North American X-15 Poster

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Burnout AR IZ N O N A UTAH N E V AD A AD OR EG ON Feet 350 TYPICAL HIGH-ALTITUDE (Thousands) STRATOSPHERE IONOSP journey of discovery, the X-15 became the fastest and highest- fying piloted winged airplane of its time. its d iscoveries set naSa o n a direct course for the exploration of space. To The edge of BALLISTIC THE OUTER s SKIN OF THE X-15 WAS p MADE OF A NICKEL-CHR a OMIUM ALLOY ce... ® SenSational, iconic, groundbreaking. th e X-15 hypersonic research airplane signifcantly extended the frontiers of fight. it was a program of outstand ing engineering achievements, jaw-dropping performance characteristics, and extraordinary human endeavor. during a 15-year 354,200 ft highesT alTiTude aTTained for a winged aircrafT (ThaT’s 67 miles high!) and an achievemenT noT surpassed unTil 2004 NW-2008-09-195-HQ 1,325º f The peaK surface TemperaTure of a TesT panel on The X-15 during a mach 5 mission 4,520 mph Top speed of mach 6.70 — an achievemenT unBroKen for 41 years 8-g The g-force eXperienced By X-15 piloTs on some flighTs during reenTry inTo earTh’s aTmosphere a wing and a prayer Test pilot Scott Crossfeld helped to design the ejection seat, which enabled “safe ejection at speeds up to Mach 4, in any attitude and at any altitude up to 120,000 feet.”After the canopy was jettisoned, the seat fred upward and, once clear of the aircraft, deployed a pair of fold-out fns and telescoping booms for stabilization. A face-heater battery activated to keep the pilot’s visor clear of ice, and oxygen was supplied from two under-seat tanks. Despite the seat’s sophistication, none of the pilots wanted to see it used on a mission. t was arguably the most successful aeronautical research efort in history. Between June 1959 and October 1968, NASA’s X-15 hypersonic research fights rewrote the rule book of conventional fight and spawned an extraordinary legacy that lives on today. The world’s frst piloted vehicle designed to study the realms of hypersonic fight—an experimental aircraft of mind-boggling performance—was conceived by a joint team from NASA, the U.S. Air Force, the U.S. Navy and North American Aviation. The goal was to fy at Mach 6—six times faster than the X-1 aircraft that exceeded the sound barrier a decade earlier. The team aimed to fy the X-15 at an altitude of 250,000 ft—nearly 50 miles above Earth’s surface. By the time NASA test pilot Bill Dana brought the 199th and fnal X-15 fight to a stop on the parched lake bed of Edwards Air Force Base in California on October 24, 1968, these goals had been achieved. The X-15 few faster and higher than any other piloted winged vehicle other than the space shuttle. On separate fights, the X-15 reached Mach 6.70 (4,520 mph) and 354,200 feet. The program could have broken every speed and altitude record in the books, but that was not the goal. The sole purpose of the X-15 was to enable research at hypersonic velocities and at the edge of space. The legacy The X-15 program yielded a treasure trove of valuable data and fresh understanding. Perhaps most critically, it provided a major technological stepping-stone to space. The Mercury, Gemini, and Apollo programs all benefted from the X-15 research and, every time a space shuttle returns from orbit, it does so using knowledge derived from the X-15. The X-15 demonstrated for the frst time that pilots could fy rocket-powered aircraft out of Earth’s atmosphere, control them successfully in an airless environment, reenter the atmosphere and perform a precision landing at a predetermined site. In other words, it invented what eventually became the basic fight profle for a space shuttle mission. Triumphs and Tragedy The achievements of the X-15 are breathtaking. Not only did the aircraft create history with its speed and altitude, it gave birth to some amazing successes—the frst extensive use of simulation as an engineering tool, frst full-pressure suit for pilot protection in space, frst application of hypersonic theory to a fight vehicle. The list goes on. However, the program also experienced its share of setbacks and one tragic loss. On November 15, 1967, Air Force test pilot Maj. Michael J. Adams reached 266,000 feet during a test fight. Suddenly, his aircraft went into a hypersonic spin from which he could not recover. In spite of the pioneering nature of the program, his was the only fatality and aircraft loss. in conTeXT “X” means “experimental.”The frst “X” designation went to the Bell X-1, which, on October 14, 1947, became the frst airplane to break the sound barrier in level fight. Since then, more than 50 diferent major research designs have used the“X” designation. Although not every “X” vehicle became a fying prototype, every design proved to be a highly valuable research tool for advancing knowledge of aerodynamics and astronautics. NASA continues to invest in next-generation technologies to ensure that the legacy of the X-15 lives on. whiTe lighTning The X-15A-2 (pictured above) was designed for maximum speed. Two external tanks for liquid ammonia and liquid oxygen provided an extra 60 seconds of engine burn and, in theory, could power the rocket plane to speeds well in excess of Mach 7. The white color of the aircraft was due to the application of an ablative coating