p-80 V Me 262

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"On February 28, 1945, the Luftwaffe High Command examined the various Emergency Fighter proposals and selected the Ta 183 to be developed and produced. Sixteen prototypes were to be built, allowing the tail unit to be interchanged between the Design II and III variations. Of the Versuchs (experimental test series) aircraft the Ta 183 V1-V3 were to be powered by the Jumo 004B turbojet, pending delivery of the He S 011 jet engine. The Ta 183 V4-V14 were 0-series preproduction aircraft and V15-V16 were to be static test aircraft. The first flight of the aircraft was projected for May 1945 but none were completed by April 8, 1945, when British troops captured the Focke-Wulf facilities."

Focke-Wulf Ta 183 - Wikipedia, the free encyclopedia

Focke Wulfe Fw Ta-183

Focke-Wulf Ta 183 Luft '46 entry

"On Febuary 27 and 28, 1945, the Emergency Fighter Competition conference was held by the OKL (High Command of the Luftwaffe), and the Ta 183 was chosen to be developed and produced. There were to be sixteen Versuchs (experimental test series) aircraft: the Ta 183 V1-V3 to be powered by the Jumo 004B turbojet, pending delivery of the He S 011 jet engine, the Ta 183 V4-V14 as 0-series preproduction aircraft and V15-V16 as static test aircraft. The maiden flight of the first aircraft was planned for May/June of 1945, and was to test both the Design II and Design III tail configuration. The first production aircraft were scheduled to be completed by October 1945, but no examples of the Ta 183 were completed because on April 8, 1945 British troops captured the Focke-Wulf facilities."

Thank you that is what every book in my library on the subject says as well. Sources are wrong though because someone else has read something different.

Ofcourse we all know as Morai so kindly put out for us that things dont work out that way.
 
Thank you that is what every book in my library on the subject says as well. Sources are wrong though because someone else has read something different.

Ofcourse we all know as Morai so kindly put out for us that things dont work out that way.

I have an issue here. My prime source has pictures of a Ju 287V-1 flying, both a Go 229V-3 and a P 1101 in build stages, but I have never seen any part of a Ta-183 that was built. I suspect it never really made it past the preliminary drawing and wind tunnel model stage. It took 6 mos. for Lockheed to design, build and fly the P-80, and that was using conventional aerodynamics, something the Ta-183 was advancing. I think it was a pipe dream to fly in May/June of 45. More probably, late 45, in early 46. And that doesn't mean that an effective warplane would have emerged.

Good move on closing down the Spiteful thread. It was very interesting on the discussion of high speed propeller flight. Then it went berserk!
 
You are more than right correct. The Ta-183 more than likely would not have flown in May/June 1945. The sources only say that it was scheduled to fly May/June 1945. This is when the Luftwaffe wanted it to fly. Would have, Could have, Should have....did not.
 
I think the p-80 had a little preformance advantage over the 262. The 2 engines of the 262 must have affected the roll rate and turn radius etc. The mk 108 was also pretty slow firing, and I think this is pretty crucial in a dog fight were planes go from one side to another in a split second.

On the other hand, the germans had allready used the 262 for 3/4 of a year when the first 2 p-80 came to europe, so german jet pilots had practised. They knew the strenghts and weaknesses of their jets in combat. The americans still had to learn this.

So I think that the first dogfights would have been won by the 262, but its pure guessing work.

Tom
I believe the 2 wing mounted engines would enhance aerobatics with a competent pilot by adjusting power on one engine . qoute from wiki about Janusz Żurakowski
." Acknowledged as one of the best aerobatic pilots in the UK, he gave a spectacular display at the Farnborough Air Show in June 1946, with the Martin-Baker MB 5, a superlative piston-engined fighter, designed too late to enter production.

In 1947, he was employed as an experimental pilot by Gloster Aircraft Company. In the following years, he became one of the world's most famous experimental and aerobatics pilots (he developed a new aerobatics maneuver, the "Zurabatic Cartwheel" which held the audience captivated as he suspended the Gloster Meteor G-7-1 prototype he was flying, in a vertical cartwheel at the 1951 Farnborough Air Show). Announcers shouted out, "Impossible!"
 
PB, youre forgetting that those early jet engines on the -262 flamed out due to them being extremely sensitive to quick throttle changes.

Differential thrust wouldnt work on the -262 because of this.

The 262 has the advantage in the top speed and probably dive speed.

P80 would have the roll rate advantage and superior endurance.

As for weapons.... I would say the 6 x .50's or even a pair of 20mm's would have the advantage over the 30mm's simply due to rate of fire and flatter trajectory.
 
PB, youre forgetting that those early jet engines on the -262 flamed out due to them being extremely sensitive to quick throttle changes.

Differential thrust wouldnt work on the -262 because of this.

QUOTE] I didn't say it wasn't going to be more interesting
aerobatics wasn't the 262's strength and I believe the P80 morphed into the T33 which was highly aerobatic
 
The 262 has the advantage in the top speed and probably dive speed.

I have seen this comment before and I don't know where it comes from. Every source I have seen shows the P-80A with a higher top speed than the Me-262. My main sources shows the P-80A capable of 558 mph and the Me-262A-1a with a top speed of 540 mph. Now, the P-80 speed is at s.l. and the Me-262 speed is at 19k, so there is no one to one comparison. However, the P-80 cannot be said to be slower than the Me-262.


