When you have missile on your tail, the engagement did go wrong in the first place. But I would rather have a missile on my tail in plane flying at 800 knots, then in one flying at 250 knots.
That is true, but besides that, two most impotant things you have to have for evading missile on your tail are high pitch rate and high AoA.
That means abrupt pitch maneuver.
The faster plane can dictate the engagement and choose when and where to attack. The higher speeds gives his missile an advantage. The faster plane stays a shorter time within the detection range of the Mk.1 Eyeball.
That is true, but why do you think that F-22 is faster than Mig-29 ?
It is faster only in dry power,in cruise.
In the battle zone, Mig-29 could engage reheat, with which it is much faster than F-22.
The cruise speed of F-22 is advantageous only before combat starts, trying to sneak to enemy aircraft.
But when Mig switch to max power, all F-22 speed advantage is gone.
Now why would some point the aircraft, if he has highly manouverable all-aspect, helemt mounted sight guided, IR missiles ??
.
Because, missiles are not allmighty. They are limited in flight time, engine burn time, max g, off-bore sight, etc.
When you read that some missile has 9 g capability, that doesn’t mean that it could be sustained. When engine stops, max g drops sharply, etc,etc.
For that reason, firing aircraft has to have good point and shot capability, to acquire firing solution faster.
When two missiles have similar off-boresight capability, the one which is launched at more favorable AoA will have a more effective range.
That is why, aircraft AoA is important.
Pure nonsense.
A regular Su-27 is limited to 27,5° AoA and becomes critical at 33° AoA.
A MiG-29A from the IAF for example is 26° AoA and becomes critical at ~30° AoA. For the MiG-29S with better stability augmentation you can add 2° to that AoA. For a few seconds a MiG-29 can be pushed behind that up to 45°, but with all the limitations of that in mind.
The last value becomes usuable with TVC support only. (see your MKI about that)
All values above 30° AoA are speed limited without TVC.
Looking inside a real MiG-29 cockpit. The artificial horizon instrument (KPP-1273SI)shows stepped markings up to 30° AoA and a single 45°AoA mark.
No, Sens.
The AoA you presented are not max possible in Mig-29/SU-27.
These are AoA to which automatic flight control system is designed.
The AFCS can hold the aircraft at these AoA.
Above these values, aircraft tends to recover itself, hands-off to low AoA.
Below these values, the pilot recovers the airplane to low AoA with stick.
Also, at these AoA, stick force is increased from 3 to 17 kg.
Aren’t you read reports of F-16,18 pilots about theirs experiences with Mig-29 ?
They all say they would like to have very high AoA capability of Mig-29.
The max AoA in Mig-29 is 90 degrees even with missiles.
Its point and shot capability is therefore extremely high.
Note also that pitch rate is closely related to AoA.
How was the F-4 a poorly designed fighter?
What do you call the R-73 then? A substitute for poor BVR avionics and weapons?
The F-4 has bad aerodynamics. It is very sensitive to departure above 20 degrees AoA, and has high wing loading and corner velocity, but that is another story.
The modern fighter must have a high pitch rate and AoA capability to point the weapons and shoot first. If you have high off-bore sight missiles, that is added benefit.
It is no wonder why German Mig-29 beats everything put against it within 20 km in NATO exercises. It is too dangerous.
got solid evidence to support your f/a-22 performance claim?
Of course, I have a solid evidence of all I said. It is not easy to find. Especially on google.
I will present that soon.
The Blackbird has been very dangerous design.
It has chines to reduce trim drag at high speeds, but on the other hand, chines also reduce longitudinal stability to such extant that flying was dangerous. The zoom climb is, because of that out of the question.
The variants before SR-71 were especially bad in that respect.
It is no wonder that enormous percentage crashed. About 40 %.
The Mig-25, on the contrary, has flying stability like every normal fighter, and can perform any fighter maneuver.
And with 4 enormous missiles can climb to more than 36 km, which is truly fantastic.
They did that at least seven times, by the way, three of them at OR OVER Mach 3.2. And the USAF-flown record flights were with equipment, albeit not missiles.
It is curious to me how YF-12 managed to fire missiles at 3,2 Mach when its max record speed was 3,13 Mach.
Note that YF-12 , used for record run, has been without unnecessary equipment. Every measure has been taken to reduce drag. Even IR sensors were deleted.
In their place, chine shape was restored.
Nevertheless, max speed could not exceed 3,13 Mach.
That is because, before SR-71, Blackbird could not possibly exceed 3,1 Mach in service.
It was unstable and dangerous at speeds above 3 Mach.
You could read various fantastic stories about it, such as:
-“ASG-18 has 500 miles detection range.”
-“YF-12 flying at 3,2 Mach, destroyed QB-47 drone with single missile from 120 miles. The AIR FORCE was extremely impressed.” (SR-71:-Crickmore)
-“The results were outstanding. The AIM-47 was able to hit targets at 140 miles away.” (Lockheed Blackbirds:-Thornborough,Davies)
These were all lies, intended to ensure production of YF-12.
The SR-71 was the fastest of the series because of better stability at high speeds.
Delta configurations are not good for a fighter. The aspect ratio is too small and it effects badly on sustained turn, climbing turn etc. The induced drag is too high.
Regarding F-22 versus SU-27/Mig-29, in close combat F-22 has no chance with 60 degrees max AoA.
SU-27, with its tremendous pitch rate (60 deg/sec), and 120 degrees AoA, will point and shoot with R-73, first.
SU-37 has unlimited, 360 degrees AoA.!!!
The F-22 ,with its 40 degrees max pitch rate and 60 degrees max AoA, has no chance to fire first, in close combat.
Its only chance is firing from the distance with AMRAAM, but that could do F-4 also, or any other bad designed fighter. The AMRAAM is substitute for a bad aerodynamics.
I’m still wondering how he managed to think the Red Baron Starfighter was equipped with the RCS of the NF-104 and the precompressor water/alcohol injection of SKYburner.
It is a matter of right information, not thinking.
Here’s something else you’re wrong on, what a suprise.
Greenamayer made three record-attempt flights in his F-104. The first two were going after the low-level world speed record. The third was when the aircraft was lost in an attempt at the altitude record.
Anyway, October 24, 1976: 988.26 MPH. Sageburner’s record fell, and the FAI did certify the record a short while later (the first attempt was apparently not certified thanks to a camera being screwed up).
I said, FAI did not recognised a new record. Check it. And his first attempt was in 1977 not 1976.
Of course it was 988. That’s never been in dispute (well not until you did anyway). If it was one-way then it wouldn’t have qualified for an FAI record. That doesn’t change the fact that it DID fly the course at 988 mph. And in this case all “home built” means is that a civilian assembled a REAL F-104.
It was not one way run, and it was disputed and not recognised for another reason.
http://members.chello.se/ipmsairrace/records.htm
Look there. Till 1953 “low-level” speed records were absolute speed-records, but than no longer.
That is true, regarding absolute speed records.
The attempts for absolute speed record after 1955 were at high altitudes (F-100C).
But, speed record attempts (not absolute) at sea level have never ended.
The F-104 RB attempted a sea level speed record, but record of F-4 proved hard to break.
“WINGS”, oct.1986:
“The Blackbird mission takes hours of preparations.” !!!
Aviation Week, 18.may.1981, Blackbird report:
” Engines must be started 40 minutes before take off.
The special engine oil, which is solid in normal temperatures, must be preheated before flight. It takes about 1 hour for every 10 degrees C of heating.”
It rendered Blackbird totaly unsuitable as interceptor, regarding alert time only. It was a maintenance nightmare.
On the other hand, The Mig-25 has alert time like every normal fighter.