Heatloss Profile picture
Apr 24, 2024 19 tweets 6 min read Read on X
The AIM-4, Pk, and Hit to Kill, or why the AIM-4 was, in my opinion, the deadliest air-to-air missile the US had in the '60s.

A short thread on why the hit-to-kill method employed by the AIM-4 Falcon was more effective than the influence fuzes of its contemporaries.🧵 Image
The best place to start is with missile development status in 1951. Thanks again to @MassiasThanos for finding this document (ADA8001650 p.158).
At the time, the relative effectiveness of various methods for warhead kill was unknown. As such, different methods were explored. Image
The Falcon was intended to exploit the advantages that its highly accurate guidance and autopilot system provided it. By ensuring a direct hit, the warhead could be much smaller (1/3-1/10 the size), performance could be higher, and front-aspect shots were more reliable. Image
This is not to say that the warheads of other missiles were not lethal. They were very dangerous to all sorts of different targets, both fighter and bomber, but the Falcon stood out, especially in regards to bomber interception.
Since I have no information on Sparrow III warhead effectiveness, I will be using Sparrow II data from CARDE instead, with continuous rod and blast-frag.
The CARDE assessment was a simulation designed to assess the performance of the AAM-N-3 Sparrow II against a TU-95 target. Image
Though this only gave rough estimates, it still proved that an expected radar missile shot against a heavy bomber was not very likely to result in a kill.
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The fears expressed in 1951 of fuze issues ended up coming true, though not in quite the same way.
The radar fuzes of early AIM-7s suffered significantly over Vietnam, even at higher altitudes. They would fail to detect the target, or detonate too early. Image
This trend of a lack of lethality continued with the Sidewinder. With more optimistic numbers, the AIM-9B's measly 25-pound warhead gave a catastrophic kill percentage of 30-40%.
The 9B's infrared influence fuze also suffered from severe issues and was rear-aspect only. Image
Why were these numbers so low? We go back to the methods that most warheads use to destroy or damage a target. Fragmentation. This means that pK is a dice roll. Due to miss distance and fragment distribution, there is a chance that none of the fragments will do any damage!
By lowering miss distance, you can ensure that more fragments will hit in a small area, increasing the point damage and the probability of damaging something important in that area, but it still does not ensure a kill.
The Falcon's accuracy allowed it to bring that miss-distance down to zero. By detonating 2.5-5 pounds of HBX explosive wherever it hit, it could ensure severe damage and increase the chances of bringing down a bomber.
This was for multiple reasons. The first was that of blast effects. The Mk 108 used by Germany in the Second World War was exceptionally effective.
The combination of blast and fragmentation, from only 3 ounces(!) of PETN explosive, could nearly cut a Bristol Blenheim in half. Image
The second reason was the semi-penetrating effect of the AIM-4.
The Falcon's wing-mounted contact fuzes were placed behind the warhead. This means that, like a timed fuze for a cannon shell, the AIM-4's warhead would penetrate the aircraft's skin before detonating. Image
This effect was noted even before the development of the Falcon, with the extremely high effectiveness of the Folding Fin Aerial Rocket in bomber interception. Even a single hit could bring down a heavy bomber. Image
This also brings us back to the first document, which mentions the low weight of the Falcon allowing the carriage of multiple missiles.
Falcons were designed to be launched in a salvo. Two or three for the early Falcons, and two for the late Super Falcons. Image
As such, Pk assessments were extremely high for the Falcon family. The Super Falcon, when employed against bombers, was expected to far outperform any of the influence-fuze-based missiles.
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Unfortunately, I've struggled to find a study for the AIM-4 comparable to the CARDE assessment of the Sparrow II, so like-for-like will have to wait until I can get my hands on test documents.
With the death of the AIM-4 program and the exaggerated issues with hit-to-kill against maneuvering targets, this method of bringing down targets was abandoned.
As higher missile maneuverability becomes possible, especially through bank-to-turn guidance, I believe we may see a return to hit-to-kill missiles for air-to-air. Their reliability and weight savings may prove a significant draw over even advanced blast-frag warheads.

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More from @heatloss1986

Mar 8
For years, I've been working towards building a website to house all of my opinions and research. Today, it goes live with the launch article: Jet Fighter Generations Aren't Real.