As far as dive speed, I cannot argue as I have no data to support one way or another. I think the Me-262 may have had a better Mach limitation.
 
Differential thrust wouldnt work on the -262 because of this.
Any twin, jet or recip with engines slung under the wing will experience differental thrust and can actually be flown with varying throttle inputs. On a "production" -262 however I'd rather tame cobras than try it.
 
Any twin, jet or recip with engines slung under the wing will experience differental thrust and can actually be flown with varying throttle inputs. On a "production" -262 however I'd rather tame cobras than try it.

With 1944/45 vintage jet engines...... thats pushing the luck of the airplane and pilot to some degree!
 
The 262 was designed to take out bombers, it is not a dog fighter..

>maneuverable

They were shot down by 'top cover' P-51D's....

What is more revealing is the fact that Allied fighters did, in reality, shoot down Me262s in air-to-air combat. The speed advantage of the Me262 was routinely negated by American escort fighters by the simple method of a height advantage – they knew what height the Me262s would need to be at to attack the bombers, and judged it from that.


Plus they took forever to 'spool' up..

By the end of the war Germany was considering using Hitler youth as jet pilots. Nevermind they did not have the 'gas' to even train them. This is in a period when the standards of Luftwaffe pilots was in decline?

So give the P-80 8,000 feet and think about all those P-51's shoting down the Me-262

Answer..

Who is faster and who can fly higher and then you can call the winner..

alternative view

The Messerschmitt Me-262 Schwalbe / Sturmvogel

The Me-262s were then shipped to the US on the Royal Navy "jeep" carrier HMS REAPER for further evaluation at Wright Field in Ohio. The tests there included a competitive fly-off against a Lockheed P-80 Shooting Star jet fighter that demonstrated the general superiority of the Me-262.
 
Any twin, jet or recip with engines slung under the wing will experience differental thrust and can actually be flown with varying throttle inputs. On a "production" -262 however I'd rather tame cobras than try it.
Yeah I remember the P38 thread on that but just thought I'd hilight it with the Meteor tale. Also I think I'd prefer to be in the P80 with a flame out
 
Jackson said:
The Me-262s were then shipped to the US on the Royal Navy "jeep" carrier HMS REAPER for further evaluation at Wright Field in Ohio. The tests there included a competitive fly-off against a Lockheed P-80 Shooting Star jet fighter that demonstrated the general superiority of the Me-262.

A test report no one seems to have seen.
 
From the handbooks and such that I have.

262 would do 513 mph at sealevel and had a mach limit of .82 to .83 depending
on which data you look at.

FWIW
 
Jackson, the Me 262 was not designed to take out bombers. When it was designed (day) bombers were of little threat to the Germans. Now if you would have said the Me 262 was developed into a fighter to take out bombers...

And there is still a question as to how many Me 262 were actually shot down by Mustangs in air combat. The Russian I-16 also shot down the much faster but less manoeuvrable Bf 109...

Kris
 
disputes are to be expected..

The link I gave discusses German fears of the B-29 and it's rush into production.



// Me-262 s where shot down by the Russians also.


I read the book by the first guy to successfully fly the ME-163..

Which came out earlier than the Me-262..

He was later in Galland's Me-262 squadron.

The Me163 was really made to get up fast and attack bombers in a 'point' defense. Not many Allied fighters would have been over Germany for any reason but to escort heavies. (recon?)

I submit the Me-163 sole purpose was against to protect against bombers.

So, the concern was there..IMHO
 
The link I gave discusses German fears of the B-29 and it's rush into production.

Erich has some good info on that, but I think it will be a bit different than that link. Erichs info comes directly from the German archives.

We have some archives here in Nurnberg. I am going to see if I can check them out.
 
The tests there included a competitive fly-off against a Lockheed P-80 Shooting Star jet fighter that demonstrated the general superiority of the Me-262.


Not Really...

The test at Wright Paterson were run by legendary test pilot Al Boyd. The USAAF compared the P-80 and Me-262 concluding: "Despite a difference in gross weight of nearly 2,000 lb (907 kg), the Me 262 was superior to the P-80 in acceleration, speed and approximately the same in climb performance. The Me 262 apparently has a higher critical Mach number, from a drag standpoint, than any current Army Air Force fighter." The P-80 handled better and had better visibility.

The Army Air Force also tested an example of the Me 262A-1a/U3 (US flight evaluation serial FE-4012), an unarmed photo reconnaissance version, which was fitted with a fighter nose and given an overall smooth finish. It was used for performance comparisons against the P-80. During testing in May-August 1946, the aircraft completed eight flights spanning four hours and 40 minutes. Testing was discontinued after four engine changes were required during the course of the tests, culminating in two single-engine landings." There were NO combat maneuvers done aircraft vs. aircraft.

This is referenced in Walter J. Boyne's book Arrow to the Future. and from Winkipedia.

For what ever reason this information was suppressed for a number of years, perhaps not to embarrass US aircraft manufacturers. While the test showed some superiority aspect of the Me 262 I think the reliability factor comes in to play as well....
 
I was trying to give an alternative view..

The flavor of my own posts concure with yours..

But the clarity which you add to it is good.
 

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