North American X-15

The North American X-15 was a hypersonic rocket-powered aircraft operated by the United States Air Force and the National Aeronautics and Space Administration as part of the X-plane series of experimental aircraft. The X-15 set speed and altitude records in the 1960s, reaching the edge of outer space and returning with valuable data used in aircraft and spacecraft design. As of 2015, the X-15 holds the official world record for the highest speed ever reached by a manned, powered aircraft. Its maximum speed was 4,520 miles per hour (7,274 km/h), or Mach 6.72.

During the X-15 program, 13 flights by eight pilots met the Air Force spaceflight criterion by exceeding the altitude of 50 miles (80 km), thus qualifying the pilots for astronaut status. The Air Force pilots qualified for astronaut wings immediately, while the civilian pilots were awarded NASA astronaut wings in 2005, 35 years after the last X-15 flight. The sole Navy pilot in the X-15 program never took the aircraft above the requisite 50 mile altitude.

Of all the X-15 missions, two flights (by the same pilot) qualified as space flights per the international (Fédération Aéronautique Internationale) definition of a spaceflight by exceeding 100 kilometers (62.1 mi) in altitude.

North American X-15
Class Aircraft
Type Utility
Manufacturer North American Aviation
Origin United States of America
Country Name Origin Year
United States of America 1959
Country Name Operational Year Retirement Year
United States of America 1959 1968 View
ManufacturerName Production From Production To Quantity
North American Aviation 3 View

The X-15 was based on a concept study from Walter Dornberger for the National Advisory Committee for Aeronautics (NACA) for a hypersonic research aircraft.[4] The requests for proposal were published on 30 December 1954 for the airframe and on 4 February 1955 for the rocket engine. The X-15 was built by two manufacturers: North American Aviation was contracted for the airframe in November 1955, and Reaction Motors was contracted for building the engines in 1956.

Like many X-series aircraft, the X-15 was designed to be carried aloft and drop launched from under the wing of a NASA B-52 mother ship, the Balls 8. Release took place at an altitude of about 8.5 miles (13.7 km) and a speed of about 500 miles per hour (805 km/h). The X-15 fuselage was long and cylindrical, with rear fairings that flattened its appearance, and thick, dorsal and ventral wedge-fin stabilizers. Parts of the fuselage were heat-resistant nickel alloy (Inconel-X 750). The retractable landing gear comprised a nose-wheel carriage and two rear skids. The skids did not extend beyond the ventral fin, which required the pilot to jettison the lower fin (fitted with a parachute) just before landing.

Cockpit and pilot systems

The X-15 was a research program and changes were made to various systems over the course of the program and between the different models. The X-15 was operated under several different scenarios including attachment to a launch aircraft, drop, main engine start and acceleration, a ballistic flight into thin air/space, re-entry into thicker air, and an unpowered glide to landing. Alternatively, if the main engine was not started the pilot went directly to a landing. The main rocket engine operated only for a relatively short part of the flight, but was capable of boosting the X-15 to its high speeds and altitudes. Without main engine thrust, the X-15's instruments and control surfaces remained functional, but the aircraft could not maintain altitude.

Because the X-15 also had to be controlled in an environment where there was too little air for aerodynamic flight control surfaces, it had a reaction control system (RCS) that used rocket thrusters. There were two different X-15 pilot control setups: one used three joysticks; the other, one joystick.

The X-15 type with multiple control sticks for the pilot included a traditional rudder and stick, and another joystick on the left which sent commands to the reaction control system. A third joystick on the right side was used during high-G maneuvers to augment the center stick. In addition to pilot input, the X-15 "Stability Augmentation System" (SAS) sent inputs to the aerodynamic controls to help the pilot maintain attitude control. The reaction control system could be operated in two modes, manual and automatic. The automatic mode used a feature called "Reaction Augmentation System" (RAS) that helped stabilize the vehicle at high altitude. The RAS was typically used for approximately three minutes of an X-15 flight before automatic power off.

The second setup used the MH-96 flight control system which allowed one joystick in place of three and simplified pilot input. The MH-96 could automatically blend aerodynamic and rocket controls depending on how effective each system was at controlling the aircraft.

Among the many controls, were the rocket engine throttle and a control for jettisoning the ventral tail fin. Other features of the cockpit were heated windows to prevent icing, and a forward headrest for periods of high deceleration.

The X-15 had an ejection seat that allowed ejection at speeds up to Mach 4 and/or 120,000 feet (37 km) altitude, although it was not used during the program. In the event of ejection, the seat had deployable fins which were used until it reached a safer speed/altitude, where it could deploy its main parachute. Pilots wore a pressure suit, which could be pressurized with nitrogen gas. Above 35,000 feet (11 km) altitude, the cockpit was pressurized to 3.5 psi (0.24 atm) with nitrogen gas, and oxygen for breathing was fed separately to the pilot.

Propulsion

Early flights used two Reaction Motors XLR11 liquid-propellant rocket engines. Later flights were undertaken with a single XLR99 rocket engine generating 57,000 pounds-force (250 kN) of thrust. The XLR11 used ethyl alcohol and liquid oxygen. The XLR99 engine used anhydrous ammonia and liquid oxygen as propellant, and hydrogen peroxide to drive the high-speed turbopump that delivered propellants to the engine. It could burn 15,000 pounds (6,804 kg) of propellant in 80 seconds. The XLR99s could be throttled, and were the first such controllable engines that were man-rated.

