Martin
X-24A
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Photo: Robert Deering 1985
National Museum of the USAF
Wright-Paterson AFB (FFO)
Dayton, Ohio
Piloted Low Speed Test (PILOT), the third phase of tech START program, investigated the flight characteristics and maneuverability of manned lifting bodies and analyzed the feasibility of using these aircraft for return from space. The X-24A, developed as a joint USAF/NASA project, was basically a large-scale manned version of the SV-5D PRIME vehicle. The ASSET and PRIME phases of the Air Force's START program conducted research in the higher altitudes and speeds, but the X-24 program concentrated on the last stage of re-entry, from about 70,000 feet (21,280 meters) altitude at 1,000 mph (2,609 km/hr) to landing.

The X-24 made its first powered flight on March 19, 1970. It was carried aloft and released at an altitude of about 40,000 feet (13,860 meters) by the same B-52 used in the X-15 program. Upon release, the X-24A pilot ignited the rocket engine which boosted the lifting body to its maximum speed and altitude. From this point, a powerless landing was made on a dry lakebed. The X-24A made 28 powered flights at the Air Force Flight Test Center, Edwards Air Force Base, Calif., during its test program.

The X-24A on display was originally the jet-powered Martin SV-5J, a derivative of the X-24A built for flight training. It was never flown. For display, the SV-5J has been converted to simulate the X-24A. It was donated by Martin in 1971.
SPECIFICATIONS: PERFORMANCE:
Span:  13 ft. 8 in. (4.2 m) Maximum speed:  1,036 mph (1,667 km/hr)
Length:  24 ft. 6 in. (7.2 m) Cruising speed: 
Height:  10 ft. 4 in. (3.2 m) Range: 
Empty Weight:  Service ceiling:  71,407 ft. (21,765 m)
Gross Weight:  10,700 lbs. (4,853 kg)  
Crew: 
Engines:  One Thiokol XLR-11 rocket of 8,000 lbs. (3,625 kg) thrust; two Bell LLRV optional landing rockets of 400 lbs. (181 kg) thrust each
Armament:   None
   
SOURCE:  National Museum of the United States Air Force