Heck no.Quote from Epic:
...I'm not by any means an aeronautical engineer, so I'm just curiously asking questions and making dumb observations. Let me know if I'm annoying you.![]()
Many of the latter model fighters have weight/thrust in the neighborhood of 1:1, AT fairly low weights.
But that's way beyond my means, not that it wouldn't be nice.
Using EAA spreadsheets my estimated takeoff run is 1,037 feet and 1,362 feet to clear a 50' obstacle. Landing distance should be about 1,049 feet or 1,957' if having to clear an obstacle near the end of the runway.
Using the same spreadsheet maximum rate of climb is estimated at around 2,600 FPM. Which is not bad, but using another slightly different method I've come up with estimates in excess of 4,000 FPM at lower weights (less fuel). Reality will probably be in between.
The airframe is stressed (assuming I haven't fucked it up) at + 9 and - 3 G's at 1850 LBS. I have spreadsheets for the wing and tail surfaces so I feel good about those numbers . I'm having to rely on self taught ability for the fuselage. Fortunately fuselage forces tend to be relatively light in comparison to the wings and tail.