What determines what kind of weapons/items can be carried by a warplane's pylons?

According to Wikipedia (that always-reliable, never-error-prone website /s) and other sites, there is considerable lack of overlap between American warplane pylons (for instance, the F-18 Super Hornet can carry LRASM and AIM-174B on its pylons, but the F-16 cannot. At the same time, many warplanes carry AMRAAM, Sidewinder, Harpoon, etc.)

I’m assuming there must be some sort of common latching device that matches pylons in order for the weapon to fit properly on the hardpoint, and also that there must be compatible software for the pilot to be able to push a button and give the launch command. If some European warplanes can use American AMRAAM (but American jets can’t use European Meteor,) is it because they were fitted with American software?

Also, are there fuel-only “wet” pylons? It’s hard to picture how the same pylon that lets an airplane suck in wet fuel liquid through a drop tank could also be used to carry a missile on other missions (wouldn’t there be fuel getting into the electronics ports?)

I’m speculating a little bit here, but I suspect it’s more of a system integration sort of thing than a physical one.

For example, both the F/A-18F Super Hornet and the F-16C can both carry AGM-84 Harpoon missiles and GBU-27 Paveway III bombs. So they can both carry the same large missiles and large bombs.

The F/A-18F can carry LRASM and AIM-174B, but the F-16C can carry B-61 and B-83 nuclear bombs.

I suspect the physical connections are identical, but the avionics of the respective planes aren’t updated yet, from reading the Wikipedia articles on the planes, and this article about LRASM integration from Lockheed Martin.

LRASM Speeds Up 21st Century Security Solutions | Lockheed Martin

Might another factor be that some weapons systems are just too large for some planes? Either too heavy, or too low-hanging to fit below the wings?

Lotta things mixed together there.

Lemme try to untangle from the beginning …

Yes, there are standard latching and release arrangements for unpowered “dumb” bombs. In the era before airplanes had computers, by and large any airplane was physically capable of carrying any then-current bomb that wasn’t too heavy. Various pylons of various eras had different mechanical weight limitations.

But the ability to drop a dumb bomb usefully included the ability of the pilot to aim it. Every type and brand of bomb falls differently. So back in the day there were reams and reams of ballistics tables from which a crew would compute aiming settings then try to fly their airplane to match the settings then let the bombs go and hope for the best.

If the Brits and Americans or the USN and the USAAF did not have each other’s paperwork (and training) to do that computation they couldn’t usefully use each other’s bombs. Even if they did mechanically fit in each other’s racks. Which back in 1943 they probably did not, but NATO and DOD within NATO has been well standardized on that stuff since the late 1960s.

Once airplanes got smart with their own computers, now to usefully use a dumb bomb your airplane has to have the software module loaded that knows all about that model of bomb to compute an aiming solution. And the UI for the computer needs to have that model of bomb added to it’s list of possiblities. And the pilot needs to be qualified in all that. And the munitions manuals for the people who load them need to be updated and they have to have a bomb truck with a rack that fits the exact shape of the bomb to be able to carry it safely from bunker to planeside. Plus the people who maintain the bombs, assemble the bombs, store the bombs, inspect the bombs, etc. all need the tools and training and books to do that work.

There is far, far more to using a modern dumb gravity bomb on a modern smart airplane than “A fully assembled and fuzed bomb has magically appeared beside a parked jet. Do the hooks and latches fit?”


Once we move on from dumb bombs to either powered bombs or missiles, the complexity explodes. Now the computer on the airplane needs to know all about how to talk to the computer on the weapon. How to awaken it, query its status, tell it “get ready; you’re next”, tell it what to “look for” as a target, receive and understand status reports back from the weapon that everything is good (or not), and then finally tell it “Go get’ em.”

All of that is a big job with a lot of bureaucracy behind it.

So if you see that the F-18 can carry LRASM but F-16 can not, you can assume the issue is bureaucracy and lack of need, rather than some mechanical obstacle. For multi-national airplanes and national weapons it gets even more complicated by national security, national pride, etc. It is a major political whoop-di-doo for e.g. the USA to choose to update their F-[whatever]s to carry some British weapon instead of a competing German one.


As @Chronos said while I was still blathering, there are some exceptions to my general outline above. The e.g. F-15 can carry weapons heavier than the smaller F-16 can. The B-52 can carry weapons much heavier and larger than the F-15.

Nuclear weapons (not that you asked) are a whole different kettle of fish with very complex interface requirements and very detailed certification paths for a lot of specialized hardware that needs to be between the pilot’s release button and the bomb and the bomb rack.


