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May 3 27 tweets 8 min read Read on X
In 1960, the Broad Jump program to upgrade the US Air Force's newest interceptor's radar, the F-106's MA-1 Automatic Weapon Control System, began. This would be a notable overhaul and improvement of the MA-1 system, giving it exceptional Electronic Protection capabilities. Image
The first systems added under Broad Jump were anti-chaff devices. One of these such devices was the leading/trailing edge range gate tracker. Normally a range gate operates as an evenly split gate, as described below. Image
A leading-edge range tracker sacrifices some range accuracy for electronic attack resistance. A trailing edge tracker works the same way, but in reverse. Image
In this case, though, the leading/trailing edge tracking options were primarily designed to allow for chaff resistance. Jamming returns were handled in other ways. Though this is an excerpt referring to the F-102's MG-10, it applies to MA-1 just the same.
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This passage also refers to range-rate memory, another part of the nose-tail computer that increased the stability of a radar lock and would help automatically re-lock the target once the target had stopped using expendable countermeasures, such as chaff and chaff rockets.
From what I can find, the nose-tail computer on the F-106 after Broad Jump was also capable of preventing range-gate pull-off attacks against advanced response(not repetition) jammers, though I'm honestly not sure how it was able to avoid them without manual nose-tail selection.
Now we get into the radar tune switch. This changed under Broad Jump(old switch shown later), and in this format, it took advantage of the next major modification: the hydraulically tunable magnetron. Image
As compared to previous Hughes tunable magnetrons which required the pilot to manually adjust the frequency, the new one had significant advantages in terms of frequency adjustment speed, allowing for computer-controlled modes.
The first was the "normal" mode. After Broad Jump, the jittered pulse repetition frequency (how much time between each emitted pulse) was augmented by pulse-to-pulse frequency shifts, making repetition jammers and most response jammers nigh useless against the Six.
F MIN and F MAX appear to be simple selections for the extreme ends of the magnetron's frequency range.
The final mode, SNIFF, is by far the most interesting. This took shape as early as late 1957, but would not enter service until Broad Jump in the early '60s. This, as described below, would tune the radar to avoid jamming frequencies. Image
At the same time as the tunable magnetron was installed, amplifier circuits were modified with new parametric amplifiers to lower the noise floor. This increased the search and detection range by about 30%, a huge upgrade in capability.
The next system was something called "Silent Lobing", or Lobe on Receive Only (LORO). Silent lobing is an interesting way to prevent angle deception jamming by inverting the "conical scan" pattern to the receiving antenna. Conical scan works like so: Image
When a target is properly centered, the amplitude change is zero between all bearings. Here, you can see the target is not centered.
Normally, the radar feedhorn (the white thing on a stick) moves in that pattern to create that conical scan. However, a jammer can track that pattern and respond at certain times to create a false position. (APQ-100 | APQ-109 with feedhorn spinning)
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This method is called inverse-gain deception jamming. A very good explanation of this can be found here: emsopedia.org/entries/invers…
There are two primary ways to handle IGDJ without a monopulse radar. In the case of AN/APQ-120 on the F-4E, it was done by constantly varying the feedhorn nutation rate. Image
Silent lobing (Lobe On Receive Only, LORO), the other method, is different. The feedhorn stays stationary and the receiver nutates to generate the conical scan pattern. This prevents a jammer from ever figuring out the scanning rate, making this type of angle jamming impossible. Image
Broad Jump furnished the MA-1 with this LORO system and four selectable "lobing frequencies"(essentially the same as different conical scan frequencies), to work around a Soviet jammer operator's potential attempts to guess the lobing frequency.
Unfortunately, I don't have any information on exactly how this worked. It's not clear from the antenna feedhorn design. On the upside, this system appears to have not been as vulnerable to a monopulse jamming technique called cross-polarization.
The MA-1 system had initially been fitted with something called MTI, or moving target indication. This was an unusual but ingenious version of MTI, designed to take out low-altitude bombers.
However, low-altitude bombers never materialized as a threat to the CONUS.
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Recognizing this as early as the early-60s, ADC moved to replace the MTI system with the much more relevant and effective Infrared Search and Track System, IRSTS. This was a very advanced system, drawing from experience developing IRSTs for the YF-12's AN/ASG-18. Image
The IRSTS, which deserves a thread of its own, provided two different options: independent scan and lock-on, if something had gone wrong with the radar or an intense form of jamming had prevented the radar from being used, and slaved mode.
In slaved mode, the radar would be slaved to the IR, allowing for radar lock-on to create a situation where IR and radar missiles could be fired. Image
There is some indication that this could go the other direction(radar-->IR), as well as some indication that this was a multi-sensor lock, preventing the tracking system from accepting error signals unless the IR and radar produced the same ones, but I have no sources for this.
Either way, the IRSTS was a huge upgrade in capability, allowing for much better handling of complex jamming environments and much more advanced electronic attack methods.
After Broad Jump and until the introduction of F-15 MSIP, I strongly believe that the F-106's MA-1 was the best airborne radar in US service when it came to dealing with the Soviet bomber threat. Its electronic protection measures were truly impressive for the time. Image

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More from @heatloss1986

May 1
A short thread on a poorly understood AIM-9 variant, the AIM-9B FGW.2, or in US nomenclature, AIM-9F. This was a German improvement program for the AIM-9B that entered service in 1969. (9F on the right) 🧵 Image
The 9F was a license-produced variant of the Sidewinder, designed to improve the seeker performance and reliability of the normal 9B. It did so in three ways: optical filtering, Carbon Dioxide cooling, and solid-state electronics.
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Apr 26
In 1943, the US Navy deployed their first single-seat night fighters. These were F6F-3 Hellcats, modified to carry the AN/APS-4 X-band airborne search and gunnery-aiding radar. It was rapidly replaced by the APS-6, an improved system. A short thread on the functions of APS-6. 🧵 Image
Sorry in advance for the poor scan quality. I cannot find a better copy of this document publicly available, nor any other documents that display the radar displays in different modes. I will use some screenshots from when the scan quality is too poor.ibiblio.org
AN/APS-6 was a surprisingly simple radar set, having no range tracking functions and only two scan patterns. However, it had three different display functions, all with unique purposes.
The best place to start is with the two scan patterns, both used for different functions.
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Apr 24
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
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Apr 21
F-8's radar controls: A short thread on why on earth the early F-8's radar controls were so bad. Image
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.


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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. Image
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Apr 18
"Why you can trust SCMP" You can't. This is mostly hot air.
A short, less-technical thread about this article. Image
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.
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