Martin-Marietta X-24

The X-24 was an experimental US aircraft developed from a joint USAF-NASA program named PILOT (1963-1975). It was designed and built to test lifting body concepts, experimenting with the concept of unpowered reentry and landing, later used by the Space Shuttle.

Martin-Marietta X-24A

Lifting bodies’ aerodynamic lift, essential to flight in the atmosphere, was obtained from their shape. The addition of fins and control surfaces allowed the pilots to stabilize and control the vehicles and regulate their flight paths.

Martin-Marietta X-24B

The X-24A was a fat, short teardrop shape with vertical fins for control. It made its first, unpowered, glide flight on April 17, 1969 with Air Force Maj. Jerauld Gentry at the controls. Gentry also piloted its first powered flight on March 19, 1970.

Martin-Marietta X-24B

The craft was taken to around 45,000 feet (13.7 km) by a modified B-52 and then drop launched, then either glided down or used its rocket engine to ascend to higher altitudes before gliding down. The X-24A was flown 28 times at speeds up to 1,036 mph (1,667 km/h) and altitudes up to 71,400 feet (21.8 km).

The X-24A was modified into the more stable X-24B with an entirely different shape in 1972. The bulbous shape of the X-24A was converted into a "flying flatiron" shape with a rounded top, flat bottom, and double delta platform that ended in a pointed nose. 

First to fly the X-24B was John Manke, a glide flight on 1 August 1973. He was also the pilot on the first powered mission 15 November 1973.Martin-Marietta X-24B


The X-24B demonstrated that accurate unpowered reentry vehicle landings were operationally feasible. Top speed achieved by the X-24B was 1,164 mph (1873 km/h) and the highest altitude it reached was 74,130 feet (22.59 km).

Among the final flights with the X-24B were two precise landings on the main concrete runway at Edwards which showed that accurate unpowered reentry vehicle landings were operationally feasible.


Martin-Marietta X-24A


Specifications (Martin-Marietta X-24A)
General characteristics

Crew: one pilot
Length: 24 ft 6 in (7.47 m)
Wingspan: 11 ft 6 in (3.51 m)
Height: 9 ft 7 in (2.92 m)
Wing area: 195 ft² (18.1 m²)
Empty: 6,360 lb (2,885 kg)
Loaded: 10,700 lb (4,853 kg)
Maximum takeoff: 11,447 lb (5,192 kg)
Powerplant:
1 x Reaction Motors Upgraded XLR-11 four-chamber rocket engine. 8,480 lbf (37.7 kN) thrust.

Performance:
Maximum speed: 1,036 mph (1,667 km/h)
Range: 45 miles (72 km)
Service ceiling: 71,407 ft (21,763 m)
Rate of climb: ft/min (m/min)
Wing loading: 59 lb/ft² (288 kg/m²)
Thrust-to-Weight: 0.70
Martin-Marietta X-24B
Specifications (Martin-Marietta X-24B)
General characteristics

Crew: one pilot
Length: 37 ft 6 in (11.43 m)
Wingspan: 19 ft 0 in (5.79 m)
Height: 9 ft 7 in (2.92 m)
Wing area: 330 ft² (30.7 m²)
Empty: 8,500 lb (3,855 kg)
Loaded: 11,800 lb (5,350 kg)
Maximum takeoff: 13,800 lb (6,260 kg)
Powerplant: 1 x Reaction Motors Upgraded XLR-11 four-chamber rocket engine. 8,480 lbf (37.7 KN) thrust.

Performance:
Maximum speed: 1,164 mph (1,873 km/h)
Range: 45 miles (72 km)
Service ceiling: 74,130 ft (22.59 km)
Wing loading: 42 lb/ft² (205 kg/m²)
Thrust-to-Weight: 0.71

Links:
http://www.codeonemagazine.com
http://www.dfrc.nasa.gov
http://www.edwards.af.mil
http://www.globalaircraft.org
http://www.drivearchive.co.uk
http://users.dbscorp.net
http://www.fas.org


Video 1:


Video 2:


(This text was adapted from http://www.wikipedia.org/ )(GFDL)
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