Lastly, as to fuel pylons.

Any fighter / attack type aircraft have what are called “hard points”: the structural accommodations up inside the wings and fuselage to bear these heavy loads. Which also include munitions-related wiring carried to up inside the wing. On the skin surface there will be large female-threaded sockets to bolt the pylon up to. And a small access hatch to open to connect wiring plugs from the pylon to sockets in the aircraft interior. Similar umbilical connections are made to the weapon unless it’s a dumb bomb.

A fuel-capable hard point will also have a fuel pipe ending up inside the wing or fuselage structure and capped off. Which pipe leads downstream towards internal tanks and eventually the engine(s). These are often, but not always, also fully capable weapons hard points.

Typically pylons are installed on hard points and left attached there for months or years. Pylons are themselves a mix of standard connections and internal components for some things and being sized and shaped for the particular spot on the particular airplane they’re going to attach to.

For modern versatile fighters you may find an entire squadron of e.g. F-18s are equipped for long range patrol and ship attack with one configuration of fuel tanks and pylons while a different squadron dedicated to short range air defense of the ship have a different assortment of pylons and tanks. Either could be converted to the other config given a day and a dozen men, but easier to just draw from the sub-fleet that’s already properly configured for the mission.

Finally weapon adaptors and weapons are hung on the pylons on a daily basis for employment.

External fuel tanks in the modern era are generally carried on dedicated pylons that resemble munitions pylons but include the extra plumbing to connect to the tank proper. and of course there’s extra wiring to connect to the fuel gauge system and extra plumbing to also carry some kind of pressurized gas into the tank to help force the fuel out. That’s often bleed air taken from the engines or the HVAC system.

External fuel tankage back in WWII was sorta standardized within any one service, net of the major technological advances in just the 5-10 years the war lasted.

Nowadays external tanks tend to be highly optimized for the individual airplane with the right size, shape for aerodynamics, capacity etc. So while one might be able to physically bolt an F-15 external tank & pylon onto an F-16, you wouldn’t want to and it probably wouldn’t work.


Some concrete examples from the era I’m most familiar with. The classic F-16 as used by USAF has 9 hardpoints: numbered from left to right. The outermost (#s 1 & 9) are on the wingtips and can carry air to air missiles only. The centerline (#5) can carry a (singular) large or small bomb, a (singular) large fuel tank, or a large ECM pod.

The inboard wing pylons (#4 & #6) can each carry a smaller fuel tank or a variety of large or small bombs or additional multi-racks that can themselves carry multiple medium-or-smaller bombs or air to ground missiles. Or air to air missiles.

The mid-span wing pylons (#3 & #7) can carry the same as 4 & 6, except no fuel tanks.

The outermost pylons (#2 and #8) are physically different from those attachable to stations 3, 4, 6, & 7, and can carry either a singe air to air missile or a multi rack with a couple of small air to air missiles.

Great book-like response, thanks. Like reading Jane’s magazine!

An additional consideration is whether the weapon/tank/etc. is certified for the particular airplane, in that it has been tested to ensure that the specific aerodynamic conditions for that item on that location on that airplane will allow it to be cleanly released/fired without hitting any part of the airplane or the weapon’s trajectory and accuracy disrupted. That big fuel tank isn’t going to help much if, when you need to drop it in flight, the ass end flips up and takes out the horizontal stabilizer.

Or maybe that big fuel tank would be fine anyway… but nobody’s tested it to be sure, yet, and nobody wants to be the first to find out the hard way.

Yeah. There’s quite a process for that. Which is all part and parcel of developing the bureaucracy and tech data to eventually build the software to use the weapon or tank. Engineers can write all the CFD simulations they want, but someody has to go try it for real the first time.

Back in my USAF days there were a bunch of official training / information vids (U-Matic format. Remember those?) remade from old film movies of various drop tests gone awry. Scary shit.

I would not be surprised to find YouTube now has some of that stuff or other newer equivalent stuff out there for public consumption. I haven’t looked.

I expect that with the progress in math and computers, the engineers çircle of uncertainty is a lot smaller than it used to be. Such that the really hairy events are mostly 1960s and before, while the 1990s and after ought to be fairly calm viewing.


Beyond testing …
Shit can still get exciting with fully qualified modern ordnance if something hangs up mechanically, or right then the tail fins fall off one of the three bombs departing that side of the airplane or …

A clean safe release is sure the way to bet. But it comes with no guarantees. Which is why the weapons don’t arm until they’re a decent distance away from the aircraft. Unless somebody screwed that up too.

Yup: