’t discuss in detail due to a lack of open source references. This is one of them.
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@hl_hp_ua It’s also difficult to disentangle a weapon’s inherent precision from Target Location Error, which is the difference between the aim point uploaded to the weapon and the desired target’s actual location.
@hl_hp_ua An example would be the strikes against the Artem Plant in Kyiv. Some of the cruise missiles impacted apartment buildings adjacent to it. That could be due to a lack of precision.
Or it could be due to TLE, with the Russians using slightly incorrect coordinates for the plant.
@hl_hp_ua So if your goal is to specifically defend military assets and infrastructure in Kyiv, as long as you prevent threats from reaching them, then your engagements are successful.
@hl_hp_ua That warhead may have submunitions or a chemical, biological, radiological, or nuclear payload that will affect a wide area, including potentially the defended asset(s), if it isn’t reliably destroyed.
@hl_hp_ua With CMs, this is less of an issue as the warhead will go down in the general vicinity of the intercept, which may be quite far from the defended asset(s)
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@Lesya_G @JSetka @P_Kallioniemi @MriyaReport @MriyaAid Hi Lesya, as you may know I was a volunteer on Walter Report, later Mriya Report, from May 2022 to January 2023.
I have Mriya Report internal communications that detail continuous coordination between MR and the MA board from the creation of MR in July 2022 through January 2023.
@Lesya_G @JSetka @P_Kallioniemi @MriyaReport @MriyaAid Given the turnover in the MA since then, I’m inclined to assume you may be unaware of that prior history.
The assertion there was no coordination between MA and MR is, from my perspective, demonstrably false. I’m happy to provide excerpted communications to that effect.
@Lesya_G @JSetka @P_Kallioniemi @MriyaReport @MriyaAid “Joe” refers to Joseph “Yehuda” Friedberg and “B” is Alexander Bakus, then MA’s Director of Treasury.
MR forked off from WR on July 17. Alex was intimately involved in the planning of this split and coordinated it with MA alongside Yehuda.
A brief round up of what we do actually know thus far about Iran's ballistic missile raid against Israel, named "Operation True Promise 2" by the IRGC.
Starting with the missiles, Iran employed 180-200 medium-range ballistic missiles (MRBMs), including Ghadr, Emad, and Kheibarshekan or Fattah-1.
A derivative of the Shahab-3, Ghadr is a liquid-fueled MRBM that ordinarily carries a single separable reentry vehicle (RV). These specfic missiles have been upgraded with maneuvering reentry vehicles (MaRVs).
Ghadr is one of the primary missiles Iran employed against Israel in April during "Operation True Promise."
A further development of Ghadr, Emad is a liquid-fueled MRBM that carries a single separable MaRV. Alongside Ghadr, is one of the primary missiles previously employed against Israel in April.
Although defense articles designated as Significant Military Equipment were exported to China without authorization, that SME does not appear to be classified.
The unauthorized hand-carry of defense articles, specifically technical data, to Russia, Iran, and Lebanon by RTX employees on personal travel with company-issued electronic devices likely only concerns unclassified defense articles.
Neither an Antenna Mast Group nor Communications Relay Group and Electric Power Unit are visible.
The CRG acting as the RLG's Launcher Control Station plus AMG and EPU are emplaced at a different site. RL1 enables the CRG/LCS to communicate with LS up to 10 km away via VHF.
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Remote launchers optimize PATRIOT's defended area against tactical ballistic missiles but create dead zones for airbreathing threats.
Remoting launchers in this instance is unusual as the RLG does not have Dnipro within its defended area for TBMs with PAC-3 or PAC-3 MSE.
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I won't detail the complete program history of S-300P/F/V as @ChungTzuW has already written excellent threads about them which I strongly recommend reading for context.
In short, all three systems emerged from a joint VKS/VMF/SV procurement program.
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VKS/VMF requirements were focused on ABTs (air-breathing threats) while SV requirements were focused on TBMs (tactical ballistic missiles). This led to a divergence into S-300P/F and S-300V using radically different missiles and radars.
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GLSDB has a range of >150 km while SDB has a range of ~110 km from a ~12 km release altitude and ~270 m/s release airspeed.
Position error due to accumulated inertial measurement unit drift is quadratically proportional to time of flight and range by extension.
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Per interviews with Ukrainian pilots, they are typically releasing JDAM-ER at ~8 km. As SDB's employment profile is likely extremely similar, this is going to bring its range to <100 km.
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