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.🧵
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
• • •
Missing some Tweet in this thread? You can try to
force a refresh
F-8's radar controls: A short thread on why on earth the early F-8's radar controls were so bad.
Our story actually starts with the F2H-3, the night fighter version of the F2H. In the F2H-3, the radar was controlled by a joystick and a range thumbwheel.
At this time, radars required high pilot workload. Scope gain was controlled manually, there was no search antenna stabilization, and acquisition had to be done manually by pointing the antenna at the target and placing the range gate over the target.
"Why you can trust SCMP" You can't. This is mostly hot air.
A short, less-technical thread about this article.
The first problem is that I cannot find a study that matches this description and date. I did look, but I came up empty-handed.
Xie Junwei, though, is a real person who does relevant research at "Air and Missile Defense College, Air Force Engineering University".
This is the big claim. This isn't a new thing, radar cross-sections change based on wavelength. Most fighters are optimized for X-band stealth (or other frequency bands around it), as those bands are the most relevant in fighter and missile radars.
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, more importantly, an active radar homing seeker.
Sparrow II: the odd one out. 🧵
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 head or side on.
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. This was very forward-thinking, and would not be properly reconsidered until AIMVAL in the 1970s.
It's about time I re-did my AIM-4 thread on this account. The AIM-4 family, despite their poor reputation, were, in reality, very advanced missiles, despite starting life as the U.S.A.F's first operational air-to-air self-guided missile (it's also my favorite missile family).🧵
There are three major varieties of AIM-4. First, the GAR-1, the first airframe design, the GAR-1C, the second airframe design, and the GAR-3/4, the third major revision to the design. These all were designed to serve on different interceptors. (GAR-1/-1D/-3A&-4A)
Within all of these different versions, there was always a radar-guided and an infrared-guided version. The purpose of this was to improve the probability of a successful interception against a target that was either jamming or dropping flares.
HAVE DASH II, AARGM-ER, and the future of American long-range air-to-air missiles:
This is going to be an unusual thread for me, completely based on speculation and some basic knowledge about the direction of experimental programs and the goals of JATM.
AARGM-ER pictured.
This is a topic I've been giving some limited thought to for a very long time, but only recently formed an opinion on. The short version is that I think JATM will use a similar airframe to AARGM-ER, with some optimizations for maneuverability.
The first place to start is with HAVE DASH, a program to develop a low-observable missile in the 90s for use on future low-observable fighters.
Okay, well, I can't come up with any good ideas for an April Fools bit so you get a thread of some of my favorite bad/questionable missiles/missile ideas. Will update it as the day goes on if I can think of any I missed.
FIRST ONE:
Diamondback. This was described in literature as a "Nuclear Sidewinder". This is a bit silly, as it shared nothing with the real Sidewinder. 12" in diameter, it packed a nuclear warhead, likely W54 derived, with a 750t TNT equivalent yield.
I can't find much about the radar homing, but the IR was cooled and likely completely unlike that of the current Sidewinder.