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The General Dynamics X-62 VISTA ("Variable Stability In-flight Simulator Test Aircraft")[2] is an experimental aircraft, derived from the F-16D Fighting Falcon, which was modified as a joint venture between General Dynamics and Calspan for use by the United States Air Force (USAF). Originally designated NF-16D, the aircraft was redesignated X-62A on 14 June 2021 as part of an upgrade to a Skyborg, with System for Autonomous Control of Simulation (SACS).[3]

X-62 VISTA
The General Dynamics VISTA/MATV NF-16D
Role	Experimental aircraft Type of aircraft
Manufacturer	General Dynamics (later Lockheed Martin) and Calspan
First flight	April 1992[1]
Primary user	United States Air Force
Number built	1
Developed from	General Dynamics F-16 Fighting Falcon

X-62A remains on the curriculum of the Air Force Test Pilot School as a practice aircraft for test pilots.[3]

Design and development

The NF-16D VISTA testbed aircraft incorporated a multi-axis thrust vectoring (MATV) engine nozzle that provides for more active control of the aircraft in a post-stall situation. As a result, the aircraft is supermaneuverable, retaining pitch and yaw control at angles of attack beyond which the traditional control surfaces cannot change attitude.^{[citation needed]}

The NF-16D VISTA is a Block 30 F-16D based on the airframe design of the Israeli Air Force version, which incorporates a dorsal fairing running the length of the fuselage aft of the canopy and a heavyweight landing gear derived from the Block 40 F-16C/D. The fairing houses most of the variable-stability equipment and test instrumentation. The heavyweight gear permits simulation of aircraft with higher landing sink rates than a standard F-16.^{[citation needed]}

The program was notable for the development of Direct Voice Input and the "Virtual HUD", which were both eventually to be incorporated into the cockpit design for the F-35 Lightning II.[4]

The VISTA aircraft is now operated by the U.S. Air Force Test Pilot School and maintained by Calspan at Edwards Air Force Base. It is regularly used in student curriculum sorties, special academic projects, and flight research.[3] As of 14 June 2021 VISTA is in the midst of upgrading. In addition to replacing the VISTA Simulation System (VSS) with a newer, upgraded version of the same system, a System for Autonomous Control of Simulation (SACS) will be added in order to operate X-62A as a Skyborg. One application is as autonomously piloted aircraft, perhaps as robotic wingman to a manned aircraft.[3]

Specifications

Data from USAF fact sheet[5] AerospaceWeb[6]

General characteristics

• Crew: 2 (pilot and safety pilot)[7]
• Length: 48 ft 7 in (14.8 m)
• Wingspan: 32 ft 2 in (9.8 m)
• Height: 15 ft 9 in (4.8 m)
• Wing area: 300 sq ft (28 m²)
• Airfoil: NACA 64A204 root and tip
• Empty weight: 18,238 lb (8,273 kg)
• Gross weight: 26,463 lb (12,003 kg)
• Max takeoff weight: 42,300 lb (19,187 kg)
• Powerplant: 1 × General Electric F110-GE-100 afterburning turbofan, 16,600 lbf (74 kN) thrust dry, 28,200 lbf (125 kN) with afterburner

Performance

• Maximum speed: 1,170 kn (1,350 mph, 2,170 km/h)
  

At sea level: Mach 1.2 (915 mph, 1,460 km/h)

At altitude: Mach 2+

• Ferry range: 2,800 nmi (3,200 mi, 5,200 km) with 3× 370 US gal (1,401 l) drop tanks
• Service ceiling: 50,000 ft (15,000 m) +
• Rate of climb: 50,000 ft/min (250 m/s)
• Wing loading: 88.2 lb/sq ft (431 kg/m²)
• Thrust/weight: 1.095

See also

Related development

• General Dynamics F-16 Fighting Falcon
• General Dynamics F-16XL

Aircraft of comparable role, configuration, and era

• Rockwell-MBB X-31

References

External links

• VISTA gets a new look

На других языках

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- [en] General Dynamics X-62 VISTA

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[fr] Lockheed Martin X-62

Le General Dynamics NF-16D/X-62 VISTA (pour « Variable stability In-flight Simulator Test Aircraft », signifiant « Avion de simulation et de tests en vol à stabilité variable »), également désigné F-16 MATV (pour « Multi-Axis Thrust-Vectoring », signifiant « poussée vectorielle multi-axiale »), était un avion expérimental américain, dérivé du F-16 Fighting Falcon et conçu pour l'US Air Force par une coentreprise entre General Dynamics — désormais Lockheed Martin — et Calspan (en) — un sous-traitant de General Dynamics — au début des années 1990.

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[it] General Dynamics F-16 VISTA

Il General Dynamics F-16 VISTA (Variable stability In-flight Simulator Test Aircraft) è stato un aereo sperimentale, costruito in un solo esemplare, derivato dall'F-16C/D Fighting Falcon e con il quale l'USAF ha condotto dal 1988 al 1997, una serie di programmi di sviluppo.

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