designed to protect the structure from the high temperatures that would be generated at such speeds. The fuselage was extended by 29 inches to carry liquid hydrogen for a planned supersonic combustion ramjet (scramjet) that was fown in mockup form but never actually tested. In the hands of pilot Pete Knight, the X-15A-2 reached Mach 6.70 (4,520 mph), the fastest fight of the X-15 program. A SERVO-ACTUATED“BALL NOSE” FLOW DIRECTION SENSORPROVIDEDACCURATE MEASUREMENT OF ANGLE OF ATTACK AND ANGLE OF SIDESLIPATSUPERSONICAND HYPERSONIC VELOCITIES. PITOT HEAD THREE-PANELS-THICK WINDSHIELD(HEATED WITH NITROGEN GAS TO PREVENT FROSTING/FOGGING) NO. 2 EQUIPMENT COMPARTMENT SKYLIGHT HATCH FUSE PANEL L AUXILIARY POWER UNITS IQUIDNITROGENTANK (AIR CONDITIONING ANDPRESSURIZATION SYSTEM) L LIQUID OXYGEN TANK VENT LIQUID OXYGEN TANK (ENGINE OXIDIZER) HELIUM TANK (FOR ENGINE PROPELLANT PRESSURIZATION) CONTROLSYSTEM THRUSTERS CALLED INCONEL X ,EMPLOYED IN A HOT STRUCTURETHATWAS CAPABLE OFWITHSTANDINGTEMPERATURES IN EXCESS OF 1200° F.THE BEAMS AND SPARS OF THE WINGS AND THE RING STRUCTURE OF THE FUSELAGE WERE CONSTRUCTED FROM STRONG TITANIUM-MANGANESE ALLOY. WING FLAP WINGATTACHMENTSTRUCTURE AMMONIA TANK (ENGINE FUEL) HYDROGEN PEROXIDE TANK (ENGINETURBOPUMPPROPELLANT) MOVABLE UPPER VERTICAL STABILIZER UPPER SPEED BRAKE XLR99-RM-1 ROCKET ENGINE HELIUMTANK (FOR ENGINE PURGE) ALL-MOVING HORIZONTAL STABILIZER OWER VERTICAL STABILIZER (JETTISONED JUST BEFORE LANDING) RETRACTABLE LANDING GEAR SKIDS BALLISTIC CONTROLSYSTEM THRUSTERS NO. 3 EQUIPMENT COMPARTMENT HELIUM TANK (FOR PRESSURIZATION) LIQUID OXYGEN TANK FILLER HYDRAULICSYSTEM RESERVOIRS HYDROGEN PEROXIDE TANK (AUXILIARYPOWER UNITANDBALLISTIC CONTROLSYSTEM PROPELLANT) HELIUM TANK (AUXILIARY POWER UNIT PROPELLANT PRESSURIZATION) TELEMETRY RECORDERS AREA FOR EXPERIMENTS NO. 1 EQUIPMENT COMPARTMENT BALLISTIC CONTROLSYSTEM THRUSTERS half a million horsepower The power generated by the X-15’s XLR99 rocket engine was awesome. The physical stress exerted on the human body was so high that test pilot Milt Thompson once joked that the X-15 was the only aircraft he had ever fown that made him glad when the engine quit. Developed and built by the Reaction Motors Division of Thiokol Chemical, the XLR99 could deliver up to 57,000 pounds of thrust, or the equivalent of over half a million horsepower. The propellants were liquid oxygen and anhydrous ammonia, fed into the engine by turbopumps at a fow rate of more than 13,000 pounds per minute. The XLR99 had a rated operating life of 1 hour, after which it could be overhauled and used again. The basic X-15 carried propellants for about 85 to 90 seconds of full-power fight, and the X-15A-2 carried propellants for more than 150 seconds of full-power fight. Early fights of the X-15 were powered by the Reaction Motors XLR11—the same engine that powered the Bell X-1—which acted as an interim engine until development work on the XLR99 was complete. I 1 TANK PRESSURIZATION SELECTO 2 ENGINE THROTTLE 3 ALTIMETER 4 AIRSPEED/MACH INDICATOR 5 ACCELEROMETER 6 CONVENTIONAL CENTER STICK (MOVED THE AERODYNAMIC CONTROL SURFACES) 7 VERTICAL VELOCITY INDICATOR 8 SYSTEM WARNING LIGHTS 9 CANOPY EMERGENCY JETTISON HANDLE 7 5 4 3 8 9 1 6 2 flying aT The edge To protect the pilot and sensitive electronics from the ferocious heat of hypersonic fight, the pressurized aluminum cockpit and equipment bay were insulated from the outer Inconel X shell by a radiation shield and insulation blanket. The X-15 included one of the frst inertial navigation systems (called a“stable platform”) to let the pilot know his precise position over the High Range, and a sophisticated Stability Augmentation System to help him maintain precise control of the aircraft. Above Earth’s atmosphere, reaction controls kept the aircraft stable. Hand controllers in the cockpit were linked to small hydrogen peroxide thrusters at the nose for pitch and yaw control, and on each outer wing to control roll. The most dangerous part of a mission was the descent. As the pilot switched from thruster control to traditional “stick-and-rudder” fying, the X-15 became a 15,000- pound unpowered hypersonic glider glowing red-hot as it decelerated from 4,000 mph to 200 mph. With only one shot at landing, there was simply no room for error. The carrier aircrafT Before the X-15 could negotiate any mission successfully, a mother ship had to carry the research airplane to high altitude since the X-15 did not have enough propellant to take of from the ground. A pair of mighty Boeing B-52 Stratofortress aircraft took the X-15 under their wings. The NB-52A was dubbed “The High and Mighty One” and the NB-52B “The Challenger.” The B-52 carried the X-15 to a launch altitude of approximately 45,000 feet. When the X-15 pilot hit the launch switch, the research airplane dropped away from the B-52, falling toward Earth just until the rocket engine ignited and then accelerating to Mach 5 or even Mach 6. The B-52/X-15 combination made 336 fights, including 199 successful launches of the X-15. Of the others, 12 were planned“captive”missions in which the X-15 remained attached to the B-52 to check out various systems, and 125 fight attempts ended as aborts in which the X-15 remained safely under the B-52’s wing until the pair returned to Edwards Air Force Base. So successful were the mother ships that the NB-52B—better known as “NASA 008”—served for nearly 50 years until its retirement in December 2004. Maintenance crews treated the venerable aircraft more like a classic car than an aging bomber. It ended its career as it began—in hypersonics. During its last mission, the NASA 008 launched the unpiloted X-43A scramjet research vehicle on a fight that reached a velocity of Mach 9.60. full-pressure suiT The full-pressure suit worn by X-15 pilots to protect them from the efects of high-altitude fight was revolutionary. Previous pressure suits were cumbersome, virtually immobilized the pilot, and were mostly inefective. Fresh thinking was required. The answer was a groundbreaking development by the David Clark Company that resulted in the MC-2 suit. The introduction of an inner nylon mesh called “link-net” radically improved mobility and provided much improved protection against the harsh environment. The suit was integral to the pilot’s environment. It provided cooling and ventilation; supplied oxygen; and contained parachute harness, a microphone, earphones and pressure regulators. Visors were heated for the same reason as car windshields—to prevent fogging. A total of 36 X-15 fights used the original MC-2 suit, while the remainder used the newer A/P22S-2, also developed by the David Clark Company. Each suit was custom-made for a particular X-15 pilot. Variants of this design would become the standard full-pressure suit used across all U.S. military and NASA programs. It was all about acceleration. The B-52 carrier deceleration. The rest of the 8- to 12-minute aircraft traveled at 500 miles per hour and fight continued without rocket power. 45,000 feet when the X-15 pilot hit the launch On high-altitude missions, the pilot switch. A few seconds of freefall followed, experienced microgravity (“zero-g”) for nearly 2 and then the earth-shatteringly powerful minutes as the X-15 often soared past 300,000 57,000-pound XLR99 rocket engine ignited feet. After glimpsing the curvature of Earth, and catapulted the 33,000-pound X-15 toward the pilot experienced 5- to 8-g during reentry. Mach 5. On high-speed missions, the X-15 reached an The heart rate of an X-15 pilot ranged from altitude of 100,000 feet, which heated the skin 145 to 185 beats per minute as the adrenaline of the airplane until it glowed nearly red-hot. It surged. Chest-to-back acceleration was 2-g could also accelerate from Mach 5 to Mach 6 in up to 4-g. At engine shutdown after nearly 90 an eye-watering six seconds. seconds thrust, he braced his helmet against a headrest in front of him for the 2-g of immediate HERE TYPICAL HIGH-SPEED MISSION PROFILE 300 3. Control in near vacuum 250 4. Reentry 2. Leave 99.9% heating 200 atmosphere Burnout MISSION PROFILE 150 1. Launch from B-52 100 5. Pull-out 65,000 ft 50 WENDOVER AFB 0 ELY HIGH RANGE TRACKING BEATTY STATION HIGH RANGE TRACKING STATION EDWARDS AFB 6. Glide to landing flighT s of discovery X-15 achievemenTs The X-15’s legacy is quanTifiaBle noT JusT in Terms of speed or alTiTude achievemenTs, BuT also in Terms of whaT iT TaughT nasa and The american puBlic aBouT The fuTure possiBiliTies of hypersonic flighT. These achievemenTs include: R » development of the frst practical full- pressure suit for pilot protection in space » first application of hypersonic theory and wind tunnel work to an actual fight vehicle » development of computer-based simulation as an engineering and fight-planning tool » development of a servo-actuated ball nose fow direction sensor for accurate measure- ment of angle of attack and sideslip angle at supersonic and hypersonic speeds » development of inertial fight data systems capable of functioning in high dynamic pressure and space environments » demonstration of a pilot’s ability to control a rocket-boosted aerospace vehicle through atmospheric exit heroes of The hypersonic a tot al of 12 test pilots from n asa, the u.s. air force, the u.s. navy a nd north americ an avi ation few the X-15. a. scott crossfeld North American Aviation’s Crossfeld was intimately involved in the design of the X-15. He piloted the frst free fight on June 8, 1959, and the frst powered fight on September 17. He completed 1 glide and 13 powered fights, reaching a maximum speed of Mach 2.97 (1,960 mph). In July 1962, he was a joint recipient of the Collier Trophy, which was presented by President John F. Kennedy. Joseph a. w alker Walker made the frst X-15 fight by a NASA pilot on March 25, 1960. He few the airplane 25 times and made the highest fight (354,200 ft) of the program on August 22, 1963. He also few the fastest fight (4,104 mph) of the basic X-15 confguration. In July 1962, he was a joint recipient of the Collier Trophy, which was presented by President John F. Kennedy. robert m. white Air Force test pilot White made 16 fights in the X-15 between April 13, 1960, and December 14, 1962. White was the frst pilot to fy any aircraft faster than Mach 4, 5 and 6, as well as the frst to fy above 200,000 and 300,000 feet. He set the only ofcial world record of the X-15 program when he few to 314,750 feet on July 17, 1962, a Fédération Aéronautique Internationale altitude record that still stands. National Aeronautics and Space Administration forrest s. peter sen Petersen was the only Navy pilot to fy the X-15. He made fve fights in the aircraft at speeds of up to Mach 5.30 (3,600 mph). Petersen had the dubious distinction of making the program’s frst uprange emergency landing on January 10, 1962, at Mud Lake. In July 1962, he was a joint recipient of the Collier Trophy, which was presented by President John F. Kennedy. John B. mcKay “Jack”McKay made 29 X-15 fights, reaching Mach 5.65 on August 26, 1964, and a peak altitude of 295,600 feet on September 28, 1965. McKay was seriously injured on November 9, 1962, during an emergency landing at Mud Lake, but he recovered and few 22 more X-15 fights. The airplane he crashed was rebuilt into the advanced X-15A-2. robert a. rushworth Rushworth few the X-15 more times than any other pilot, logging 34 fights in total, including 2 with the interim XLR11 engines. During these fights, he achieved Mach 6.06 (4,018 mph) and 285,000 feet altitude. He was the second Air Force X-15 pilot (after Bob White) to attain an astronaut rating by fying the X-15 and was the frst pilot to fy the advanced X-15A-2. neil a. armstrong A name synonymous with aeronautical achievement, Armstrong was actively engaged in both piloting and engineering aspects of the X-15. As a NASA test pilot, he completed seven X-15 fights, including the frst fight of the MH-96 adaptive fight control system. Armstrong would ensure his place in history on July 20, 1969, when he became the frst human to land on the moon during the Apollo 11 mission. Joe h. engl e Engle completed 16 fights in the X-15, exceeding Mach 5 on 10 of those fights. In June 1965, he climbed to an altitude of 280,600 feet, thereby earning his Air Force astronaut rating long before he joined the NASA Astronaut Corps. He accumulated the last of his 224 hours in space when he commanded the Space Shuttle Discovery during STS-51I in 1985. milton o. Thompson Thompson began fying X-15s on October 29, 1963, and went on to complete 14 fights during the next 2 years, reaching Mach 5.48 (3,712 mph) and a peak altitude of 214,100 feet. In 1962, Thompson was selected as the sole NASA test pilot for the X-20 Dyna-Soar, the frst viable reusable spacecraft. The Dyna-Soar program was canceled prior to its frst fight. william J. Knight “Pete” Knight few the fastest fight of the program on October 3, 1967, when his advanced X-15A-2 reached Mach 6.70 (4,520 mph). He also had more than his share of eventful fights. For instance, while climbing through 107,000 feet at Mach 4.17 on June 29, 1967, he sufered a total electrical failure. Knight calmly glided to a safe emergency landing. william h. dana Bill Dana was at the controls of the 199th and fnal fight. During this, his 16th mission, he achieved a speed of 3,897 miles per hour and a peak altitude of 306,900 feet—slightly above 58 miles. Along with three other NASA X-15 pilots, he was later awarded astronaut wings for his achievement. For his service as a fight research pilot, he received NASA’s Distinguished Service Medal in 1997. michael J. adams Adams few the X-15 seven times. He reached a maximum speed of Mach 5.59 and a maximum altitude of 266,000 feet, which qualifed him as an Air Force astronaut. On November 15, 1967, Adams was at the controls when the third X-15 entered a hypersonic spin and broke up at approximately 62,000 feet. Adams was killed; the X-15-3 destroyed. Of the dozen pilots, eight few the X-15 to a height above 254,000 feet (50 mi) and qualifed to receive astronaut wings. X-15 program milesTones 1952 The national advisory committee on aeronautics, naca, increases research into fight up to mach 10 and to altitudes of 12 to 50 miles. 1954 naca teams establish the characteristics of a new research airplane, which subsequently becomes the X-15. 1954 naca, the u.s. army and u.s. navy sign a memorandum of understanding to create a "Joint project for a new high-speed research airpl ane." 1955 north american avi ation is chosen to develop three X-15 research airplanes. 1956 reaction motors is awarded contract to develop the Xlr99 rocket engine. 1957 construction begins of the X-15 airplanes. 1958 work on the X-15-1 is completed. 1959 first captive fight of the X-15 mated to the B-52. 1959 first glide fight of the X-15-1. 1960 first fight using the Xlr99 engine. 1961 first fight above mach 5. 1961 first fight above 200,000 feet. 1961 first fight above mach 6. 1961 first fight above 300,000 feet. 1963 first civilian fight above 50 miles. 1963 unof fcial world altitude record of 354,200 feet set on august 22. 1967 unof fcial world speed record of mach 6.70 (4,520 mph) set on oct ober 3. 1968 The fnal fight, piloted by Bill dana, takes place on oct ober 24. www.nasa.gov Bill Dana, pilot on the 199th and fnal X-15 mission. In the late 1960s and 1970s, Dana was the project pilot on the manned lifting body programandendedadistinguished career as chief engineer at Dryden Flight Research Center. THE X-15 MEGAGRAPHICS TEAM: AnthonySpringer(NASAHeadquarters),PeterMerlin(DrydenFlightResearch Center), Dennis R. Jenkins, Tony Landis (Dryden Flight Research Center), Karen L. Rugg (NASA Headquarters) The Pipeworks Design Collective: Paul Derby (research, writing), Simon Pipe (creative direction, project management), Cem Ceylan (design), Harriet Pellereau (3-D modeling) For more information: http://www.aeronautics.nasa.gov

