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Originally posted by Darce
reply to post by Tifozi
I can't find any info on Tomcats with USAF markings. They probably wanted to replace the F-4 with something that had a gun.
Oh well thread derailed. We'll see if anything comes of this incident.
Originally posted by Tifozi
reply to post by Darce
Actually no. The F-15 was rushed up in order to fulfill the gaps of the F-14, and to give an extra edge on the US military, even in the Navy.
I think they were designing the F-15N with a hook to land on carriers, but problems due to weight or design prevented them from using it.
That's why they reinforced it's role by using mid-air refueling.edit on 26/1/12 by Tifozi because: typo
Maneuverability
In order to avoid being forced to accept the FX specification then being developed by the USAF, the Navy insisted on an airplane uncompromised by the air superiority requirements. This was actually a code phrase which meant retaining the primary FADF capability of the relatively heavy Phoenix missile.
If the F-14 was created to shoot down bombers, and it was not optimized for maneuvering air combat as the primary design goal, it has even been suggested that the F-14's extraordinary maneuverability is due to the accident of a low approach speed requirement.
However, the Grumman design was able to create a design in which the FDAF and AS requirements did not significantly compromise each other.
The F-14 would use a wing sweep program to optimize lift and drag at all combat speeds, twin tails for stability, greatly reduced weight through extensive use of titanium to achieve a better thrust to weight ratio than the F-4, a pancake fuselage for increased lift, a raised tandem cockpit for reduced drag and increased visibility, a gun for close-in fighting, and widely spaced engines for weapons carriage and survivability.
Though as the first of a new generation of air superiority fighters, it would be criticized for not possessing the desired 1:1 combat thrust to weight ratio as was intended in the proposed upgraded F-14B and F-14C, it would prove to be competitive in training against a variety of competitors throughout its service life, especially at low speeds with a fully forward wing at full afterburner.
Originally posted by steppenwolf86
You really have no idea what you are talking about on many fronts. And even when you admit you are wrong, such as when you referred to the f-14 in the US Airforce, you laugh it off as if speaking in some general terminology.
The weight of an airplane has EVERYTHING to do with how it flies, because of thrust to weight ratio. If you do a search in google or on here for f-14 vs f-15 maneuverability you will find that I am correct in that the f-15 is a superior turning aircraft.
If you were simply willing to use google or the ATS search function and do a little reading, you will find that the people who look past the sentimental value and looks of an f-14 will admit that the f-15 was a better pure dogfighter. The Airforce plane was in fact superior in maneuverability to the Navy plane.
Sadly, it was put out of it's misery by another masterpiece of US air force, the F-15.
Of course, when I say Airforce, I mean that in a broad sense, and allow for no distinguishing between naval and air aviation wings, making statements such as THE F-15 REPLACED THE F-14 one hundred percent true.
Yikes, how can you take yourself seriously? Just admit your mistake, no need to be perfect.
Friendly advice if I may. I gather from your post that you are younger and passionate about the subject. It is a great topic.
You might want to think twice about calling other people idiots even when your information is correct, it is unnecessary and just turns people off from what you might have to say.
In this case, the conclusions you are drawing from the pedestrian information you have posted are both incorrect and show a superficial understanding of the subject.
I think (without researching or cheating on google) it had something to do with how the air flow affected the aircraft.
Contrary to your assertion that weight in a fighter makes no difference, I would beg to differ. Weight still makes a huge difference when it comes to maneuverability, regardless of thrust to weight and lift to drag ratio you still have to overcome inertia. The more something weighs the more force is needed to affect it, this was part of the design basis that the Light Weight Fighter program, otherwise known as the YF-16 and YF-17.
As the previous poster stated, variable geometry is heavy and complicated. It was an ambitious solution for the operational problems faced by its proponents 50 years ago, modern computerized flight systems have negated the advantages of variable geometry.
It was a beautiful craft, and very well made, apart from some "mistakes". People unknown to the aircraft must be aware of how complex that thing was, and how ahead of it's time it was.
The system did work, and it wasn't all that complex. Actually, it didn't have any problem besides the fact that it was too ahead of it's time. The wings weren't the problem, it was a genius idea. The problem was that the rest of the envolving tech in the plane wasn't all that clever to take the most of the design.
The F-14 is a formidable aircraft that did its job very well however declaring it to be superior to the F-15 at the F-15's own game is not a matter of opinion, it is incorrect.
Sadly, it was put out of it's misery by another masterpiece of US air force, the F-15.
The Navalised variant, F-15N-PHX was a study that was rejected nearly as soon as the ink dried. I don't understand your comment on mid air refueling? One of the FX requirements from the begining was the ability to aerial refuel.
Originally posted by steppenwolf86
You were the first to insult me. You called me an idiot, and made it personal long before I did.
But then, I am a fan of John Boyd. Also, to suggest that a problem is solved by not exceeding supersonic speed when the primary role of the aircraft is as an interceptor is laughable. However, since you stated that the f-15 replaced the f-14 in the US Airforce, I will take everything you say with a grain of salt.
Wikipedia is your friend.
And by the way, the fact that you don't even know how to elaborate a post quoting different people, only shows how mentally limited you are, and I take your tone as highly offensive.
Once again, instead of simply saying that you were wrong, you try to deflect blame. As another poster said, the next time you want to call someone an idiot, at least have the courtesy to get your facts straight.
Also, I did not derail the thread any more than you did. I merely responded to your posts, pointing out that your opinions, assumptions and conclusions were misguided at best.
I love how you try to play the I am not an american card. When you come into a thread and try to play expert, you open yourself up to people who will make sure your claims are based in fact. If your claims are based on mere opinion, and not backed up by reliable sources, it is your own fault for trying to play expert in the first place.
I think (without researching or cheating on google) it had something to do with how the air flow affected the aircraft.
Originally posted by steppenwolf86
reply to post by Tifozi
Fine, I am sorry for being arrogant. I admit I have little patience for being corrected when I am actually in the right on everything I said. I made the wikipedia comment because I genuinely hoped you would take a look at it. I have spent hours browsing the pages there for different air forces and planes, and I reccomend it once again since you are obviously interested in the topic.
Also, if you or anyone else is interested, I referred to John Boyd in passing. He was a Colonel in the US Airforce who helped change the way we design and evaluate fighter planes, and then warfare in general.
www.amazon.com...
My whole opinion on the f-14 changed when I was 17 and read this book. While it is a biography, it also explains topics from dogfighting strategy to the math that was developed to design the dominant planes that both you and I dream of flying.
2009 Iranian Air Force Ilyushin Il-76 accident
The 2009 Iranian Air Force Ilyushin IL-76MD accident of 22 September 2009 resulted in the destruction of Iran's only functional Airborne Warning and Control System (AWACS) aircraft, an Ilyushin IL-76MD.
Sources conflict on the cause of the loss, with some stating that there was a mid-air collision with an Iranian Air Force Northrop F-5E Tiger II or a HESA Saeqeh, and others stating that the rotodome detached from the aircraft, striking and removing the tailplane while the aircraft was manoeuvreing for an emergency landing following an engine fire.