This website comes with a major change in how I produce and share content, so please read. 🧵Image
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First, here's a link to the article. I would have put it in the tweet above, but this website hates external links, and so it wouldn't have been shown to many of you.
For this reason (among others), I politely ask you to spread the word about this website.greatdefensesite.org/articles/fight…
X has unfortunately limited the topics I can present, the formats I can present them in, and the wording I can use to make a point. This website, for all its claims of free speech, has countless filters and algorithm features that harm post visibility. I'm tired of that.
Read 9 tweets
Feb 14
I think I've found my least favorite Sidewinder variant. From everything I can tell, it's a perfectly serviceable heat-seeking Air to Air missile with decent capabilities. But I hate it.

This is the Republic of China's Tien Chen-1 (天劍一).
🧵 Image
The TC-1 was the ROC's first attempt at an indigenous air-to-air missile. From what I can tell, it appears to be slightly better than the AIM-9P-5, which is a great showing, but again, I hate it. Image
To explain why I hate a missile that looks like an AIM-9L, we have to take a few steps back. When the AIM-9D was developed as a follow-on improvement to the AIM-9B, the Sidewinder went through a major redesign. Image
Read 21 tweets
Jan 10
During the development of the Tomahawk Cruise missile, an airfield attack version was proposed.
This was to utilize runway-cratering submunitions as an alternative to manned missions or nuclear strikes to disable a Soviet airfield in a war.
This was MRASM BKEP, or AGM-109H.
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MRASM BKEP was a sub-variant of MRASM, which itself was a subvariant of Tomahawk. AGM-109H (Photo 4) should also be distinguished from the AGM-109 variant proposed to compete with the Boeing AGM-86 (Photo 3) and the shorter tactical AGM-109L (Photo 2). Image
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MRASM as a concept started life in the late 1970s, as a joint program between the USAF and USN. It was mostly ignored until 1980, when Boeing won the Air Launched Cruise Missile competition with the AGM-86. Though AGM-86 was better for the role, AGM-109 offered unique advantages. Image
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Read 17 tweets
Jan 5
AAM-N-3 started life sometime in the early 1950s as a replacement for the beam-riding AAM-N-2 Sparrow I, which proved to be wholly inadequate. It featured an aerodynamic redesign and an active radar homing seeker.
Sparrow II was the odd one out.🧵
[Thread update] Image
Developed by Sperry-Douglas, like the first one, the second Sparrow was primarily intended to provide a better guidance system to allow for successful intercepts of maneuvering targets, or from other angles besides directly ahead or astern of the target.
A secondary goal was the higher survivability that Sparrow II would offer to the launching aircraft, as it did not have to maintain a target lock to guide the missile.
In bomber interception, this meant that the pilot could turn away long before he entered cannon turret range. Image
Read 29 tweets
Jan 4
In the dawn of the air-to-air missile, aircraft, radars and fire control systems were tied together. This allowed for optimization of the airframe to the missile and the missile to the fire control system. As this method of design has died out, the advantages have also been lost. Image
After the success of the AIM-7, and the expansion of AIM-7 carriage from F-3B to F-4 to F-15 and F-16, AAM development has become largely uncoupled from airframe and fire control radar development. This has been mostly a positive, but there are some negative aspects as well. Image
AMRAAM's original design focused on providing an active AIM-7 replacement with a higher F-pole range with the technology of the early 1980s. This meant that AMRAAM would reach a target at a given range FASTER than AIM-7.
This meant a 7" airframe and the same length as AIM-7. Image
Read 8 tweets
Dec 31, 2024
I often complain that USAF procurement has a history of choosing a cheaper product rather than a better product.
The Philco-Ford AIM-9E is a case study in how a price tag can influence the USAF. From the reports I can find, 9E was worse than the 9B.
A short🧵 Image
Though the development history of the AIM-9E is somewhat murky, we have some information.
The USAF liked the low cost of the AIM-9B, and the much higher cost and somewhat protracted development of the Navy's advanced nitrogen-cooled AIM-9D frustrated the USAF.
As the war in Vietnam began to ramp up, AIM-9B stocks began to diminish as pilots expended them in combat.
As a response, the USAF reached out to Philco-Ford, the current primary producer of the AIM-9, to see if they could produce a version of the 9D more similar to the 9B.
Read 21 tweets

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