The Ryan XV-5 Vertifan family comprised two initial XV-5A aircraft and the later XV-5B modification, developed with General Electric for the U.S. Army. Two J85 turbojets supplied gas to two wing lift fans and a smaller nose fan for pitch control. The XV-5A first flew in 1964 and validated the gas-driven fan-in-wing V/STOL concept, while exposing high pilot workload, a narrow conversion corridor, and abrupt pitch changes during transition. The modified XV-5B first flew in 1968 with wider-track landing gear, linked stabilizer and diverter-valve actuators, improved fuel management, and cockpit changes. NASA used it to study steep terminal approaches, powered-lift control, and aircraft noise.
Future launches and major activity directly linked to this vehicle family.
The Ryan XV-5 Vertifan family comprised two initial XV-5A aircraft and the later XV-5B modification, developed with General Electric for the U.S. Army. Two J85 turbojets supplied gas to two wing lift fans and a smaller nose fan for pitch control. The XV-5A first flew in 1964 and validated the gas-driven fan-in-wing V/STOL concept, while exposing high pilot workload, a narrow conversion corridor, and abrupt pitch changes during transition. The modified XV-5B first flew in 1968 with wider-track landing gear, linked stabilizer and diverter-valve actuators, improved fuel management, and cockpit changes. NASA used it to study steep terminal approaches, powered-lift control, and aircraft noise.
Future launches and major activity directly linked to this vehicle family.