Shortround6
Major General
The A6M was NOT a light fighter. It was lighter than the F4F but is was the heaviest fighter the Japanese Navy was buying for the first few years of the war.
The Me-109 was NOT a light fighter when it was designed. It weighed close to what most other first line fighters did at the time. It worked "fine" as a short endurance interceptor in later years but was lacking in many of the capabilities of the P-38 and P-47.
" The F-16 worked just fine vs MiG23s and MiG25s" is a real hoot. Sure it did
the Mig 23 first flew in June of 1967 and went into service in 1970. The Mig 25 first flew in 1964 and went into service in 1970. The F-16 first flew in 1974 and went into service in 1978.
Want to tell me how well the F-16 did against the two Russian planes in the 8 years from 1970 to 1978??
And I suppose the Americans made absolutely NO ADVANCES on propulsion/electronics/aerodynamics/flight control in the years between the Russian planes being designed and the F-16 being designed?
you Know, like the engine in the F-16 weighing 3085lbs for about 15,000lbs thrust (dry) compared to the Mig-25s over 5000lb engines of about the same power*?
*Dry means no after burner in this case.
By the way, just how many Mig 25s did the F-16 shoot down?
The Me-109 was NOT a light fighter when it was designed. It weighed close to what most other first line fighters did at the time. It worked "fine" as a short endurance interceptor in later years but was lacking in many of the capabilities of the P-38 and P-47.
" The F-16 worked just fine vs MiG23s and MiG25s" is a real hoot. Sure it did
the Mig 23 first flew in June of 1967 and went into service in 1970. The Mig 25 first flew in 1964 and went into service in 1970. The F-16 first flew in 1974 and went into service in 1978.
Want to tell me how well the F-16 did against the two Russian planes in the 8 years from 1970 to 1978??
And I suppose the Americans made absolutely NO ADVANCES on propulsion/electronics/aerodynamics/flight control in the years between the Russian planes being designed and the F-16 being designed?
you Know, like the engine in the F-16 weighing 3085lbs for about 15,000lbs thrust (dry) compared to the Mig-25s over 5000lb engines of about the same power*?
*Dry means no after burner in this case.
By the way, just how many Mig 25s did the F-16 shoot down?