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. The X-15's official world record for the highest speed ever recorded by a manned, powered aircraft, set in October 1967 when William J. Knight flew Mach 6.72 at 102,100 feet (31,120 m), a speed of 4,520 miles per hour (7,274 km/h; 2,021 m/s), has remained unchallenged as of May 2018.
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 these pilots as being astronauts. The Air Force pilots qualified for astronaut wings immediately, while the civilian pilots were eventually awarded NASA astronaut wings in 2005, 35 years after the last X-15 flight. The only Navy pilot in the X-15 program never took the aircraft above the requisite 50 mile altitude and thus never earned astronaut wings.
Video North American X-15
Design and development
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. The requests for proposal (RFPs) 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. Air Force NB-52A, "The High and Mighty One" (serial 52-0003, a.k.a. Balls Three), and NB-52B, "The Challenger" (serial 52-0008, a.k.a. Balls 8) served as carrier planes for all X-15 flights. 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 just before landing. The lower fin was recovered by parachute.
Cockpit and pilot systems
The X-15 was the product of developmental research 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, ballistic flight into thin air/space, re-entry into thicker air, unpowered glide to landing, and direct landing without a main-engine start. The main rocket engine operated only for a relatively short part of the flight, but boosted 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 placed a traditional rudder and stick between a left joystick that sent commands to the Reaction Control System, and a third joystick on the right 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 (RCS) 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 alternative control 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 included heated windows to prevent icing and a forward headrest for periods of high deceleration.
The X-15 had an ejection seat designed to operate at speeds up to Mach 4 (4,480 km/h; 2,784 mph) and/or 120,000 feet (37 km) altitude, although it was never used during the program. In the event of ejection, the seat was designed to deploy fins, which were used until it reached a safer speed/altitude at which to deploy its main parachute. Pilots wore pressure suits, 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, while oxygen for breathing was fed separately to the pilot.
Propulsion
The initial 24 powered flights used two Reaction Motors XLR11 liquid-propellant rocket engines, enhanced to provide a total of 16,000 pounds-force (71 kN) of thrust as compared to the 6,000 pounds-force (27 kN) that a single XLR11 provided in 1947 to make the Bell X-1 the first aircraft to fly faster than the speed of sound. The XLR11 used ethyl alcohol and liquid oxygen.
By November 1960, Reaction Motors was able to deliver the XLR99 rocket engine, generating 57,000 pounds-force (250 kN) of thrust. The remaining 175 flights of the X-15 used XLR99 engines, in a single engine configuration. The XLR99 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; Jules Bergman titled his book on the program Ninety Seconds to Space to describe the total powered flight time of the aircraft.
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 to enable it to fly in a steady manner 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.
A wedge shape was used because it is more effective than the conventional tail as a stabilizing surface at hypersonic speeds. A vertical-tail area equal to 60 percent of the wing area was required to give the X-15 adequate directional stability.
Stability at hypersonic speeds was aided by side panels which could be extended from the tail to increase the overall surface area, and these panels doubled as air-brakes.
Maps North American X-15
Operational history
Altitudes attained by X-15 aircraft fell short of those of Alan Shepard's and Gus Grissom's Project Mercury space capsules in 1961, or of any other manned spacecraft. However, 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 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 weighing 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, AF Ser. No. 56-6672, 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 g0 (150 m/s2) vertical and 8.0 g0 (78 m/s2) 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-15, X-15-2, was rebuilt after a landing accident. It was lengthened by 2.4 feet (73 cm), had a pair of auxiliary fuel tanks attached beneath its fuselage and wings, and a complete heat-resistant ablative coating was added. The plane was renamed the X-15A-2, and took flight for the first time on 28 June 1964. It reached its maximum speed of 4,520 miles per hour (7,274 km/h) in October 1967 with pilot William "Pete" Knight of the U.S. Air Force in control.
