NASA X-43 - Development

Development

The initial version, the X-43A, was designed to operate at speeds greater than Mach 9.8 (6,600 mph; 11,000 km/h) at altitudes of 30,000 m or more. The X-43A is a single-use vehicle and is designed to crash into the ocean without recovery. Three of them have been built: the first was destroyed; the other two have successfully flown, with the scramjet operating for approximately 10 seconds, followed by a 10 minute glide and intentional crash.

The first flight in June 2001 failed when the stack spun out of control about 11 seconds after the drop from the B-52 carrier plane. It was destroyed by the Range Safety Officer and crashed into the Pacific Ocean. NASA attributed the crash to several inaccuracies in data modeling for this test, which led to an inadequate control system for the particular Pegasus rocket used.

The X-43A's second flight was successful when it became the fastest free flying air-breathing aircraft in the world.

The third flight of the X-43A set a new speed record of 10,617 km/h (6,598 mph), or Mach 9.65 at 33,528 meters (110,000 ft), on November 16, 2004. It was boosted by a modified Pegasus rocket which was launched from a B-52 mother ship at an altitude of 13,157 meters (43,166 ft). After 10 seconds of free flight, the spacecraft made a planned crash into the Pacific Ocean off the coast of southern California.

The X-plane series of aircraft was replaced by the X-51. The X-43 was part of NASA's Hyper-X program, involving the American space agency and contractors such as Boeing, Micro Craft Inc, Orbital Sciences Corporation and General Applied Science Laboratory (GASL). Micro Craft Inc. built the X-43A and GASL built its engine.

The Hyper-X Phase I is a NASA Aeronautics and Space Technology Enterprise program being conducted jointly by the Langley Research Center, Hampton, Virginia, and the Dryden Flight Research Center, Edwards, California. Langley is the lead center and is responsible for hypersonic technology development. Dryden is responsible for flight research.

Phase I was a seven-year, approximately $230 million, program to flight-validate scramjet propulsion, hypersonic aerodynamics and design methods.

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