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NASA

Transcript of North American X-15 Poster

Page 1: North American X-15 Poster

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journey of discovery, the X-15 became the fastest and highest-flying piloted winged airplane of its time. its discoveries set naSa on a direct course for the exploration of space.

To The edge of Ballistic the outer

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SenSational, iconic, groundbreaking. the X-15 hypersonic research airplane significantly extended the frontiers of flight. it was a program of outstanding engineering achievements, jaw-dropping performance characteristics, and extraordinary human endeavor. during a 15-year

354,200 ft highesTalTiTude aTTained forawinged aircrafT (ThaT’s 67 miles high!) andan achievemenT noT surpassed unTil 2004

NW-2008-09-195-HQ

1,325º f The peaK surface TemperaTure of a TesT panel on The X-15 during a mach 5 mission

4,520 mph Top speed ofmach 6.70 —anachievemenT unBroKen for 41 years

8-g The g-force eXperienced By X-15 piloTs on some flighTs during reenTry inTo earTh’s aTmosphere

awing and a prayer test pilot scott crossfield helped to design the ejection seat, which enabled “safe ejection at speeds up to mach 4, in any attitude and at any altitude up to 120,000 feet.” after the canopy was jettisoned, the seat fired upward and, once clear of the aircraft, deployed a pair of fold-out fins and telescoping booms for stabilization. a face-heater battery activated to keep the pilot’s visor clear of ice, and oxygen was supplied from two under-seat tanks. despite the seat’s sophistication, none of the pilots wanted to see it used on a mission.

t was arguably the most successful aeronautical research effort in history. Between June 1959 and october 1968, nasa’s X-15 hypersonic research flights rewrote the rule book of conventional flight and spawned an extraordinary legacy that lives on today.

the world’s first piloted vehicle designed to study the realms of hypersonic flight—an experimental aircraft of mind-boggling

performance—was conceived by a joint team from nasa, the u.s. air force, the u.s. navy and north american aviation.

the goal was to fly at mach 6—six times faster than the X-1 aircraft that exceeded the sound barrier a decade earlier. the team aimed to fly the X-15 at an altitude of 250,000 ft—nearly 50 miles above earth’s surface. By the time nasa test pilot Bill dana brought the 199th and final X-15 flight to a stop on the parched lake bed of edwards air force Base in california on october 24, 1968, these goals had been achieved.

the X-15 flew faster and higher than any other piloted winged vehicle other than the space shuttle. on separate flights, the X-15 reached mach 6.70 (4,520 mph) and 354,200 feet. the program could have broken every speed and altitude record in the books, but that was not the goal. the sole purpose of the X-15 was to enable research at hypersonic velocities and at the edge of space.

The legacy the X-15 program yielded a treasure trove of valuable data and fresh understanding. perhaps most critically, it provided a major technological stepping-stone to space.

the mercury, gemini, and apollo programs all benefited from the X-15 research and, every time a space shuttle returns from orbit, it does so using knowledge derived from the X-15.

the X-15 demonstrated for the first time that pilots could fly rocket-powered aircraft out of earth’s atmosphere, control them successfully in an airless environment, reenter the atmosphere and perform a precision landing at a predetermined site. in other words, it invented what eventually became the basic flight profile for a space shuttle mission.

