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UPDATE: ONLY 38 copies left….NOW that is a deal: The Hush-Kit Book of Warplanes is STILL half price for Black Friday https://unbound.com/books/hushkit


When you’ve flown 52 different aircraft types (and counting), you often get asked what your favourite is. So, it was a welcome change when I was asked to choose the ten worst aircraft. No holds barred, the more brutal, the better, was the brief; but, despite my best efforts, I can only think of seven that truly deserve my savaging.
Sure, I’ve flown aircraft with ‘interesting’ handling characteristics that, if ignored, can cause massive embarrassment massive embarrassment and in some cases a not insignificant amount of paperwork (such as being aggressively flicked out of a turn whilst pushing that little too much and thinking “I’ll just sweeten this shot with a touch of VIFFâ€, or encountering yaw divergence for the first time after rapid rolling for more than the 360 degree limit you’d read somewhere in the Aircrew Manual but completely forgotten about, that sort of thing), and sat in cockpits that defy all logical design criteria and hide essential switches in the most bizarre of places, or place things like ‘weapon jettison’ buttons adjacent to gear buttons and flap levers (thereby increasing the risk of inadvertent jettison when putting the gear down in the dark and leaving a fuel tank or two in someone’s back garden).
“Hovering a Wessex was like trying to hover a semi-detached house from the upstairs bedroom window.”
But does that make them bad aircraft and, hence, the worst to fly? No, that’s just aviation, and having experienced enough variety so far I can compare and contrast and see that repetitive design faults are not deliberate, they just happen. And aerodynamicists don’t purposely make their aircraft dangerous to fly, it’s more that foibles in aircraft handling come about because design compromises have to be made to satisfy an overall design specification. Also, there’s no such thing as a perfect aircraft. It’s a bit like cars – they’ll all get you from A to B in their own unique way, some faster than others, some with higher levels of comfort, some with no comfort at all, and some will inherently pull to one side when you brake, and there’s no international standard when it comes to which side of the steering wheel the indicator stalk lives on. But you get used to all of that and drive accordingly. And so it is with aircraft, but, like cars, some really do stand out from the crowd as unlovable stinkers. So here goes, in no particular order………
Grob Tutor

As a budding RAF pilot, I cut my teeth on the Scottish Aviation Bulldog back in 1988. I didn’t know much as a pilot back then, having only flown the venerable de Havilland Chipmunk and the Cessna 150. But what I did know was that the Bulldog was a joy to fly – with a compact and easy to manage cockpit, agile handling and enough power to fly aerobatics without having to trade height for speed, what more could I want?
Alas, all good things, like civilisation and a bottle of good whisky, come to an end. When the Bulldog went out of service, in stepped the drearily sluggish Grob Tutor. What a contrast – heavy in roll, festooned with checks despite not having much more in the systems department than a Bulldog except for a GPS navigation control unit that alone took hours to get to grips with (the Harrier was easier to flash up and get going), and it always finished aerobatics lower than where it started.
The first time I flew one was 15 years after the Bulldog, 13 years after I joined the RAF, and I’m glad it didn’t figure in any of my flying training. I’ve said it before – would I buy one even if it was the last aircraft on Earth? No, I’d craft an aircraft from coconuts and old bin bags scratch instead.
However, if, and only if, there is a plus side, I suppose it’s passable as a clipped-wing motor glider.
Harrier T.Mk.10 ‘The Hump-Jet’


“What?!†I hear you scream, as you throw your martini at your butler, and spit your tiramisu out in rage,
“Has he gone mad?â€
Well, not exactly. The T10 was a two-seat training variant of the excellent Harrier GR7, and there are two reasons why the T10 is on my list – its general inability to hover because of its extra airframe weight and the use of a Pegasus 105 engine that was the same as the lighter GR7’s, so unless stripped of weight (wing stores) and flying on cold, high atmospheric pressure days, forget about attempting all that fun VSTOL stuff. Oh, and one too many seats. Enough said.
Beagle Bassett ‘Shirty Bertie’

This aircraft goes down as the worst aircraft I never flew. Eh? How can that be? Well, ‘Bertie,’ as the Empire Test Pilots’ School Bassett was affectionately known, was a highly modified, variable stability test bed aircraft that until recently was a stalwart of the ETPS fleet.
Capable of simulating the flying characteristics of any other aircraft through the intervention into the right-hand seat flying controls of a very complicated box of tricks on the cabin floor that could be fiddled with and adjusted to change performance through control responses, it really was quite a machine. However, due to the limitation of not allowing the box of tricks to have its say below a minimum height in case it ‘threw a wobbly,’ the person in the right hand seat wasn’t allowed to physically fly Bertie anywhere near the ground. In my capacity as the ETPS Multi-engine Instrument Rating Examiner at the time, it was my job to test the person in the left-hand seat (who had an independent, original, non-modified set of flying controls) and make sure he could fly solely on instruments, predominantly in order to return to an airfield and land in inclement weather.
As a result, the test profile was conducted no higher than about 3000 feet above the ground. And well below the box of tricks minimum height. So despite conducting this annual test around four times at ETPS, I never actually flew Bertie, only in Bertie. And that, as a pilot, is frustrating. Top tip – never fly when you’re angry or frustrated, as it’ll probably mean you rate the experience poorly and end up slagging the aircraft off in an article about the worst ones you’ve flown. (Of course this was not actually Bertie’s fault, bless him, and he’s now enjoying his retirement at the Boscombe Down Aviation Collection).
Westland Wasp ‘Balancing a pyramid on a castor’

