Martin
X-24B
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Photo: Robert Deering 1985
National Museum of the USAF
Wright-Paterson AFB (FFO)
Dayton, Ohio
In 1972 the X-24A was stripped to the basic framework and rebuilt as the X-24B with a more stable external configuration designed by the Air Force Flight Dynamics Laboratory. The new body was delta-shaped and had twice the lifting surface of the X-24A. As a continuation of PILOT, the goals of the testing program were to explore handling qualities of the wingless configuration for extended near-earth flight and for conventional runway approaches and landings.

The flight plan for the X-24B was much the same as that of the X-24A. After being carried to about 45,000 feet (13,680 meters) altitude by a B-52, the X-24B was released. Following ignition and burnout of the rocket engine, the pilot guided the lifting body to a glide landing. On Aug. 5, 1975, the X-24B made the first landing of a lifting body on a conventional runway. A second landing on the same runway on Aug. 20, 1975, confirmed that the lifting body could safely be landed like normal aircraft.

The X-24B made its 36th and last flight on Nov. 26, 1975. It was delivered to the museum in November 1976.
SPECIFICATIONS: PERFORMANCE:
Span:  19 ft. 2 in. Maximum speed:  1,163 mph
Length:  37 ft. 6 in. Cruising speed: 
Height:  10 ft. 4 in. Range: 
Empty Weight:  Service ceiling:  74,130 ft.
Gross Weight:  13,000 lbs. loaded  
Crew: 
Engines:  One Reaction Motors XLR-11 rocket of 8,000 lbs. thrust and two bell LLRV optional landing rockets of 400 lbs. thrust each
   
SOURCE:  National Museum of the United States Air Force