Triumphs and Tragedy the achievements of the X-15 are breathtaking. not only did the aircraft create history with its speed and altitude, it gave birth to some amazing successes—the first extensive use of simulation as an engineering tool, first full-pressure suit for pilot protection in space, first application of hypersonic theory to a flight vehicle. the list goes on. however, the program also experienced its share of setbacks and one tragic loss.

on november 15, 1967, air force test pilot maj. michael J. adams reached 266,000 feet during a test flight. suddenly, his aircraft went into a hypersonic spin from which he could not recover. in spite of the pioneering nature of the program, his was the only fatality and aircraft loss.

in conTeXT “X”means“experimental.”the first“X”designation went to the Bell X-1, which, on october 14, 1947, became the first airplane to break the sound barrier in level flight. since then, more than 50 different major research designs have used the“X” designation. although not every“X”vehicle became a flying prototype, every design proved to be a highly valuable research tool for advancing knowledge of aerodynamics and astronautics.

nasa continues to invest in next-generation technologies to ensure that the legacy of the X-15 lives on.

whiTe lighTning the X-15a-2 (pictured above) was designed for maximum speed. two external tanks for liquid ammonia and liquid oxygen provided an extra 60 seconds of engine burn and, in theory, could power the rocket plane to speeds well in excess of mach 7. the white color of the aircraft was due to the application of an ablative coating designed to protect the structure from the high temperatures that would be generated at such speeds. the fuselage was extended by 29 inches to carry liquid hydrogen for a planned supersonic combustion ramjet (scramjet) that was flown in mockup form but never actually tested. in the hands of pilot pete knight, the X-15a-2 reached mach 6.70 (4,520 mph), the fastest flight of the X-15 program.

a servo-actuated “Ball nose” flow direction

sensorprovidedaccurate measurement of angle of attack and angle of

sideslipatsupersonicand hypersonic velocities.

pitot head

three-panels-thick windshield(heated with nitrogen gas to prevent frosting/fogging)

no. 2 eQuipment compartment

skylight hatch

fuse panel

lauXiliary power

units

iQuidnitrogentank (air conditioning andpressuriZation system)

l

liQuid oXygen tank vent

liQuid oXygen tank (engine oXidiZer)

helium tank (for engine propellant pressuriZation)

controlsystem thrusters

called inconel X , employed in a hot structurethatwas capaBle ofwithstandingtemperatures in eXcess of 1200° f.the Beams and spars of the wings and the ring structure of the fuselage were constructed from strong titanium-manganese alloy.

wing flap

wingattachmentstructure

ammonia tank (engine fuel)

hydrogen peroXide tank (engineturBopumppropellant)

movaBle upper vertical

staBiliZer

upper speed Brake

Xlr99-rm-1 rocket engine

heliumtank (for engine purge)

all-moving horiZontal

staBiliZer

ower vertical staBiliZer (Jettisoned Just Before landing)

retractaBle landing gear skids

Ballistic controlsystem

thrusters

no. 3 eQuipment compartment

helium tank (for pressuriZation) liQuid oXygen

tank filler

hydraulicsystem reservoirs

hydrogen peroXide tank (auXiliarypower unitandBallistic controlsystem propellant)

helium tank (auXiliary power unit propellant pressuriZation)

telemetry recorders

area for eXperiments

no. 1 eQuipmentcompartmentBallistic

controlsystemthrusters

half a million horsepower the power generated by the X-15’s Xlr99 rocket engine was awesome. the physical stress exerted on the human body was so high that test pilot milt thompson once joked that the X-15 was the only aircraft he had ever flown that made him glad when the engine quit.

developed and built by the reaction motors division of thiokol chemical, the Xlr99 could deliver up to 57,000 pounds of thrust, or the equivalent of over half a million horsepower. the propellants were liquid oxygen and anhydrous ammonia, fed into the engine by turbopumps at a flow rate of more than 13,000 pounds per minute.

the Xlr99 had a rated operating life of 1 hour, after which it could be overhauled and used again. the basic X-15 carried propellants for about 85 to 90 seconds of full-power flight, and the X-15a-2 carried propellants for more than 150 seconds of full-power flight.

early flights of the X-15 were powered by the reaction motors Xlr11—the same engine that powered the Bell X-1—which acted as an interim engine until development work on the Xlr99 was complete.

I

1 tank pressuriZation selecto

2 engine throttle

3 altimeter

4 airspeed/mach indicator

5 accelerometer

6 conventional center stick (moved the aerodynamic control surfaces)

7 vertical velocity indicator

8 system warning lights

9 canopy emergency Jettison handle

7 54

3

8

9

1

6

2

flying aT The edgeto protect the pilot and sensitive electronics from the ferocious heat of hypersonic flight, the pressurized aluminum cockpit and equipment bay were insulated from the outer inconel X shell by a radiation shield and insulation blanket.

the X-15 included one of the first inertial navigation systems (called a“stable platform”) to let the pilot know his precise position over the high range, and a sophisticated stability augmentation system to help him maintain precise control of the aircraft.

above earth’s atmosphere, reaction controls kept the aircraft stable. hand controllers in the cockpit were linked to small hydrogen peroxide thrusters at the nose for pitch and yaw control, and on each outer wing to control roll.

the most dangerous part of a mission was the descent. as the pilot switched from thruster control to traditional “stick-and-rudder”flying, the X-15 became a 15,000- pound unpowered hypersonic glider glowing red-hot as it decelerated from 4,000 mph to 200 mph. with only one shot at landing, there was simply no room for error.