As a fixed wing pilot, I’ve been lucky enough to have flown eight helicopters over the years. My first experience was the pre-Harrier hover course, a weeklong stint at RAF Shawbury flying the Squirrel helicopter where my brain was taught how to stop then land, as back then it only knew how to land then stop. And I would suggest that’s quite important ahead of being let loose with a Harrier. Since then, I’ve flown the Agusta Westland 109, Lynx, Gazelle, Jet Ranger III, Schweitzer 300 and the US Navy UH-72, all with helicopter instructors and hence all my hands-on from lifting to landing. As I said, I’ve been very lucky. I like helicopters.
And as luck would have it, one day when I was about to take a Piper Warrior for a flight out of Thruxton airfield near Salisbury, I was offered the opportunity, completely out of the blue, to fly in a Wasp that had just had some maintenance performed on it and needed a check flight after something called ‘blade tracking’. I said I like helicopters, but I don’t profess to understand how they work, but I do appreciate that any angry palm tree/large collection of rotating parts flying in very close formation requires a lot of very special and considered care and attention. So, I wasn’t worried when told that we were going to see how much vibration there might be, and hopefully at acceptable levels. After all, helicopters vibrate even when they stand still, so this was just a matter of keeping it all in check. Anyhow, after a successful take off and flight to assess said vibration, during which I have to say I was quite enamoured by the vintage and overall quirkiness of this little helicopter, I was allowed to fly it back to Thruxton to land. It was during the last four feet of the flight that I began to think, ‘I’m not enjoying this’.
I knew how to hover, how to pick a ground reference just forward of the nose on which to ‘formate’ and stay steady against, and yet I had to choose one dandelion after another as I proceeded to move randomly across the airfield in a desperate attempt to stay put and land. This was quite frustrating (see advice above about flying frustrated), and it dampened my initial attraction to the Wasp, but after some time seemingly having to totally relearn how to fly a helicopter (it’s not really that easy in the first place when you’re a novice, made even harder when your steed seems to have a mind of its own), I landed. Subsequently I asked some former Wasp pilot mates of mine whether I was alone in my inability to hover the damn thing, and they said “No, to begin with its a bit like trying to balance a pyramid upside down on a single castor, but you get used to it!†Ah well, maybe I’ll be lucky again in the future and have a second chance to get used to it, but until then, it’s definitely on the list.
(Another favourite helicopter analogy of mine was hearing how hovering a Wessex was like “trying to hover a semi-detached house from the upstairs bedroom window.†Somehow helicopter mates tend to come out with the best analogies, and I add it here for your delectation).
Boeing 767 ‘The Power Couple’

I’ve only flown the 767 simulator, but due to the fidelity of modern-day simulation, I can only assume the real thing is just as crap. I currently fly the 787-9 as my day job – which, through its fly-by-wire flight control system allows me to hand fly what feels like a big Cessna – and yet I still have to trim the aircraft when changing speeds or changing flap settings, and there’s plenty of feedback, which for any pilot is vitally important. But at least when I put on loads of power to speed up, or conversely take power off to slow down, the aircraft doesn’t try to reach heaven or bury us all in the nearest part of Mother Earth.
Because that’s what a 767 tries to do.
The ‘pitch/power couple’ as it’s called (an aircraft’s want to pitch up with power, or nose down on power reduction) is alarmingly strong on a 767. I’d been warned about it in the briefing before the simulator session (and that alone speaks volumes about this Boeing design), and sure enough, what a handful. There’s something quite alarming about having to dial nose down trim in as you accelerate such that you’re still having to push hard whilst doing so. Let alone pull like a dingbat whilst decelerating as the trim can’t operate fast enough. Overall, sub-optimal, and I’ll stick with my 787, thank you very much.
(Incidentally, my venerable old 747-400 didn’t behave anywhere near as badly either, so what was going on in the 767 planning meetings is anyone’s guess, and my ex-737 colleagues speak of similar things there).
Short Tucano TMk 1

Before I start pulling the Tucano to pieces, I just want to say that I loved flying it. I flew it as a student, so I have some lovely memories of flying solo as high as 25,000ft, strapped to an ejection seat, pulling up to 6g without a g-suit. And I was an instructor on it for my first tour in the RAF, as well as at Empire Test Pilots’ School as their Standards pilot. I flew it to Sweden, Denmark, the Czech Republic, Germany, Belgium, Portugal, France and all over the UK. I thoroughly enjoyed flying aerobatics in it, and never had a major emergency in it.
So, how come it’s on this list? When I talk to friends and colleagues about their memories of the Tucano, it’s the worst aircraft they’ve ever flown, so by democractic principles, it’s also one of mine. It has to be, right? It wasn’t a jet, so totally inferior to the Jet Provost it replaced, and the secondary effects of being propellor driven meant it never had ‘jet-like handling’ despite what it said in the Embraer sales catalogue. Its build quality was a little suspect, for sure, but it wasn’t my airbrake that fell off. Apparently, it could have done with automatic rudder trim to compensate for the torque effect of 1100 shaft horsepower, but to be fair using the electric rudder trim on the throttle wasn’t exactly arduous. So according to everyone else, the Tucano was one of the worst aircraft I’ve flown. But actually, according to me, she was one of the nicest and I miss her.
Klemm Kl.25

In another case of being in the right place at the right time, a very good friend of mine was given the responsibility, and it was a huge one, of periodically airing a Klemm 25 down in Wiltshire. Built in Germany between the wars, the Klemm 25 was officially branded as a ‘light leisure, sports and training aircraft’ and no doubt was used to train quite a few ‘civilian’ pilots to get around those pesky Treaty of Versailles rules that prevented Germany from training pilots for a Luftwaffe it wasn’t supposed to have.
Removable wings are quite handy if you don’t own an airfield, or if your hangar is a bit on the small side, and especially useful in the ‘30s when you could tow your aircraft home and park it on the drive. I’m pretty sure if you did that today, well, you can probably imagine what would happen, you’d get Arts Council funding granted and be bothered by culture-vultures treading on your flowerbeds, but I digress.
I found myself standing in a field watching the wings being attached and on closer inspection I began to realise that ‘basic’ is an understatement when it comes to describing the work of Herr Hanns Klemm back in 1928.
Accustomed as I am to all the mod cons and electronic wizardry of 21st century aviation, the Klemm is akin to comparing a 1969 Hillman Imp to a Bentley Continental GT – in an Imp you’re not sure when you insert the key whether it’ll start or not, electronics hadn’t even been invented for the motor car when it was made, you better have a mechanically sympathetic driving style as well as an ear for impending mechanical doom, and best wear a coat as it’ll be cold (no such worries with a Bentley).
And so, it was with the Klemm. Noisy, windy, I couldn’t hear a word Charlie was saying in the front seat as there was no intercom, and no instruments to speak of – there was an airspeed indicator, a clock, an engine rpm gauge, a compass, and a rate of climb and descent indicator. That was it. The Klemm is a true seat—of-the-pants aircraft (as well as just being a pants aircraft) and you have to rely on senses you have but rarely call upon in order to fly it, and I freely admit that I was out of my comfort zone. But am I complaining unduly? Probably, as it is of its time and some 600-odd were built, which even by today’s standards of small aircraft production is really quite an achievement. So, is it truly one of the worst aircraft I’ve flown? I suppose only when compared to aircraft that came after it, and that’s like using hindsight when analysing a historical event and suggesting it would have happened differently had one been involved.
I was very lucky to fly the Klemm, it gave me my one and only insight to date into the very early days of aviation and just how actually cutting edge it would have been almost 100 years ago. And yes, I own a 1969 Hillman Imp that I wouldn’t trade for a Bentley Continental GT even if you paid me because it’s good, clean, honest fun to drive and reminds me of the basics.

