On the topic of day fighters, one of the more misunderstood day fighters is the F-104. However, it suffered from many issues of light/day fighters of the era.🧵
The concept of the F-104 came from an unusual place--pilot opinions. Kelly Johnson interviewed pilots in the Korean War on what they wanted from a new fighter.
The answers were almost unanimous. Fast, simple, maneuverable, and with good high-altitude performance.
The F-104 was the answer to that call. It was an air superiority fighter, first and foremost. It was lightweight, incredibly fast, responsive for the time, and nearly untouchable above mach.
In a way, this was the 1950s predecessor to the LWF concept.
And, when I say light, I mean it. The Starfighter was nearly a ton LIGHTER than the F-16A. The engine alone weighed almost a third of the empty aircraft!
One of the design goals throughout the 104's development was the minimization of drag to increase performance. The narrow, small, and very fine wings are a representation of that.
Another issue that Korean War pilots fought was the aerodynamics of their own aircraft. Early fighter jets were not well equipped to handle the transonic region and suffered all sorts of odd and hard-to-control effects. @BaA43A3aHY can probably explain these better than I.
The 104's very thin wings helped prevent these issues.
But the 104's wings weren't designed for just low drag. They were designed to give optimum maneuver performance across the range of expected combat speeds. The same was true of the high T-tail.
And now a few snippets that describe thrust-drag as it relates to the Starfighter, and an acceleration chart of the 104C.
Yes, that is 4 minutes from Mach 0.9 to Mach 2.0 at 35,000 feet.
The acceleration at lower altitudes was even more extreme, though no charts exist.
And now, turn performance. While I cannot find any information in manuals on lower altitude turns, from what I've read, it still performs well, though you should probably try to keep any fights at 10,000 feet or above.
Above Mach, though, the F-104 was one of, if not the most, maneuverable fighter in US service until the F-15.
Some of the emphasis on the dogfighter nature of the F-104 can be seen in the design of the early 104's fire control system: its main goal was to lead the pilot into visual range of the target through a simple and easy-to-understand radar.
The 104C even contained an advanced optical sight to aid in target engagement by ensuring the pilot knows when he is "in range".
There were a few small aerodynamic problems with the 104, such as the low-speed performance and the inertial coupling, which could destroy the plane if the control limiters were not operating. However, I know of no losses to internal coupling related issues.
Now, we get into some of the problems. The first one that everyone points to is the ejection seat. The choice to go with a downward firing seat was novel and in many ways designed to protect the pilot as much as possible.
In a combat ejection scenario, which was when the seat was expected to be used, the ejection seats of the mid-1950s would not throw the pilot clear of the looming T-tail of the F-104. The only thing that pilots would have to train to do is remember to roll when at low altitudes.
Once seats had been improved, though, it was also better understood that ejections were very rare at speed and altitude, and that an upward-firing ejection seat would be more than adequate for the F-104.
The biggest issue that the F-104 faced was the eternal problem of the day fighter. Without longer-range missiles, a powerful radar, and with a limited payload of what missiles it could carry, it quickly became less relevant as the wonderful air superiority fighter it was born as.
It was, however, still an incredibly stable, simple and durable mach 2 capable airframe. The F-104G that would go on to serve in the Air Forces of many nations expanded on this capability, turning this high-speed dogfighter into a lightweight, multi-role fighter-bomber.
Given this, it should come as little surprise that four of the European nations that operated F-104s, Netherlands, Belgium, Denmark, and Norway, signed on to purchase the F-16. Like the 104, it was easy to produce and maintain at home and was a very capable multirole day fighter.
There are many other topics I could cover on the 104, including poor training in many countries, loss rate as a statistic versus accidents/100,000 flight hours, and more. I've promised a friend that I'd let him write an article on 104 safety on my website, so we'll have to wait.
In the next few days, though, I should be receiving an uncommon F-104G manual that details the weapons systems and the radar. I think we'll go over it when I have some time to sit down and digest it.
Until then,
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Someone asked me to do a comparison of capabilities between F-35A and JAS-39E Gripen. A ton of material is classified but I will do my best here.
In short, Gripen is not even in the same class as F-35A. It isn't awful, but it is not a competitor with F-35.
Let's start with one of the greatest advantages of the Gripen: its electronic warfare systems. The Gripen has a relatively robust signal receiver network across the aircraft, with several antennas capable of electronic attack, such as the wingtip pods and external jammers.
The Gripen's wingtip pods provide an uncommon capability called "crosseye jamming." Crosseye jamming can create a positional false target in the horizontal or vertical plane, rather than just range.
If you want to try to optically track a target with damn near zero contrast, be my guest.
The Japanese Navy found that at night the human eye struggled to pick up ships over about five miles. A ship on the horizon is a significantly bigger target than a B-2 or F-117.
For a computer, greater signal to noise ratios are required to effectively track a target. This is why imaging infrared is preferable to optical contrast. Shown below is the last few seconds of flight of an AIM-9X.
This uses imaging infrared to detect and track the target.
Since the end of the Cold War in 1991, the US Navy's ability to conduct air superiority and offensive strikes has been slowly diminishing. Today, we stand at an inflection point, where the F/A-XX program to deliver a new strike fighter to the Navy is in Jeopardy.
🧵
This thread is a pitch for a congressional write-in campaign. The first part is a history of the degradation of the Navy's air wing. The second part is an analysis of a recent oversight hearing. The last post of this thread contains instructions for emailing your representatives.
In the 1980s, the A-6F was proposed for development. This was to be an updated A-6E including modern avionics, new engines, and AMRAAM. This would have provided the Navy with a relatively low cost program, retaining a two-seat crew with a large payload and good mission systems.
Some very interesting stuff going on here with the Shenyang aircraft. 🧵
Exhaust appears visually similar to the F-22's with 2D thrust vectoring and shrouding. Wing shaping is nothing particularly special but seems good. Like JH-36, it retains some conventional control surfaces.
The all moving wingtips are a novel solution. I don't know what the trade offs are but they must be at least somewhat worth it. Potentially these are considered lower risk, higher strength, or more effective than the semi-morphing control surfaces on the JH-36.
The intake design is interesting. Unlike JH-36, which uses caret intakes underneath and uses a DSI above, the Shenyang aircraft uses what appears to be two DSIs below. The gear appears to fold sideways into a bay ABOVE the side bays, giving it a J-20-esque four bay arrangement.
With the renewed interest in the Europa wars, this may be the best time to bring up the unusual short ranged missile developed for space-superiority craft.
The AIM-95E "Europa Agile," the only missile designed for operation in deep space AND within thin atmospheres.🧵
First off, I apologize in advance for the lack of photos on this topic. All existing photos of Agile are of the ones designed in the 1970s for operation within Earth's atmosphere. Therefore, you will have to imagine some of these changes to the system.
The Agile for aerial use was cancelled in the mid 1970s after about $50m was wasted developing several different airframes and seekers. This spelled the end for the program as most know it, but this would only be the starting point for the Europa Agile.
For my entire life I have been taught about the importance of effective searches. Since May 2024, I have fought with an unwanted feature that has made my experience worse.
A rant about "AI Overview," AI assisted search and their impact on using Google as a tool for research.🧵
Google has billed these features as "taking the legwork out of searching" and "able to answer complex questions." This is a bald faced lie.
The AI has wasted more time than it has saved me, lied about results, and forced me to learn methods to get around it rather than to use it.
I do a lot of research using keywords that I need matched exactly. For example, right now, I was looking up the specific thrust of the General Electric F414 engine used in the X-59, an experimental plane in development for NASA. This should be a simple question to answer.