Parade Ground Aircraft
A7 A10 B17 B24 B25 B26 B29 C45 C47 C118 C119 C121
C123 F15 F16 F82 P38 P47 P51 P63 SR71 T6 T28 T34
Other USAF Aircraft
Bombers
B1 B2 B45 B47 B50 B52 B58 F111 - - - -
Cargo, VIP, & Tanker
C5 C17 C21 C24 C46 C97 C130 C133 C140 C141 KC10 KC135
Experimental & Prototype
D558 F107 X1 X2 X3 X4 X5 X15 XB70 YC14 - -
Fighters
A1 F4 F5 F22 F84 F84F F86 F86D F100 F101 F102 F104
F105 F106 F117 P40 P80 - - - - - - -
Helicopters
CH3E CH21 CH54A H5A HH43 MH60 R4B R6A UH1P UH13 UH19 V22
Reconnaissance
E3 O1G OV2 OV10 RF4 RF101 U2 - - - - -
Trainers
T6A T33 T37 T38 T41 - - - - - - -

North American X-15 Rocket Plane


The North American X-15, a rocket-powered research aircraft, bridged the gap between manned flight in the atmosphere and space flight. After its initial test flights in 1959, the X-15 became the first winged aircraft to attain hypersonic velocities of Mach 4, 5, and 6 (four to six times the speed of sound) and to operate at altitudes well above 30,500 meters (100,000 feet).

The X-15 was carried to an altitude of 12,000 meters (40,000 feet) under the wing of a Boeing B-52 bomber. During one test, it attained an altitude of over 108 kilometers (67 miles), flying so high that it functioned more as a spacecraft than an airplane. In 1967 it reached Mach 6.72 (7,297 kilometers or 4,534 miles per hour).

The X-15 was designed to explore the problems of flight at very high speeds and altitudes. The X-15 and other research aircraft contribute to the advancement of aerospace technology. Transferred from the National Aeronautics and Space Administration.

Design Features: The wedge-shaped tail surfaces of the X-15 provided directional stability at speeds where conventionally shaped airfoils would not be effective. The large upper and lower fins and the downward slant of the wings enabled the aircraft to remain stable during steep climbs and at high altitudes. The substructure of the X-15 is titanium with a covering of Inconel X, a nickel alloy capable of withstanding temperatures of 650¡ (1,200¡). The black color of the aircraft helped to dissipate heat, and the gaps along the fuselage closed as the external temperature increased. The small holes near the nose are for attitude control jets, used at very high altitudes where airfoil surfaces no longer provide aerodynamic control.

Wingspan: 6.7 m (22 ft)

Length: 15.5 m (51 ft)

Height: 4 m (13 ft)

Weight, gross: 17,237 kg (38,000 lb)

Engine: Thiokol (Reaction Motors) XLR-99-RM-2 rocket engine rated at 250,000 newtons (57,000 lbs) thrust at sea level

Manufacturer: North American Aviation, Los Angeles, California, U.S.A., 1959

 

Parade Ground Aircraft
A7 A10 B17 B24 B25 B26 B29 C45 C47 C118 C119 C121
C123 F15 F16 F82 P38 P47 P51 P63 SR71 T6 T28 T34
Other USAF Aircraft
Bombers
B1 B2 B45 B47 B50 B52 B58 F111 - - - -
Cargo, VIP, & Tanker
C5 C17 C21 C24 C46 C97 C130 C133 C140 C141 KC10 KC135
Experimental & Prototype
D558 F107 X1 X2 X3 X4 X5 X15 XB70 YC14 - -
Fighters
A1 F4 F5 F22 F84 F84F F86 F86D F100 F101 F102 F104
F105 F106 F117 P40 P80 - - - - - - -
Helicopters
CH3E CH21 CH54A H5A HH43 MH60 R4B R6A UH1P UH13 UH19 V22
Reconnaissance
E3 O1G OV2 OV10 RF4 RF101 U2 - - - - -
Trainers
T6A T33 T37 T38 T41 - - - - - - -