So there you have it, my take on what I think are the worst (and indeed not actually worst at all) aircraft I’ve flown to date. My opinion, my list, and I’m sure I’ll get an email or three from some real Tucano haters, and that’s fine.
But as Air Marshall of Necromancy in the Hushkonian Air Force, watch out…….
Matt Doncaster, 787 pilot, former Harrier pilot and Air Marshall of Necromancy in the Hushkonian Air Force
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The attack helicopter is costly and complex to operate, yet it is taking a mauling in the Russian invasion of Ukraine. Russia’s full-scale invasion attempt of Ukraine starting in 2022 has shown both the vulnerability of helicopters and the effectiveness of small, uncrewed aircraft against armour. With this in mind, we ask: Is the attack helicopter dead?
Few observers thought Ukraine could withstand the Russian onslaught of 2022. Footage released in April footage of the destruction of a Russian Kamov attack helicopter was a huge morale boost. And more followed. The war in Ukraine has been marked by staggering losses of both anti-armour helicopters and armour.
Armour operations
Typical Western doctrine (offensive or defensive) uses manned armoured reconnaissance ahead of the Forward Line of Own Troops (FLOT) to locate enemy forces and determine their intentions. Increasingly, manned operations will be supported by other ISR (intelligence, surveillance, and reconnaissance) platforms, such as Uncrewed Air Vehicles (UAV) and later Uncrewed Ground Vehicles (UGVs), to augment the manned platforms.

Recce: This is driven by a recce Plan determined by the Commander’s Critical Information Requirements (CCIRs), designed to fill in gaps in intelligence and distinguish enemy feints and deception tactics from their main force’s true intentions and timing. Other objectives would typically be to locate enemy command and control, logistics, air defence units, long-range artillery, and other high-value/high-threat components.
The recce info will then shape the deployment of main armour and infantry (again offensive or defensive), supporting anti-armour helicopter and precision long-range artillery operations.
Manned armoured reconnaissance beyond the FLOT (i.e., in enemy territory) is likely hazardous, particularly if the enemy has effective electronic surveillance capabilities. Traffic analysis can be used to locate signal traffic from unknown forces and, even if encrypted, is likely to result in unwelcome attention. The US tends to assume its comms cannot be read, so it reports every enemy observation. The UK is more concerned about detected transmissions (even if not read) and operates largely under radio silence.
Terrain masking to avoid detection may make Very High Frequency traffic difficult, so HF or datalink to SATCOMs may have to be used.
Armour and Mechanised Infantry: In addition, armour, on both sides, is having a hard time. In the Ukraine case, the threat has proven to be a combination of precision artillery and long-range missile attack, combined with top attack by armed drones.
The author identified this latter threat as a concern more than a dozen years ago – having noted that Hezbollah, in the first Lebanon conflict, had deployed armed drones against Israeli armour.
Because the high mass of protective armour leads to weight and mobility issues, MBT protection is concentrated against direct fire attacks from other MBTs. Top protection is typically reduced, primarily against artillery near misses rather than direct hits, which are now the norm. Even with these measures, deployed MBT mass is typically around 62 tonnes, and top protection is one area that is typically traded off to achieve acceptable mobility.

Active protection systems are not yet regarded as mature and may introduce hazards to nearby personnel (if operating with infantry, for example). I am unsure how successful these are in Israeli use, or whether they have been used successfully in Ukraine.
Furthermore, Western armour generally has no organic means of detecting or countering the drone threat, although directed energy weapons or RF countermeasures may offer some capability in the future and are undoubtedly being actively researched and trialled.
So heavy armour is looking increasingly vulnerable, as, in the Ukrainian conflict at least, attack helicopters. However, heavy armour is clearly still important for taking and holding ground, so it will most likely continue to be central in many operations.
Attack Helicopter operations

When the UK was developing its thinking for GST3971 to acquire a dedicated attack helicopter in the mid-1980s, the vision was of a helicopter that could engage in autonomous direct-fire attack of heavy armour. The threat was essentially Cold War, with massed Soviet armour operating across the North German Plain. Organic air defence (then primarily radar-directed ZSU-23-4) was a significant threat, leading to a desire to stand-off outside its lethal range. Priority targets were enemy air defence, command and control centres and heavy armour.

The solution was deemed to be a low-signature helicopter (radar and IR signatures, particularly) fitted with a mast-mounted sight and using terrain screening. A long-range fire-and-forget weapon was required so that the helicopter would not be exposed throughout the weapon’s flight time.
Initially, Apache was not favoured because the AH-64A was regarded as having large visual and radar signatures and an inadequate sighting system. Without a mast-mounted sight, Scout helicopter support would also be required for target acquisition and designation.
The AH-64D with Longbow and RF Hellfire largely solved these problems by acquiring targets at long range and engaging in indirect fire. However, the missile and target detection range exceeded the recognition and identification range of the TADS sight (which also required the helicopter to be exposed to gain a line of sight to the target). This introduced some concern about the ability to achieve positive target identification when operating under restrictive rules of engagement.
The Situation in Ukraine
Russian operations over Ukrainian-held territory
Today, taking the Ukraine experience as representative, Russian attack helicopters are operating over large regions of Ukrainian-held territory without air superiority and with a dispersed infantry threat armed with capable MANPADS systems. The defending forces can adopt positions that are well hidden, but which offer good fields of fire.
The difficulty of detecting and countering this threat, combined with extensive areas lacking terrain cover, significantly increases the risk to attack helicopters in transit to and from their targets. This is compounded by the apparent ineffectiveness of the helicopter protection and countermeasures equipment.
There are reports of both sides in Ukraine using armed drones for anti-personnel operations against individual soldiers, so operation under cover, if not actually below ground is becoming necessary, if there are enemy drones in the area. This undoubtedly reduces the opportunities for, or increases the risk of, MANPADS operation.
Ukraine perspective – early phase
In the early phase of the invasion there was an armoured attack along the borders, but particularly moving south towards Kyiv from Belarus. This was largely canalised along main routes, as were its supporting logistic columns. This resulted in heavy losses. These were inflicted mainly by mines and artillery. Flooding of off-road terrain reduced the transit route options for the invading force.

