Spitfrnd:
I simply don't understand the post just below mine that says you (i.e., Spitfrnd) have produced no data to show that the P80A was superior. Your post 37 has the data and notes that you have experience with one of the two aircraft in question.
Thank for pointing that out but what interesting is Spitfrnd has put the wrong spec down for the P-80A & the me 262
And no one is denying that the ME262 is a good aircraft; the issue is not whether the ME262 is good, the issue is whether the ME262 is better than the P80A.
Me 262 performance =
* Maximum speed: 900 km/h (559 mph)
* Range: 1,050 km (652 mi)
* Service ceiling: 11,450 m (37,565 ft)
* Rate of climb: 1,200 m/min (At max weight of 7,130 kg) (3,900 ft/min)
* Thrust/weight: 0.28
P-80-A Performance =
Maximum Speed: 558 mph (898 km/h) @ Sea Level
Maximum Speed: 492 mph (792 km/h) @ 40,000 ft (12,192 km)
Cruise Speed: 410 mph (660 km/h)
Climb: 5.5 minutes to 20,000 ft (6,096 km)
Climb: 4,580 ft (1,396 m) in 1 minute.
Service Ceiling: 45,000 ft (1
Range:
Normal: 780 mile
The USAAF compared the P-80 Shooting Star and Me 262 concluding, "Despite a difference in gross weight of nearly 907 kg (2,000 lb), 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 testing program proved very dangerous. Burcham was killed on 20 October 1944 while flying the third YP-80A produced, 44-83025. The "Gray Ghost" was lost on a test flight on 20 March 1945, although pilot Tony LeVier escaped. Newly promoted to chief engineering test pilot to replace Burcham, LeVier bailed out when one of the engine's turbine blades broke, causing structural failure in the airplane's tail. LeVier landed hard and broke his back, but returned to the test program after six months of recovery. Noted ace Major Richard Bong was also killed on an acceptance flight of a production P-80 in the United States on 6 August 1945. Both Burcham and Bong crashed as a result of main fuel pump failure. Burcham's death was the result of a failure to brief him on a newly installed emergency fuel pump backup system, but the investigation of Bong's crash found he had apparently forgotten to switch on the emergency fuel pump that could have prevented the accident. He bailed out when the aircraft rolled inverted but was too close to the ground for his parachute to deploy.
He bailed out when the aircraft rolled inverted but was too close to the ground for his parachute to deploy.
Operational history
The Shooting Star began to enter service in late 1944 with 12 pre-production YP-80A's one of which was destroyed in the accident that killed Burcham. A thirteenth YP-80A was modified to the only F-14 photo reconnaissance model and lost in a December crash), Four were sent to Europe for operational testing (two to England and two to the 1st Fighter Group at Lesina, Italy) but when test pilot Major Frederic Borsodi was killed in a crash caused by an engine fire on 28 January 1945, demonstrating YP-80A 44-83026 at RAF Burtonwood, the YP-80A was temporarily grounded. Because of the delay the Shooting Star saw no combat in World War II.
Shooting Stars first saw combat service in the Korean War, employing both the F-80C variant and RF-80 photo-recon variants. The first jet-versus-jet aircraft battle took place on 8 November 1950 in which an F-80 piloted by Lieutenant Russell J. Brown shot down a MiG-15.[7] Despite the initial success, the straight-wing F-80s were inferior in performance to the MiGs and were soon replaced in the air superiority role by the swept-wing F-86 Sabre