In addition to F-100, F-104 and F5D chase aircraft, H-22 helicopters, C-130 transports, and one C-47 transport, five aircraft were used during the span of the X-15 program: three X-15 planes and two B-52 bombers:
- X-15-1 - 56-6670, 82 powered flights
- X-15-2 (later X-15A-2) - 56-6671, 31 powered flights as X-15-2, 22 powered flights as X-15A-2, and 53 in total
- X-15-3 - 56-6672, 64 powered flights
- NB-52A - 52-003 nicknamed "The High and Mighty One" (retired in October 1969)
- NB-52B - 52-008 nicknamed "The Challenger", later "Balls 8" (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 Air Force Museum at Wright-Patterson Air Force Base for display.
Current static displays
- X-15A-1 (AF Ser. No. 56-6670) is on display in the National Air and Space Museum "Milestones of Flight" gallery, Washington, D.C.
- X-15A-2 (AF Ser. No. 56-6671) is at the National Museum of the United States Air Force, at Wright-Patterson Air Force Base, near Dayton, Ohio. It was retired to the museum in October 1969. The aircraft is displayed in the museum's Research and Development Gallery alongside other "X-planes", including the Bell X-1B and Douglas X-3 Stiletto.
Mockups
- Dryden Flight Research Center, Edwards AFB, California, United States (painted with AF Ser. No. 56-6672)
- Pima Air & Space Museum, adjacent to Davis-Monthan AFB, Tucson, Arizona (painted with AF Ser. No. 56-6671)
- Evergreen Aviation & Space Museum, McMinnville, Oregon (painted with AF Ser. No. 56-6672). A full-scale wooden mockup of the X-15, it is displayed along with one of the rocket engines.
Stratofortress mother ships
- NB-52A (AF Ser. No. 52-0003) is displayed at the Pima Air & Space Museum adjacent to Davis-Monthan AFB in Tucson, Arizona. It launched the X-15-1 30 times, the X-15-2, 11 times, and the X-15-3 31 times (as well as the M2-F2 four times, the HL-10 11 times and the X-24A twice).
- NB-52B (AF Ser. No. 52-0008) is on permanent display outside the north gate of Edwards AFB, California. It launched the majority of X-15 flights.
Record flights
Highest flights
The FAI set the limit of space at 100 kilometers (62.1 mi). But in the 1960s, the U.S. Air Force considered an altitude of 50 miles (80 km) as the limit of space; U.S. Air Force and NASA pilots and crew exceeding that altitude at the time could be awarded the astronaut badge. Thirteen X-15 flights went higher than 50 miles, two of which exceeded 100 kilometers.
+ fatal
Fastest recorded flights
Pilots
+ Killed in the crash of an X-15
** White replaced selected pilot Iven Kincheloe, who died before the first X-15 flight.
Specifications
Other configurations include the Reaction Motors XLR11 equipped X-15, and the long version.
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
See also
- Single-person spacecraft
- Aircraft of comparable role, configuration and era
- Bell X-2
- Douglas D-558-2 Skyrocket
- Related lists
- List of rocket aircraft
- List of X-15 flights
- List of spaceflight-related accidents and incidents
References
- Notes
- Bibliography
External links
- NASA
- X-15: Hypersonic Research at the Edge of Space
- Transiting from Air to Space: The North American X-15
- Proceedings of the X-15 First Flight 30th Anniversary Celebration
- Hypersonics Before the Shuttle: A Concise History of the X-15 Research Airplane
- Interview with Neil Armstrong about his experience in the X-15
- NASA Armstrong Fact Sheet: X-15 Hypersonic Research Program
- X-15 photos at NASA Armstrong
- X-15 movies at NASA Armstrong
- The short film Research Project X-15 is available for free download at the Internet Archive
- Non-NASA
- X-15A at Encyclopedia Astronautica
- X-15: Advanced Research Airplane, design summary by North America Aviation
Source of the article : Wikipedia
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