Rockwell-MBB X-31: Wikis

  
  

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X-31
The X-31 aircraft returns from a test flight for VECTOR.
Role Experimental
Manufacturer Rockwell
Messerschmitt-Bölkow-Blohm
First flight 1990
Primary users DARPA
NASA, DLR
Number built 2

The collaborative U.S.-German Rockwell-Messerschmitt-Bölkow-Blohm X-31 Enhanced Fighter Maneuverability program was designed to test fighter thrust vectoring technology. Thrust vectoring allows the X-31 to fly in a direction other than where the nose is pointing, resulting in significantly more maneuverability than most conventional fighters. An advanced flight control system provides controlled flight at high angles of attack where conventional aircraft would stall.

Contents

History

Two X-31s were built, with the first flying on October 11, 1990.[1] Over 500 test flights were carried out between 1990 and 1995. The X-31 featured fixed strakes along the aft fuselage, as well as a pair of movable computer-controlled canards to increase stability and maneuverability. There are no horizontal tail surfaces, only the vertical fin with rudder. Pitch and yaw are controlled by the three paddles directing the exhaust (thrust vectoring). Eventually, simulation tests on one of the X-31s showed that flight would have been stable had the plane been designed without the vertical fin, because the thrust-vectoring nozzle provided sufficient yaw and pitch control.

The X-31 showing its three thrust vectoring paddles.

During flight testing, the X-31 aircraft established several milestones. On November 6, 1992, the X-31 achieved controlled flight at a 70-degree angle of attack. On April 29, 1993, the second X-31 successfully executed a rapid minimum-radius, 180-degree turn using a post-stall maneuver, flying well beyond the aerodynamic limits of any conventional aircraft. This revolutionary maneuver has been called the "Herbst maneuver" after Dr. Wolfgang Herbst, an MBB employee and proponent of using post-stall flight in air-to-air combat.[2] Herbst was the designer of the Rockwell SNAKE, which formed the basis for the X-31.[3]

Front-side view of the X-31 in Oberschleißheim, Germany.

In the mid-1990s, the program began to revitalize and a $53 million VECTOR program was initiated capitalizing on this previous investment. VECTOR is a joint venture that includes the US Navy, Germany’s defense procurement agency BWB, Boeing's Phantom Works, and the European Aeronautic, Defense and Space Company in Ottobrunn, Germany. As the site for the flight testing, Naval Air Station Patuxent River in Maryland was chosen. From 2002 to 2003, the X-31 flew extremely short takeoff and landing approaches first on a virtual runway at 5,000 feet in the sky, to ensure that the Inertial Navigation System/Global Positioning System accurately guides the aircraft with the centimeter accuracy required for on the ground landings. The program then culminated in the first ever autonomous landing of a manned aircraft with high angle of attack (24 degree) and short landing. The technologies involved a differential GPS System based on pseudolite technology from Integrinautics and a miniaturized flush air data system from Nordmicro.

Serial numbers

  • BuNo 164584, 292 flights - Crashed January 19, 1995 north of Edwards AFB, CA. Crash was caused by ice inside the pitot tube, sending incorrect airspeed data to the flight control computers. Contributing factors included the replacement of a heated pitot tube with an unheated Kiel probe, and ground crew/pilot ignorance of an option to override computer control. The pilot ejected safely.[4][5][6]
  • BuNo 164585, 288 flights. Now on display at Oberschleißheim museum (part of Deutsches Museum).

Specifications (X-31)

Designed and constructed as a demonstrator aircraft by Rockwell International Corporation's North American Aircraft and Deutsche Aerospace, the X-31 had a wing span of 23.83 feet. The fuselage length was 43.33 feet.

The X-31 was powered by a single General Electric F404-GE-400 turbofan engine, producing 16,000 pounds of thrust in afterburner.

Typical takeoff weight of the X-31 was 16,100 pounds including 4,100 pounds of fuel.

The X-31 design speed was Mach 0.9 with an altitude capability of 40,000 feet. For specific tests to determine thrust vectoring effectiveness at supersonic speeds the aircraft was flown to Mach 1.28 at an altitude of 35,000 feet.

Orthographic projection of the Rockwell X-31.

General characteristics

Performance

See also

Comparable aircraft

Related lists

References

  1. ^ Dorr 1996, p.42.
  2. ^ Smith, R. E.; Dike, B. A.; Ravichandran, B.; El-Fallah, A.; Mehra, R. K. (2001) (PDF). Discovering Novel Fighter Combat Maneuvers in Simulation: Simulating Test Pilot Creativity. United States Air Force. http://www.cs.ucl.ac.uk/staff/Rob.Smith/PCES.pdf. Retrieved 2007-01-16.  
  3. ^ "Partners in Freedom: Rockwell-MBB X-31." Langevin, G. S.; Overbey, P. NASA Langley Research Center. October 17, 2003.
  4. ^ "The Crash of the X-31A". http://www.check-six.com/Crash_Sites/X-31_crash_site.htm. Retrieved 21 November 2008.  
  5. ^ Destroyed in Seconds, Discovery Channel, aired: 19 December 2008, 1:30 A.M. EST
  6. ^ "Loss of the X-31A". http://www.nasa.gov/centers/dryden/news/X-Press/stories/2004/013004/new_x31.html. Retrieved 10 August 2009.  

Gallery

External links








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