FEOS wrote:
I was wondering if you were going to bring that up. Now you're looking at multi-role performance, not just dogfighting. You're changing the argument, and not in your favor. The F-4 was fucking exquisite as a bombing platform, particularly with the introduction of PGMs, since it had the backseater. In fact, the first use of the LGB was by the F-4 in Vietnam.
I know it is not in my favor, but the point is accuracy. Though I am not really changing the argument either, you are the one that implied I was only talking about its dogfighting ability because I was pointing out its flaws. No reason to mention something it did sufficiently.
Of course being a bombing platform isn't entirely difficult. You fly real fast, have the ability to be really heavy so you can carry lots of bombs, be able to be even heavier so you can carry two people instead of one...oh wait that's exactly what the Phantom does, at the expense of maneuverability.
FEOS wrote:
It didn't fly like a brick.
It looked like a fucking brick. With wings. And big engines.
Aesthetics =/= performance.
Learn the difference.
I do not care
at all about aesthetics. What I cannot possibly comprehend is the level of bullshit it takes to say aviators use the word "brick" to describe an ugly plane, not a plane with poor performance as it is used
here in the last sentence of the first paragraph. Can you give me
one other person that uses the term like that?
FEOS wrote:
OK. So it was "very communicative and easy to fly on the edge of its performance envelope" but "was subject to irrecoverable spins during aileron rolls" due to "adverse yaw during hard maneuvering". All of which the pilots would be trained to deal with when learning to fly and employ. And again, was not considered an issue
if you look at the original employment concept for the F-4 for which it was designed, which was to take on large bomber formations.Let's compare that to its primary adversary, the MiG-21:
wikipedia wrote:
Like many aircraft designed as interceptors, the MiG-21 had a short range. This was not helped by a design defect where the center of gravity shifted rearwards once two-thirds of the fuel had been used. This had the effect of making the plane uncontrollable, resulting in an endurance of only 45 minutes in clean condition. The issue of the short endurance and low fuel capacity of the MiG-21F, PF, PFM, S/SM and M/MF variants—though each had a somewhat greater fuel capacity than its predecessor—led to the development of the MT and SMT variants. These had a range increase of 250 km (155 mi) compared to the MiG-21SM, but at the cost of worsening all other performance figures (such as a lower service ceiling and slower time to altitude).[1]
The delta wing, while excellent for a fast-climbing interceptor, meant any form of turning combat led to a rapid loss of speed. However, the light loading of the aircraft could mean that a climb rate of 235 m/s (46,250 ft/min) was possible with a combat-loaded MiG-21bis,[1] not far short of the performance of the later F-16A. Given a skilled pilot and capable missiles, it could give a good account of itself against contemporary fighters.
The bolded part is why the F-4 was not a military engineering success. The role it was designed for was flawed, and made for severe miscalculations in the design requirements. The lack of an internal gun is just one example of such a flaw - that one was fairly easily rectified yes, but it demonstrates a mode of thinking that permeated the design of the airplane. It would be great if the primary use was for large bombing formations, with air to air encounters handled by tracking missiles that actually worked, but in practice those strengths were not as valuable as were first thought to be. The F-4 was essentially doomed from becoming anything more than sufficient from the start.
The failures of the F-4 have nothing to do with the failures of other aircraft. The aircraft was designed for a circumstance that didn't happen.
FEOS wrote:
Did you have something to say about wing loading? Because if you did, you must've forgotten to post it.
You asked what I meant by "...the obvious emphasis even from just looking at the chassis of thrust over wing surface area that would have let it be a solid fighter...". I meant wing loading.
(in standard because we aren't dirty commies)
Wing loading of F-4: 78 lb/ft²
Wing loading of MiG-19: 61.6 lb/ft²
A huge contribution to why the F-4 wasn't anywhere near as agile as it's MiG counterparts. The 21 was heavier than the 19...but that's exactly why a lot of their pilots preferred the 19.
FEOS wrote:
wikipedia wrote:
All in all, the Phantom set 16 world records. With the exception of Skyburner, all records were achieved in unmodified production aircraft. Five of the speed records remained unbeaten until the F-15 Eagle appeared in 1975.
Nope. I guess it didn't.
Ohhh wooooooow, it set 16 speed and altitude records. "That's a pretty impressive, kid" the SR-71 chuckles.
Seriously, Skunk Works made and introduced into service a fucking
Blackbird 4 years after the F-4 did the same. Two different aircraft to be sure. The engineers at Skunk Works still make the people that designed the F-4 look like retards.
FEOS wrote:
No, it's not. It's saying you want the plane that's best for the job. That's saying you want the F-15E over the F-22. And maybe you DO want the F-16 over the F-22 for a given mission. There are plenty that the Raptor is not suited to.
I'm not saying the F-4 is the kind of kings today. Never even implied it. It is clearly obsolete today. You, however, said it was shit then. That is where you are wrong and where our opinions clearly differ. And where the facts leave you far, far behind.
If being not nearly expensive/numerous/expendable is a mission, sure. Or does the Air Force officer want to provide an example?
What, so was it an amazing craft then? King of kings? My first response to you sums it up best:
Flaming_Maniac wrote:
Considering the amount of money we have dumped into defense spending during and after WWII, it would be a travesty if it wasn't [better than just about everything else, for it's time].
I'm just saying this wasn't exactly our finest moment in engineering.
---
FEOS wrote:
The Viper has less range, payload, avionics, one less crewmember to deal with the EW aspect, can't take the same amount of damage, isn't as fast...shall I continue?
Interesting that you--with all your aerospace engineering and aviation experience--think that. Perhaps you should submit a white paper or something.
Besides
FEOS wrote:
avionics
bullshit
The F-16 was designed to be a cheaper supplement to the Eagle yes?
FEOS wrote:
That's pretty much what I've been doing the last several days. And it's getting kind of old, tbh.
Don't you have a philosophy class to get to? Because I have a USAF squadron to go direct the operations of.
Oh yes your squadron of Phatom IIs...oh wait no we haven't used those in 20 years.
I know it's kind of like an unwritten rule that you have to give a reach-around to past and present military hardware, but just ignoring the flaws is a bit silly.
FEOS wrote:
Ever? Or during a given era?
The era of jet-powered flight. Judged against the scientific advances of the time (but
not necessarily against other craft of the time).