Later Developments
After being pushed back from Kyiv in the initial armour thrust, Russian armour and mechanised infantry have been grinding out attacks from Ukraine’s borders, particularly from the south and east. This relatively static land battle is accompanied by long-range missile attacks on critical infrastructure and population centres.
Both sides have effective anti-aircraft missile systems, and neither side has achieved full air superiority over the battlefield. The later Russian attack has featured the use of medium- to long-range stand-off weapons (cruise or ballistic missiles and glide bombs), air-or ground-launched, often from within Russian territory. There seems little scope to counter this, while the political does not exist to mount attacks on launch locations well into Russian territory. The best possible missile defence system may ameliorate damage but will not hasten the end of the conflict, which has become strategic rather than tactical.
Significant numbers of western ground-to-air missile systems are also being supplied. Ukrainian anti-armour operations have increasingly been able to use precision artillery such as HIMARS and ATACMS. The availability of such systems and their munitions is likely to be in short supply and is dependent on enduring political support from EU and NATO countries. It is, therefore, vulnerable, for example, should Donald Trump be returned as US President following the November election.
It seems likely that NATO surveillance assets (E-3, RC-135W, U-2S and satellite cover) are gathering real time intelligence over the battlefield – whether such information is being passed to inform Ukraine deployments and targeting decisions has not been revealed. In any future conflict, using such overhead assets and effective datalinks to transmit near real-time intelligence is likely to be key to effective offensive or defensive operations.
Both Russia and the Ukraine have adopted the use of armed drones for the top attack of armour and these appear to have been very successful. (Relatively little imagery has been released showing Ukraine anti-armour helicopter attacks on Russian armour, or indeed Russian helicopter attacks on Ukrainian armour – Western or otherwise).
NATO nations are beginning to supply air-to-ground weapons such as Brimstone and Storm Shadow, and F-16 aircraft have entered Ukrainian service. It is not known whether Western air-to-ground missiles have been integrated for release from existing Russian-built equipment operating with the Ukrainian Air Force.
Suggested Success Factors for Helicopter anti-armour operations

What do you need for successful helicopter anti-armour missions? Ideally, you want air superiority and not to operate over large swathes of enemy-held territory occupied by determined resistance, equipped with capable MANPADS and other air defence systems such as S-200 and S-300.
Here is a list of possible success factors for postulated helicopter anti-armour operations.
Defensive Operations
The above factors suggest that deploying attack helicopters operating defensively (over one’s territory) could still be effective.
If the enemy uses the same or similar equipment, there would still be problems to solve regarding positive target ID. Also, effective command and control to deal with a fluid ground situation could be problematic, as could maintaining a supply of munitions to the AH force. Missile countermeasures remain an uncertain problem.
Offensive Operations
Long-range indirect fire engagements would be preferred for both offensive and defensive operations, and they would probably be essential in the offensive case.
The high helicopter losses sustained by Russia in current offensive operations probably reflect high risk operations, in the face of determined opposition with capable weapons and not much terrain cover for the helicopters. Also, no air superiority to provide top cover and hinder ground air defence, together with apparently ineffective measures to hinder missile lock-on and to break lock, once engaged.

Moreover, the threat is not the organic air defences of battlegroups or a Soviet Motor-Rifle Regiment or Brigade but dispersed and well-hidden infantry and special forces units equipped with modern MANPADS missile systems. Furthermore, because the enemy forces are operating over the defenders’ own ground, the defence can be cued and alerted to approaching helicopters, given good data connectivity.
In the case of offensive operations, it would appear that stand-off operations from the ground already held by one’s own forces might be the order of the day. In this case, the helicopters might operate similarly to a highly mobile precision artillery unit, able to redeploy kilometres across the field of operations in minutes. With a lack of local air superiority, the Russian use of stand-off weapons launched from within their territory supports this proposition.
A further consideration is that maintaining the mobility of the helicopter force is likely to benefit it by hampering any drone threat targeted at it.
The focus of attack might shift towards enemy logistics – MBTs without fuel or ammunition cannot conduct manoeuvre warfare.
Increasing the range at which the attack is conducted could suggest the use of larger helicopters to carry the heavier weapons likely to be required – feasible if operating over safe ground. The carriage of Exocet on certain export Sea King aircraft is an example of such a usage. Rafael Spike and Brimstone are also attracting interest because of their long-range capability. Clearly, target selection would be entirely dependent on the higher-level ISTAR infrastructure, although salvo-fired Brimstone has already shown some autonomous target discrimination capability.
An alternative to using one heavy long-range missile per tank destroyed might be to use a larger helicopter to launch long-range drone-carrying systems. This could allow several medium helicopters to launch attack and surveillance drones into a given operational area, possibly in the enemy’s rear. Command and control, logistics, comms, armour, barracks, and hardened targets could all be engaged in this way.
Forward-launched recce drones could provide target designation and satisfy positive ID requirements when operating under tight rules of engagement.
Such an approach could also overload the enemy air defence command and control and be usefully deployed in conjunction with simultaneous missile and/or manned aircraft operations.
This capability is alluded to in several planned US programmes, including the abandoned FARA and FLRAA. We are talking about air-launched effects (LE) for reconnaissance or attack and Future Tactical Unmanned Aircraft Systems. The air-launched effects were described (Vertiflite March / April 2024) as being deployed from FARA, FLRAA and Black Hawk “to decoy, disrupt or destroy enemy air defences and to spot targets for joint forcesâ€. The same article indicates that â€the Army plans first flight of a fully-integrated ALTIUS – Air-Launched, Tube Integrated Unmanned System from a Black Hawk this year†potentially for a rapid fielding decision in 2025.
The US’s â€long-standing interest in technologies that enable a single operator to control multiple UAS is associated with this.â€
Perhaps network-enabled command and control, ISTAR, and other means of target verification can integrate existing AH capability in defensive operations. Medium helicopters operating further back could launch a mix of longer-range weapons and ‘Launched effect UAS’ in both offensive and defensive scenarios.
Further to the suggestion of stand-off medium helicopters for anti-armour ops over enemy territory (and the US reference to Air Launched Effects), see here.