The carrier aircrafT

Before the X-15 could negotiate any mission successfully, a mother ship had to carry the research airplane to high altitude since the X-15 did not have enough propellant to take off from the ground. a pair of mighty Boeing B-52 stratofortress aircraft took the X-15 under their wings. the nB-52a was dubbed“the high and mighty one”and the nB-52B“the challenger.”

the B-52 carried the X-15 to a launch altitude of approximately 45,000 feet. when the X-15 pilot hit the launch switch, the research airplane dropped away from the B-52, falling toward earth just until the rocket engine ignited and then accelerating to mach 5 or even mach 6.

the B-52/X-15 combination made 336 flights, including 199 successful launches of the X-15. of the others, 12 were planned“captive”missions in which the X-15 remained attached to the B-52 to check out various systems, and 125 flight attempts ended as aborts in which the X-15 remained safely under the B-52’s wing until the pair returned to edwards air force Base.

so successful were the mother ships that the nB-52B—better known as “nasa 008”—served for nearly 50 years until its retirement in december 2004. maintenance crews treated the venerable aircraft more like a classic car than an aging bomber. it ended its career as it began—in hypersonics.

during its last mission, the nasa 008 launched the unpiloted X-43a scramjet research vehicle on a flight that reached a velocity of mach 9.60.

full-pressure suiT�the full-pressure suit worn by X-15 pilots to protect them from the effects of high-altitude flight was revolutionary. previous pressure suits were cumbersome, virtually immobilized the pilot, and were mostly ineffective. fresh thinking was required.

the answer was a groundbreaking development by the david clark company that resulted in the mc-2 suit. the introduction of an inner nylon mesh called“link-net”radically improved mobility and provided much improved protection against the harsh environment.

the suit was integral to the pilot’s environment. it providedcooling and ventilation; supplied oxygen; and contained parachute harness, a microphone, earphones and pressureregulators. visors were heated for the same reason as car windshields—to prevent fogging.

a total of 36 X-15 flights used the original mc-2 suit, while the remainder used the newer a/p22s-2, also developed by the david clark company. each suit was custom-made for aparticular X-15 pilot. variants of this design would become the standard full-pressure suit used across all u.s. military andnasa programs.

it was all about acceleration. the B-52 carrier deceleration. the rest of the 8- to 12-minute aircraft traveled at 500 miles per hour and flight continued without rocket power. 45,000 feet when the X-15 pilot hit the launch on high-altitude missions, the pilot switch. a few seconds of freefall followed, experienced microgravity (“zero-g”) for nearly 2 and then the earth-shatteringly powerful minutes as the X-15 often soared past 300,000 57,000-pound Xlr99 rocket engine ignited feet. after glimpsing the curvature of earth, and catapulted the 33,000-pound X-15 toward the pilot experienced 5- to 8-g during reentry. mach 5. on high-speed missions, the X-15 reached an

the heart rate of an X-15 pilot ranged from altitude of 100,000 feet, which heated the skin 145 to 185 beats per minute as the adrenaline of the airplane until it glowed nearly red-hot. it surged. chest-to-back acceleration was 2-g could also accelerate from mach 5 to mach 6 in up to 4-g. at engine shutdown after nearly 90 an eye-watering six seconds. seconds thrust, he braced his helmet against a headrest in front of him for the 2-g of immediate

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flighT s of discovery X-15 achievemenTs The X-15’s legacy is quanTifiaBle noT JusT in Terms of speed or alTiTude achievemenTs, BuT also in Terms of whaT iT TaughT nasa and The american puBlic aBouT The fuTure possiBiliTies of hypersonic flighT. These achievemenTs include:

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» development of the first practical full-pressure suit for pilot protection in space

» first application of hypersonic theory andwind tunnel work to an actual flight vehicle

» development of computer-based simulation as an engineering and flight-planning tool

» development of a servo-actuated ball nose flow direction sensor for accurate measure-ment of angle of attack and sideslip angle atsupersonic and hypersonic speeds

» development of inertial flight data systems capable of functioning in high dynamic pressure and space environments

» demonstration of a pilot’s ability to controla rocket-boosted aerospace vehicle throughatmospheric exit

heroes of The hypersonic a total of 12 test pilots fromnasa, the u.s. air force, the u.s. navy and north american aviation flew the X-15.�

a. scott crossfield north american aviation’s crossfield was intimately involved in the design of the X-15. he piloted the first free flight on June 8, 1959, and the first powered flight on september 17. he completed 1 glide and 13 powered flights, reaching a maximum speed of mach 2.97 (1,960 mph). in July 1962, he was a joint recipient of the collier trophy, which was presented by president John f. kennedy.

Joseph a. walker walker made the first X-15 flight by a nasa pilot on march 25, 1960. he flew the airplane 25 times and made the highest flight (354,200 ft) of the program on august 22, 1963. he also flew the fastest flight (4,104 mph) of the basic X-15 configuration. in July 1962, he was a joint recipient of the collier trophy, which was presented by president John f. kennedy.

robert m. white air force test pilot white made 16 flights in the X-15 between april 13, 1960, and december 14, 1962. white was the first pilot to fly any aircraft faster than mach 4, 5 and 6, as well as the first to fly above 200,000 and 300,000 feet. he set the only official world record of the X-15 program when he flew to 314,750 feet on July 17, 1962, a fédération aéronautique internationale altitude record that still stands.

national aeronautics and space administration

forrest s. petersen petersen was the only navy pilot to fly the X-15. he made five flights in the aircraft at speeds of up to mach 5.30 (3,600 mph). petersen had the dubious distinction of making the program’s first uprange emergency landing on January 10, 1962, at mud lake. in July 1962, he was a joint recipient of the collier trophy, which was presented by president John f. kennedy.