The X-15 reaction control system (RCS), for maneuvering in low-pressure/density environment, used high-test peroxide (HTP), which decomposes into water and oxygen in the presence of a catalyst and could provide a specific impulse of 140 seconds. The HTP also fueled a turbopump for the main engines and auxiliary power units (APUs). Additional tanks for helium and liquid nitrogen performed other functions, for example the fuselage interior was purged with helium gas, and the liquid nitrogen was used as coolant for various systems.

Wedge tail and hypersonic stability

The X-15 had a thick wedge tail for stability at hypersonic speeds. This produced a significant amount of drag at lower speeds; the blunt end at the rear of the X-15 could produce as much drag as an entire F-104 Starfighter.

Stability at hypersonic speeds was aided by side panels that could extend out from the tail to increase area, and the panels doubled as air-brakes.

Altitudes attained by X-15 aircraft do not match those of Alan Shepard's and Gus Grissom's Project Mercury space capsules in 1961, nor of any other manned spacecraft. The X-15 ranks supreme among manned rocket-powered aircraft, becoming the world's first operational spaceplane in the early 1960s.

Before 1958, United States Air Force (USAF) and NACA officials discussed an orbital X-15 spaceplane, the X-15B that would launch into outer space from atop an SM-64 Navaho missile. This was canceled when the NACA became NASA and adopted Project Mercury instead.

By 1959, the Boeing X-20 Dyna-Soar space-glider program was to become the USAF's preferred means for launching military manned spacecraft into orbit. This program was canceled in the early 1960s before an operational vehicle could be built. Various configurations of the Navajo were considered, and another proposal involved a Titan I stage.

Three X-15s were built, flying 199 test flights, the last on 24 October 1968.

The first X-15 flight was a captive-carry unpowered test by Albert Scott Crossfield, on 8 June 1959. Crossfield also piloted the first powered flight, on 17 September 1959, and his first flight with the XLR-99 rocket engine on 15 November 1960. Twelve test pilots flew the X-15. Among these were Neil Armstrong, later a NASA astronaut and first man to set foot on the Moon, and Joe Engle, later a commander of NASA Space Shuttle test flights.

In a 1962 proposal, NASA considered using the B-52/X-15 as a launch platform for a Blue Scout rocket to place satellites up to 150 pounds (68 kg) into orbit.

In July and August 1963, pilot Joseph A. Walker exceeded 100 km in altitude, joining NASA astronauts and Soviet cosmonauts as the first human beings to cross that line on their way to outer space. The USAF awarded astronaut wings to anyone achieving an altitude of 50 miles (80 km), while the FAI set the limit of space at 100 kilometers (62.1 mi).

On 15 November 1967, U.S. Air Force test pilot Major Michael J. Adams was killed during X-15 Flight 191 when the (X-15-3) entered a hypersonic spin while descending, then oscillated violently as aerodynamic forces increased after re-entry. As his aircraft's flight control system operated the control surfaces to their limits, acceleration built to 15 g vertical and 8.0 g lateral. The airframe broke apart at 60,000 feet (18 km) altitude, scattering the X-15's wreckage for 50 square miles (130 km2). On 8 May 2004, a monument was erected at the cockpit's locale, near Randsburg, California. Major Adams was posthumously awarded Air Force astronaut wings for his final flight in X-15-3, which had reached an altitude of 50.4 miles (81.1 km). In 1991, his name was added to the Astronaut Memorial.

The second X-15A was rebuilt after a landing accident. It was lengthened 2.4 feet (0.73 m), a pair of auxiliary fuel tanks attached beneath its fuselage and wings, and a complete heat-resistant ablative coating was added. Renamed the X-15A-2, this plane first flew on 28 June 1964. It reached a maximum speed of 4,520 miles per hour (7,274 km/h) in October 1967 while being flown by William "Pete" Knight of the U.S. Air Force.

Five aircraft were used during the X-15 program: three X-15s planes and two B-52 bombers:

  • X-15A – 56-6670, 82 powered flights
  • X-15A (later X-15A-2) – 56-6671, 31 powered flights as X-15A, 22 powered flights as X-15A-2, and 53 in total
  • X-15A – 56-6672, 64 powered flights
  • NB-52A – 52-003 (retired in October 1969)
  • NB-52B – 52-008 (retired in November 2004)

A 200th flight over Nevada was first scheduled for 21 November 1968, to be flown by William "Pete" Knight. Numerous technical problems and outbreaks of bad weather delayed this proposed flight six times, and it was permanently canceled on 20 December 1968. This X-15 was detached from the B-52 and then put into indefinite storage. The aircraft was later donated to the museum at Wright-Patterson Air Force Base for display.

Role Experimental high-speed rocket-powered research aircraft
Manufacturer North American Aviation
First flight 8 June 1959
Introduction 17 September 1959
Retired December 1968
Primary users United States Air Force
NASA
Number built 3


General characteristics

  • Crew: one
  • Length: 50 ft 9 in (15.45 m)
  • Wingspan: 22 ft 4 in (6.8 m)
  • Height: 13 ft 6 in (4.12 m)
  • Wing area: 200 ft2 (18.6 m2)
  • Empty weight: 14,600 lb (6,620 kg)
  • Loaded weight: 34,000 lb (15,420 kg)
  • Max. takeoff weight: 34,000 lb (15,420 kg)
  • Powerplant: 1 × Reaction Motors XLR99-RM-2 liquid propellant rocket engine, 70,400 lbf at 30 km (313 kN)

Performance

  • Maximum speed: 4,520 mph (7,274 km/h)
  • Range: 280 mi (450 km)
  • Service ceiling: 67 mi (108 km, 354,330 ft)
  • Rate of climb: 60,000 ft/min (18,288 m/min)
  • Wing loading: 170 lb/ft2 (829 kg/m2)
  • Thrust/weight: 2.07

End notes