It is also worth noting that Sea King was cleared for export customers to launch Sea Eagle (India) and Exocet (Qatar, Pakistan), suggesting plenty of payload for air-launched systems controlled by medium support helicopters. [A good role for the FAA Merlin Mk.4 force?]


The Drone Threat to Helicopters
In a traditional mechanised offensive, armour and infantry fighting vehicles (IFVs) operate collectively to gain and hold ground. Helicopters are used forward to take out enemy armour and attack command posts while scouting and designating targets for precision artillery strikes.
Infantry also relies on helicopter support for air cover and casevac. Recently, drones have been used in kamikaze attacks on helicopters. Used in this way, drones could significantly hamper helicopter operations and severely affect infantry morale.
Both helicopters and ground vehicles now need to adopt design and protection / defensive measures cognisant of the drone threat. In this scenario, the twin tail rotors suggested on some Westland designs (admittedly for other purposes) could provide a degree of redundancy.
General Observations
As the earlier discussion shows, the systems are more important than the platform. Ideally, you want to be network-enabled (so that someone else sorts out the targets and satisfies the rules of engagement). Then you want a long-range fire-and-forget weapon system capable of defeating enemy countermeasures and with a tandem charge, warhead to deal with ERA. If the missile sensor can discriminate between target types, so much the better. If I were in a tank, I’d still be worried about drones – as I said in a briefing a dozen years ago.

Given the right network integration and the right weapons, you could inflict a deal of pain in a fairly basic helicopter while staying well out of the way of any air defence. You still have to protect yourself against chance encounters – partisans or special forces with shoulder-launched weapons, for example. This appears easier said than done.
Assuming conditions allow offensive aircraft operations, integrating western weapon systems such as Brimstone on suitable platforms, such as Frogfoot, could provide the ability to salvo fire against multiple targets. Its MMW radar seeker is supposed to support this capability, with the weapons themselves avoiding duplication of effort and allocating targets across the salvo (fire-and-forget en masse).

The capacity offered by a medium helicopter in this role could extend to area denial or countermobility operations. This type of platform might be used to deliver area denial or scatterable countermeasures (even mines, perhaps) to rapidly counter enemy armour. Missiles such as Brimstone might be more effectively employed in this scenario.
Whether in a defensive or offensive posture, an agile and responsive command and control system will be required to maintain a responsive decision-making process. This is known as the OODA-loop (OODA stands for observe, orient, decide, act). There is some question as to whether current NATO surveillance assets are providing near-real-time intelligence to Ukraine. It is clear, however, that long-range stand-off anti-armour operations will require a persistent (probably stealthy) high-flying or stand-off system to provide situation awareness, detect armour targets across the battlefield and enable the use of precision indirect fires (whether by artillery or helicopter, operations).
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One very good use case for low or zero sensors but good comms is to have airborne nodes in a ‘scrum half’ position behind the tactical edge. Anything up threat (exquisite and LO) can use directional comms to get data back / receive C2 and Intel from the nodes; the nodes then use any route to get to the optimal place – including space and terrestrial – from a position that cannot be easily targeted by OPFOR.
Urgent Operational Requirements manage rapid change during conflict, usually in response to painful lessons learned. This is generally at the subsystem/protection level rather than the system and platform level. Examples could be the rapid introduction of electronic countermeasures, protective screens, and responses to enemy countermeasures. The targeting infrastructure required to support helicopter indirect fire long-range attacks appears a little different from that required to support MLRS / HIMARS / ATACMS operations and should, therefore, be available, provided suitable tasking orders can be accommodated.
Interestingly, the available description of the Leonardo AW249 mentions the ability to operate air-launched RPVs. The latest Aerospace magazine indicates more on its network capability: “acts as a sensor ISR node on a C4 network, and (can) control and manage UAVs – with a Wide Band LOS Datalink … LTE Gateway and Link 16.” The articles do not address the routine concept of operations, but the connectivity and network capabilities could allow a range of collaborating systems to provide targeting data. Now they just need to adapt AW149 and/or NH90 TTH to the stand-off anti-armour role …”
Tentative Conclusions
There are many problems facing armoured units in modern land warfare. Broadly, these fall into
(1) threats: enemy armour, helicopters, armed drones, precision artillery and missiles, minefields and obstacles;
and (2) the difficulty of sustaining operations over time at long range: logistics – fuel, ammunition, repair, crew sustainment, rules of engagement.
Similarly, one can discuss the problems facing the counter-armour forces – again dependent on terrain/area of operations, posture, equipment and C4ISTAR systems and their connectivity.
Operational changes may arise under TTPs (Tactics, Techniques, and Procedures) rather than wholesale doctrinal revisions. The challenge is to inflict heavy casualties on enemy forces while increasing one’s own chances of survival.
Used carefully, existing attack helicopters operating over ‘friendly’ terrain can still be effective. Increased use of ‘network-enabled warfare’ seems essential, combined with the ability to engage targets primarily at range and preferably non-line-of-sight.

You might end up with some new operational concepts and the reprioritisation of target lists. Flooding of land to ‘canalise’ (literally and metaphorically) the routes available to armour (and logistics); out-of-contact launching and controlling of recce/designator / armed drones – and longer-range missiles from medium helicopters looks like a decent tactic for anti-armour operations and may have a place in both defensive and offensive postures.

Brimstone 2 (helicopter launched) has a stated range of 40 km+. As an operational concept, half a dozen AW149s (or NH90s, or Merlins, or Sea Kings), each with eight Brimstone 2, could do a lot of damage providing indirect fire—provided near real-time networked stand-off target information was available. In this role, the helicopter fleet operates as a highly mobile precision artillery force.
Exploitation of night capability and simultaneous attacks along a front might come into play. Deep strikes into enemy training and rear areas (and recruitment centres) might also be targeted to affect public opinion and morale.

Other options could include using dummy armour supported by signals deception activity to draw in enemy forces or distract from more covert operations.