John B. mcKay “Jack”mckay made 29 X-15 flights, reaching mach 5.65 on august 26, 1964, and a peak altitude of 295,600 feet on september 28, 1965. mckay was seriously injured on november 9, 1962, during an emergency landing at mud lake, but he recovered and flew 22 more X-15 flights. the airplane he crashed was rebuilt into the advanced X-15a-2.

robert a. rushworth rushworth flew the X-15 more times than any other pilot, logging 34 flights in total, including 2 with the interim Xlr11 engines. during these flights, he achieved mach 6.06 (4,018 mph) and 285,000 feet altitude. he was the second air force X-15 pilot (after Bob white) to attain an astronaut rating by flying the X-15 and was the first pilot to fly the advanced X-15a-2.

neil a. armstrong a name synonymous with aeronautical achievement, armstrong was actively engaged in both piloting and engineering aspects of the X-15. as a nasa test pilot, he completed seven X-15 flights, including the first flight of the mh-96 adaptive flight control system. armstrong would ensure his place in history on July 20, 1969, when he became the first human to land on the moon during the apollo 11 mission.

Joe h. engle engle completed 16 flights in the X-15, exceeding mach 5 on 10 of those flights. in June 1965, he climbed to an altitude of 280,600 feet, thereby earning his air force astronaut rating long before he joined the nasa astronaut corps. he accumulated the last of his 224 hours in space when he commanded the space shuttle discovery during sts-51i in 1985.

milton o. Thompson thompson began flying X-15s on october 29, 1963, and went on to complete 14 flights during the next 2 years, reaching mach 5.48 (3,712 mph) and a peak altitude of 214,100 feet. in 1962, thompson was selected as the sole nasa test pilot for the X-20 dyna-soar, the first viable reusable spacecraft. the dyna-soar program was canceled prior to its first flight.

william J. Knight “pete”knight flew the fastest flight of the program on october 3, 1967, when his advanced X-15a-2 reached mach 6.70 (4,520 mph). he also had more than his share of eventful flights. for instance, while climbing through 107,000 feet at mach 4.17 on June 29, 1967, he suffered a total electrical failure. knight calmly glided to a safe emergency landing.

william h. dana Bill dana was at the controls of the 199th and final flight. during this, his 16th mission, he achieved a speed of 3,897 miles per hour and a peak altitude of 306,900 feet—slightly above 58 miles. along with three other nasa X-15 pilots, he was later awarded astronaut wings for his achievement. for his service as a flight research pilot, he received nasa’s distinguished service medal in 1997.

michael J. adams adams flew the X-15 seven times. he reached a maximum speed of mach 5.59 and a maximum altitude of 266,000 feet, which qualified him as an air force astronaut. on november 15, 1967, adams was at the controls when the third X-15 entered a hypersonic spin and broke up at approximately 62,000 feet. adams was killed; the X-15-3 destroyed.

ofthedozenpilots,eightflew the X-15 to a height above 254,000 feet (50 mi) and qualified to receive astronaut wings.

X-15 program milesTones

1952 The national advisory committee on aeronautics, naca, increases research into flight up to mach 10 and to altitudes of 12 to 50 miles.

1954 naca teams establish the characteristics of a new research airplane, which subsequently becomes the X-15.

1954 naca, the u.s. army and u.s. navy sign a memorandum of understanding to create a "Joint project for a new high-speed research airplane."

1955 north american aviation is chosen to develop three X-15 research airplanes.

1956 reaction motors is awarded contract to develop the Xlr99 rocket engine.

1957 construction begins of the X-15 airplanes.

1958 work on the X-15-1 is completed.

1959 first captive flight of the X-15 mated to the B-52.

1959 first glide flight of the X-15-1.

1960 first flight using the Xlr99 engine.

1961 first flight above mach 5.

1961 first flight above 200,000 feet.

1961 first flight above mach 6.

1961 first flight above 300,000 feet.

1963 first civilian flight above 50 miles.

1963 unofficial world altitude record of 354,200 feet set on august 22.

1967 unofficial world speed record of mach 6.70 (4,520 mph) set on october 3.

1968 The final flight, piloted by Bill dana, takes place on october 24. www.nasa.gov

Bill dana, pilot on the 199th and finalX-15mission.inthelate1960s and 1970s, dana was the project pilot on the manned lifting body programandendedadistinguished career as chief engineer at dryden flight research center.

the X-15 megagraphics team:

anthonyspringer(nasaheadquarters),petermerlin(drydenflightresearch center), dennis r. Jenkins, tony landis (dryden flight research center), karen l. rugg (nasa headquarters)

The Pipeworks Design Collective: paul derby (research, writing), simon pipe (creative direction, project management), cem ceylan (design), harriet pellereau (3-d modeling)

For more information: http://www.aeronautics.nasa.gov