Interesting info from "Greg Goebel / In The Public Domain"
[1.0] Crusader In Development
The fact that the Crusader made considerable demands on pilot skill for safe operation suggested to some that a conversion trainer might be desireable, and so the 77th production F8U-1 was modified as a tandem two-seat trainer, with a new forward fuselage that lengthened the aircraft by 60 centimeters (2 feet). The rear seat was "stepped up" to give the flight instructor an outstanding forward view.
Two of the cannon were removed, as was the built-in rocket pack, but the ability to launch Sidewinders was retained. Avionics were updated to F-8E standard. As something of an experiment, the conversion was fitted for short-field landings, with low-pressure tires and a drag chute stowed at the base of the tailfin, allowing it to land in half the space of a conventional Crusader. The resulting "F8U-1T Twosader", as it was called, first flew in early 1962.
However, budget cuts in 1964 meant no US production orders for the type, and only one Twosader was ever built. The Twosader was then demonstrated in Europe. The British considered buying the type, with various improvements and equipped with a powerful Rolls-Royce Spey turbojet, with 53.5 kN (5,450 kgp / 12,000 lbf) dry thrust and 89.3 kN (9,100 kgp / 20,000 lbf) afterburning thrust. This would have resulted in significant improvements in performance and range, but the British opted for the Spey-powered Phantom instead.
[1.0] Crusader In Development
The fact that the Crusader made considerable demands on pilot skill for safe operation suggested to some that a conversion trainer might be desireable, and so the 77th production F8U-1 was modified as a tandem two-seat trainer, with a new forward fuselage that lengthened the aircraft by 60 centimeters (2 feet). The rear seat was "stepped up" to give the flight instructor an outstanding forward view.
Two of the cannon were removed, as was the built-in rocket pack, but the ability to launch Sidewinders was retained. Avionics were updated to F-8E standard. As something of an experiment, the conversion was fitted for short-field landings, with low-pressure tires and a drag chute stowed at the base of the tailfin, allowing it to land in half the space of a conventional Crusader. The resulting "F8U-1T Twosader", as it was called, first flew in early 1962.
However, budget cuts in 1964 meant no US production orders for the type, and only one Twosader was ever built. The Twosader was then demonstrated in Europe. The British considered buying the type, with various improvements and equipped with a powerful Rolls-Royce Spey turbojet, with 53.5 kN (5,450 kgp / 12,000 lbf) dry thrust and 89.3 kN (9,100 kgp / 20,000 lbf) afterburning thrust. This would have resulted in significant improvements in performance and range, but the British opted for the Spey-powered Phantom instead.