Finally, it would appear that heavy armour forces do need organic close-in air defence. Perhaps the naval approach (e.g., Phalanx)—whether by high rate-of-fire radar-directed gun systems, electronic countermeasures (potentially including EMP to disrupt connectivity of control systems), or directed energy means—might go a good way to countering the ‘kamikaze drone’ threat. Target detection and tracking systems would have to be modified to suit the targets to be engaged.
The low cost and simplicity of the drones mean that they have a significant number of advantages, and identifying and then defeating drones once in the air is hard; their low profile and low signature are a challenge, and their agility makes physical defeat hard. This strongly favours electronic countermeasures might be the preferred approach.
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The discussion suggests that intelligence, communications, and the ability to counter enemy operations are becoming dominant factors in future land warfare. Land platforms and helicopters should now be designed, considering enemy drone operations as a key threat.
Equally, friendly drone operations – offensive, defensive, intelligence gathering, defence suppression, etc. —should be integrated into and with operational planning and land and air platform capabilities.
RV Smith
Dr Ron Smith joined the British helicopter company Westland in 1975, working in Research Aerodynamics, and remotely piloted helicopters (before they were cool), and later became Head of Future Projects. He had a strong influence on the design of the NH90 helicopter, and was involved in the assessment of the Apache for Britain. He also explored a variety of exotic future technologies for Westland. One such exotic machine was a secret stealth attack helicopter.
Credit is also due to John Puddy, Robert Hopkins, Jeremy Smith, and Jim Smith for the valuable insights they provided.

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We take class warfare to 300mph as we pit the aristocratic Mosquito against the no-nonsense proletariat muscle of the Beaufighter to find out who the real war-winning twin is.
A well-born beauty with two Merlins running on blueblood, the ecstatically swift Mosquito was the most refined fighter in the war. The Mosquito was stealthy enough to choose fights as it wished and had a reputation for invulnerability. Then there was the honest, almost thuggish, functionalism of the Beaufighter, which was all firepower and brute force – a design that seemingly believed streamlining was for cowards. The Beau carried enough ammunition to invade a small nation single-handedly and outgunned everything it faced with its multiple cannons and machine guns. But when push comes to shove, which was actually the war winner, the Mosquito or the Beaufighter? To determine the answer, we’ve developed some unimpeachable criteria based on actual operational usage. We then did a fucking ton of homework. Strap in!
ROUND 1: Timing
If World War II had started two years earlier, the Bristol Blenheim would have been legendary, and the Fairey Battle would still be remembered as shite.
In the crucial aspect of timing, the Beaufighter scores extraordinarily well. Its introduction coincided with the Luftwaffe switch to night bombing in early September, and it was there for the first Airborne Interception radar in the Autumn of 1940. Crucially, it also arrived late enough to avoid being squandered on the hopeless Battle of France or mis-deployed in the Battle of Britain, like its forerunner, the Bristol Blenheim.

The Beaufighter’s presence meant crucial lessons about night-fighter interception were learned in time to later defeat the Blitz in the Spring of 1941. Its contemporaries, such as the Blenheim, simply didn’t have the performance to keep up with German bombers, while the Boulton Paul Defiant was obsolete the moment AI radar was made to work. The perfect timing would play out with its introduction into the Mediterranean Theatre in 1941 and 1942, in time to make a decisive difference. The Beaufighter shone a harsh light on the shortcomings of its predecessors and would revolutionise aerial anti-shipping, as we’ll soon see.
However, the Mosquito was also well-timed, though somewhat later. Reaching squadrons in early 1942, its arrival as a light bomber coincided with Bomber Command’s building of a strategic air force. There was also a desperate need for a high-performance light bomber for target-marking when losses were soaring, and it was discovered that bombers were missing their targets by miles. Like the Beaufighter, it truly underscored where the RAF was going badly wrong, and had it been available one year earlier, the RAF might have avoided the idiocy of mass-escorted Stirlings, Hampdens and Blenheims on futile and wasteful Circus and Rhubarb raids (small-scale fighter sorties against ground targets of opportunity).

By the end of the war, both the Mosquito and Beafighter remained effective in what they were tasked to do (even if the Mosquito had some time earlier superseded the Beaufighter as the RAF’s main night fighter).
The Beaufighter edges it with perfect timing of its introduction at the inception of AI and the Luftwaffe’s switch to night bombing.
Beaufighter 1, Mosquito 0
8 MORE BLOODY ROUNDS TO COME…STAY TUNED!
Eddie Rippeth/Joe Coles
Eddie Rippeth is Head of Primary Publishing, International schools
Cambridge University Press

Last week, the KC-10 Extender, a superb aerial refuelling aircraft, retired. We spoke to a KC-10 pilot to learn about ‘Big Sexy’.
The best KC-10 was its versatility and the flexibility of its crews. Unlike the KC-135, the KC-10 was ready to refuel probe or drogue receivers without any extra work or attachments needed before launch. With the ability to be refuelled itself, the KC-10 could be launched and flexed to almost any refuelling mission quickly.
The worst thing about the KC-10 was taxiing it around on smaller airfields. The nosewheel sits 20+ feet behind the pilots, so you must be very careful about turning sharp corners or trying 180° turns. In these cases, we’d often have a boom operator open the forward doors, lay on their stomach & hang out of the aircraft; they were on the intercom, relaying the position of the main and nose wheels to the pilots, keeping us from crunching taxi lights or ending up in the grass (which we sometimes did anyway).
Based on overall capacity, the KC-10 was better than the KC-135; it could take off with a much higher fuel load. While it burned more per hour, there was still significantly more fuel available for receivers. The ‘135 also couldn’t do Drogue receivers unless the boom was modified ahead of time (which meant it couldn’t do probe receivers) or if you attached pods to the wings. The KC-10 was ready for either at any time (and we could put our own pods on the wings, if needed).

The empty weight of the KC-10 was about 250,000 lbs. Maximum takeoff weight was 590,000 lbs…so about 340,000 lbs of fuel, if you weren’t carrying cargo. All of it could be offloaded, other than what we needed to save to get ourselves home…and sometimes we pushed that limit! In one case, I pushed a little too far – we got back to our deployed base, and it was fogged in. We couldn’t even attempt an approach.
We were getting close to diverting, which would have been painful, but another KC-10 arrived. They took up a holding pattern over the base, a couple thousand feet above us. We started coordinating between ourselves to balance fuel out so nobody had to divert, then just did it. At one point, there were four of us in the pattern, talking to each other, and passing fuel so that everyone got to sleep in their own bunks. The fog eventually lifted, and we all made it in.

