X plane 10 north america
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Operational history ĥ1-9307 at the National Museum of the United States Air Force in Dayton, OhioĪt the time it entered service, the X-10 was one of the fastest turbojet-powered aircraft flown. Later X-10s included an N-6 inertial navigation system which completely controlled the vehicle through the cruise portion of the flight. Though the X-10 was receiving directional commands from a radio-command guidance system, these commands were sent through the on-board computer which implemented the commands. Thus, the X-10 is similar to modern military fighters which are flown by the onboard computer and not directly by the pilot. It also made the vehicle unstable requiring active computer flight control in the form of an autopilot. The combination of a delta wing with an all-moving canard gave it extremely good aerodynamics in the transonic and supersonic environments. The X-10 was powered by two Westinghouse J40 turbojet engines with afterburners, and equipped with landing gear for conventional take off and landing. The first flight occurred on 14 October 1953. Preliminary design of the X-10 was completed in February 1951 and the first vehicle was delivered to Edwards Air Force Base in May 1953. These included proving the basic aerodynamics to Mach 2, flight testing the inertial guidance unit and flight control avionics to the same speed, and validate the recovery system for the next phase in the Navaho program. This vehicle was to prove critical flight technology for the design of the Navaho cruise missile. To facilitate development of the long-range Navaho surface-to-surface cruise missile, North American Aviation (NAA) developed the RTV-A-5 (Research Test Vehicle, Air Force), or X-10 in 1951. The X-10 deployed a parachute to shorten its landing roll.