The KC-10 was actually pretty easy to take off and land. It was very stable and large, and bumps that would affect smaller jets didn’t have much impact on us. The controls were pretty straightforward. On landing, you’d start the process of “flaring†just after the 50’ radar altimeter callout.
You rarely landed smoothly, though, as the centre gear touched down first on crowned runways. It shook & rattled, so there was always some of that, except in the rare instance you’d land with the centre gear retracted.
There weren’t many foibles to the jet; it handled well. It was just very large. When refuelling with KC-135s years ago, the bow wave of a heavy KC-10 could hit a sensor in the 135’s tail, disconnecting their autopilot. If they weren’t watching it, you’d suddenly end up with a face-full of KC-135 as their autopilot kicked off and the nose dropped. They eventually fixed that problem, if I recall.
One peculiar aspect was that the number 2 engine in the tail was angled down at about 2.5°. We tried not to use it for taxiing, as we were already worried about blowing things over…some would limit how much they used it when air refuelling, too, as a big input could push the nose down.

Something you may not know about the KC-10: well, it had a large space under the cargo floor that was just empty. I think it was the galley on the DC-10, but the Air Force had no need. We called it “The Pool Roomâ€; I was told it was because you could put a pool table in there, and have room to play. Getting into it was a hassle.
You could access the KC-10 through the nose gear. We occasionally had to do that; you’d climb up & shimmy through the avionics compartment, eventually ending up in the cockpit. It was a tight fit!
The newer KC-46 is a decent aircraft. It’s had teething issues, but they will eventually sort it out. The problem is that losing the KC-10 still represents a major loss of overall capacity, as there will be less fuel in the air at any given time. The Air Force already can’t meet all its demand for Air Refueling, and I’m afraid that is much worse today.

My favourite aircraft to refuel was the B-1; it wasn’t particularly cool or anything, but when it showed up on your schedule in Afghanistan, they were going to take about 100k lbs of fuel…and your day just got a lot shorter!

My least favourite aircraft to refuel was the A-10. It doesn’t have the power of other jets and flies pretty slowly; we had to use slats and sometimes flaps to get slow enough. Above certain weights, it was just not possible.
The deck angle when refuelling A-10s could be in excess of 5° nose up…almost feels like you are setting up for a power-on stall. We had a procedure to help called a “Tobogganâ€â€¦we’d enter a slight descent at around 300 feet per minute. That gave the A-10 the help it needed to get on the boom, but you only had 1,000’ below you before you’d be outside of your protected airspace, so you’d only get 3 minutes or so. Then you’d have to climb up & do it again.
Nobody was necessarily bad at meeting the tanker, and we went out of our way to come to them. It didn’t always work, but we usually managed to end up 1-3 miles in front of them. Many fighter types referred to the KC-10 as the “mothership†because it was so large and was just there, in front of you.
Occasionally, the AWACs would control our rejoins. They didn’t seem to have much practice doing so; I can recall them vectoring us to our bomber, and vectoring the bomber to us…AWACs handed us off nose to nose at around 3 miles, closing at probably 600-700 knots. We were separated by 1,000’, so it wasn’t unsafe, but AWACs kind of said, “There you go,†and we immediately shot past each other in opposite directions. It was funny…we took over & directed a mutual turn on the same magnetic heading, which at least put us abeam each other & fixed it from there.
The KC-10 set the bar for tanker ops, hands down. As we discussed, the flexibility to do any Air Refueling mission at any time was key, and our ability to be refuelled meant we could be doing it for long hours.
We also had a significant cargo capacity. You could load up support troops and their equipment, then drag multiple fighters across an ocean. When you landed, you were almost your own little Air Force and could start operations quickly.
1A good tanker crew got to be a mini family. We didn’t use ranks in the KC-10 while flying, but rather, first names. We wanted every member of the crew to feel like they could speak up if they saw something wrong; everyone knew who the Aircraft Commander was, but that wasn’t something you wanted to flex on your crew – doing so may mean you win the battle, but you’re losing the war.

A good crew got to the point where they knew what everyone else needed, and they were ready before anyone asked. They understood the bigger picture, and took care of each other; you could complain, but my only rule was that the complaints better be funny because there wasn’t a lot we could do about most of it…it was better to laugh about it than to make each other miserable.
Big Sexy was the most common name, yes. Sometimes referred to as Gucci, but the official name was the Extender.
Three engines weren’t particularly unusual, no. The tail engine was exactly like the other two, but with a longer cowling. It was angled down slightly, though, as I mentioned.
If you had an engine failure (like we did in the simulator every quarter), you hoped it would be the tail engine. There was no asymmetrical thrust; the loss of one of the wing engines caused a lot of asymmetrical thrust, which required a lot of rudder to counteract.
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There’s a Hush-Kit Book of Warplanes Vol 1, and there will soon be a Vol 2 and then a Vol 3!
Thank you for reading the Hush-Kit site. It’s all been a massive labour of love to which I have devoted much time over the last 12 years. There are over 1100 free articles on Hush-Kit; think of the work that’s gone into that! To keep this going, consider donating (see button on top of page) or supporting on Patreon. Not having a sponsor or paid content keeps this free, unbiased (other than to the Whirlwind) and a lot naughtier. We can only do this with your support. I love this site and want it to keep going; this is where you come in.
To those who already support us I’d like to say a big thank you.
All the best, Hush-Kit


In 1943, the USAAF desperately needed an aircraft that could fly a vast distance, penetrate the Japanese Empire’s defence, outrun fighters, perform vital reconnaissance of the heartland and then fly back. This was a very tall order in 1943, even more so when the USAAF demanded a 400mph aeroplane capable of prolonged flight at 40,000 feet. This was the first time a reconnaissance aircraft was designed from scratch, not a converted fighter or bomber, but a modern dedicated camera platform incorporating all the latest technical advances. This was a new game, and manufacturers cock-blocked from the heavy aircraft market now stood a chance. Republic, creator of the incredible P-47, leapt the opportunity to compete for this potentially lucrative opportunity. The result was the superb Republic Rainbow, the most impressive piston-engine aircraft ever flown.

10. Empire of pane
Long before Concorde used its famous ‘droopsnoot’ to exchange high-speed aerodynamics for a better view for the pilot during landing, the Rainbow had a similar solution. Like the earlier the B-29, the Rainbow had a nose of curved glass panes. While B-29 crews loved the curved glazed nose for the unobstructed view in flight, and its low drag, they hated the fact it cast dangerously distracting reflections during landing. Designer Kartveli (the genius behind the P-47) was keen to avoid the B-29’s problem, and his solution was to make the curved sections of glass in the nose slide out of the way when not required, revealing a flat windscreen.
Shhh, here’s a secret link to the Hush-Kit Substack which has a load of very cool aviation articles.

9. Obscene speed
Very few piston-engined aircraft exceeded 450mph, even fewer could exceed 470mph. The only piston-engined aircraft (other than heavily modified racers) that have reached 470 mph were: the F4U-5, Ta 152H, Hornet, Do 335, P-47M, XP-82, Fury/Sea Fury, Spiteful, P-51H, XP-72 and XP-47J. The Rainbow is quite unlike the other aircraft, which are all fighters, and mostly single-engined radials. The Rainbow was the fastest four piston aircraft ever to fly.
8. Obsene Climbrate

The Rainbow’s astonishing climb rate of 5,000 feet per minute made it a better climber than most of the ultimate piston-engined fighters, including the Tigercat and even the Supermarine Spiteful.
7. Obscene Power

13,000 horsepower is a hell of a lot of power. To put this in perspective, the B-17 Flying Fortress had 4800 horsepower, meaning the Rainbow had 2.7 times more. The four-engined Rainbow had a superior power-to-weight ratio to the rival XF-11, boasting 0.128 to the XF-11’s 0.103. Like the rival Hughes XF-11, the XF-12 utilised the Pratt & Whitney R-4360 radial engine.
Instead of the usual two rows of nine cylinders like most large radial engines, the 4360 was unusual in having four rows of seven cylinders. Though this configuration presented cooling issues for the aft cylinders, it did bless the engine with a comparatively small frontal area for such a powerful engine.
6. Range

The second prototype flew coast-to-coast in the USA. The aircraft could fly more than 4,000 miles on internal fuel.
5. High altitude
The Rainbow could reach 40,000 feet, around 8,000 feet higher than the B-29. In tests it had exceeded 44,000 feet.
4. Extra power

The Rainbow featured a radical turbo supercharger arrangement, where spent exhaust gases were channelled through a narrow oval jet pipe, providing an extra 300 horsepower of power.
3. The flying darkroom

Much photographic intelligence is extremely time-sensitive. The Rainbow featured an onboard darkroom and intelligence specialists, meaning on landing, the aircraft had interpreted intelligence ready to be shared, a forerunner of today’s real-time data linking of visual footage.

2. Streamlining

Design leadership from Republic’s Alex Kartveli, creator of the superb P-47 Thunderbolt, emphasised streamlining almost unprecedentedly for the XF-12. The B-29 had redefined the modern aeroplane; the Rainbow, flying four years later, took many of these ideas even further. The attention to detail was incredible, producing what may have been the aerodynamically cleanest four-prop aircraft ever flown. Like the Mustang before it, it was an ultra ‘hygienic’ design. Every proturbence that could be eliminated, was, in a fanatical quest for the least drag.
As an example, cooling air for the oil coolers and intercoolers came from neat inlets in the wing leading edge. These were extremely efficient, and once used, the now heated air was routed through flush exhausts, angled backwards, at the underside of the nacelle, generating some handy extra horsepower.
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1. Civil options

An airliner variant, the 46-seat RC-2, was planned to kick open the civil market door. The RC-2 would have been a superb airliner, the best in its class and far superior to the offerings of Lockheed and Douglas. Unlike the Rainbow, the RC-2 was to have only one turbo-supercharger per nacelle (as opposed to two), making the heavier aircraft marginally slower. Despite this, it would still have been able to fly 3,450 miles at 400mph at 40,000 feet. American Airlines was the planned launch customer, with an initial order for twenty.
MiG-23MS, the worst MiG-23?

In Hush-Kit’s video (see end of article) on the 10 worst Soviet aircraft, the MiG-23MS was lambasted as a piece of shit. Today, I’m NOT going to complain about how crappy the MiG-23MS was. Instead, I will tell you two things which it did better than the MiG-23M and MiG-23MF.
1. Internal fuel capacity

The MiG-23MS had the largest internal fuel capacity of any MiG-23 fighter variant. Since it didn’t have the heavy and voluminous Sapfir-23D-III radar of the MiG-23M, a part of the avionics bay behind the cockpit could be used for more fuel. The extra space was used to install fuel tank â„– 1a, and tank â„– 1 was larger, same as on the MiG-23BN. This meant that the MiG-23MS had 5400 litres of usable internal fuel (again, same as on the MiG-23BN). Total internal fuel was 5626 litres. For comparison, the MiG-23M and MF had 4700 litres of usable internal fuel (4910-4928 L of total internal fuel). The MiG-23ML had an even smaller internal capacity, since it doesn’t have fuel tank â„– 4 either. Just 4300 L usable internal fuel volume, 4440-4458 L of total volume. The worst was the MiG-23UB, with 4240 L total internal fuel volume.

Note: if you want to calculate weights, standard Soviet fuel density at 15° C considered was 0.830 kg/L for the T-1 kerosene, and 0.785 kg/L for TS-1.
2: Empty aircraft weight

Since the MiG-23MS swapped the MiG-23M’s Sapfir-23D-III (or MiG-23MF’s Sapfir-23E) for the MiG-21’s RP-22SM “Jaybird” radar (just like the MiG-23S). This resulted in a noticeable weight reduction. I’ve never managed to find out how much an empty MiG-23MS weighs, but I can look at the radar weights and take a guess. The MiG-23M/MF radar weighs 564.5/641 kg. The MiG-21BIS radar (RP-22SMA) weighs 196.3 kg.

Now we can’t just subtract the difference between the two, because I don’t know if any ballast weight was necessary. If not, then that would mean at most 368.2/444.7 kg difference between the MS and M/MF. Considering also the lack of TP-23 IRST, my guess about 58 kg (that’s how much the TP-23M, изд. 26Ш1, of the MiG-23ML weighs).

So at most, a 426.2/502.7 kg weight difference, for reference an empty MiG-23M/MF should weigh about 10845-10890 kg. An empty MiG-23ML/MLD-export should weigh 10150 kg to 10230 kg (some give 10310 kg).

But can we find any confirmation for these from former MiG-23 pilots?
But can we find any confirmation from former MiG-23 pilots? The following pilot’s impressions are the only that I’ve found that confirm these features of the MiG-23MS:

Of course, none of this means to insinuate that the MiG-23MS was a good fighter. It had poor weapons (R-3S, R-3R & R-13M at best), structural problems limiting the maximum load factor, crude flight controls, poor roll-yaw stability at high AoA (all of these giving hard-wing Phantom levels of manoeuverability at best), bad visibility out of the cockpit… really, its only redeeming features were high speed & supersonic acceleration.

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