19 November 1952

Captain J. Slade Nash, U.S. Air Force, with the record setting North American Aviation F-86D Sabre. (U.S. Air Force)
Captain J. Slade Nash, U.S. Air Force, with the record setting North American Aviation F-86D Sabre. (U.S. Air Force)
The Henry De la Vaulx Medal.
The Henry De la Vaulx Medal.

19 November 1952: Captain James Slade Nash, U.S. Air Force, a test pilot at the Air Force Flight Test Center, Edwards Air Force Base, California, flew a North American Aviation F-86D-20-NA Sabre, 51-2945, to a Fédération Aéronautique Internationale (FAI) World Absolute Speed Record at the Salton Sea, in the Colorado Desert of southeastern California.

Operating out of NAS El Centro, Captain Nash flew four passes over a 3-kilometer course at an altitude of 125 feet (38 meters). The official average speed was 1,124.14 kilometers per hour (698.508 miles per hour).¹ He was awarded the FAI’s Henry de la Vaulx Medal for achieving the World Absolute Speed Record.

North American Aviation F-86D-20-NA Sabre 51-2945, holder of the World Absolute Speed Record, 1952. This was the second of 188 Block 20 aircraft built. (U.S. Air Force) (U.S. Air Force)

The Desert Sun reported:

Sabre-Jet Sets new World Speed Mark at Salton Sea

Record of 699.9 Mile Per Hour Established in Four Flights over Below Sea Level Course

     The desert area, few miles east of Palm Springs, was the setting for a new international airplane speed record last week when an F-86D Sabre jet roared over Salton Sea at 699.9 miles an hour. It was reported that in test runs previously the plane had exceeded 700 miles an hour.

     Risking his life to set the new record was Capt. Slade Nash, a 31-year-old Sioux City, Iowa man with three children. His wife, but not his three daughters, watched as Captain Nash barreled the swept-wing North American interceptor jet four times over the course, as close as 100 feet to the ground although he could have flown it at 328 feet.

      Nash had only to hit 676 miles an hour to shatter the previous world speed record set September 15, 1948, by Maj. Richard L. Johnson, air material command test pilot, at Edwards Air Force Base in an earlier Sabrejet—the F-86A. Johnson’s mark was 670.981 m.p.h. and Nash was required to fly 5 m.p.h. faster to set a new record.

     NASH’S SABRE jet carried a full rocket load. Adding hazard to the inherent danger of gunning a plane to near 700 m.p.h. was the low altitude below sea level—at when the run for record was made.

     Fuel requirements are much higher at sea level than at high levels and air pressure on the plane is about four times greater. In addition, aerodynamic problems of drag, buffet, stability and structural strength are greatly increased at sea level. However, low altitude and higher temperatures make higher speeds possible.

     CONDITIONS WERE NOT ideal for the test. Officials had hopes for 85-degree temperatures, but, at approximately 1:45 p.m., when the speed runs were made, the reading was only 75.5 degrees.

     Nash came within shouting distance of the speed of sound—about 760 m.p.h. at sea level. The speed of sound—called MACH 1—has many times been surpassed by jet planes in dives at high altitudes—in fact, most jet pilots pass this barrier at some time or another—but never under the considerably more difficult conditions of an official attempt to break the world speed record.

     NASH ALSO SET another record—being the first pilot to break a world speed record at below-sea-level altitudes. The Salton Sea is 235 feet below sea level and Nash’s Sabre jet was not believed to have gone above the sea level mark during his speed runs.

     Scene of the run was a desolate, gully-slashed barren shore land about a mile and a half below Durmid, a railroad crossing, and just south of the Riverside-Imperial county lines.

     About 100 newsmen, cameramen, manufacturers’ representatives and Air Force members were present. Head timer was C.S. Logsdon of Washington, D.C., director of the NAA Contest Division. Rules of the Federation Aeronautique Internationale and the Nationals Aeronautics [sic] Association (NAA) were followed.

     Official timing was made with high speed movie cameras. Processing of those films was necessary before the exact official speed of the run could be determined.

The Desert Sun, Palm Springs, California, Vol. XXVI, No. 17, Thursday, November 27, 1952, Page 2, Columns 1 and 2

The record-setting F-86D, 51-2945, was damaged in a ground collision with a Douglas RB-26C Invader, 44-35942, 29 October 1953, at K-14, Kinpo, Korea.

North American Aviation F-86D-1-NA Sabre 50-463, the eighth production aircraft. (North American Aviation, Inc.)

The North American Aviation, Inc., F-86D Sabre was an all-weather interceptor developed from the North American Aviation F-86 fighter. It was the first single-seat interceptor, and it used a very sophisticated—for its time—electronic fire control system. It was equipped with search radar and armed with twenty-four unguided 2.75-inch (69.85 millimeter) Mk 4 Folding-Fin Aerial Rockets (FFAR) rockets carried in a retractable tray in its belly.

The aircraft was so complex that the pilot training course was the longest of any aircraft in the U.S. Air Force inventory, including the Boeing B-47 Stratojet.

North American Aviation F-86D-20-NA Sabre 51-3045. (U.S. Air Force)

The F-86D was larger than the F-86A, E and F fighters, with a longer and wider fuselage. It was also considerably heavier. The day fighter’s sliding canopy was replaced with a hinged “clamshell” canopy. A large, streamlined radome was above the reshaped engine intake.

The F-86D Sabre was 40 feet, 3¼ inches (12.275 meters) long with a wingspan of 37 feet, 1½ inches (11.316 meters), and overall height of 15 feet, 0 inches (4.572 meters). The interceptor had an empty weight of 13,518 pounds (6,131.7 kilograms), and maximum takeoff weight of 19,975 pounds (9,060.5 kilograms). It retained the leading edge slats of the F-86A, F-86E and early F-86F fighters. The horizontal stabilizer and elevators were replaced by a single, all-moving stabilator. All flight controls were hydraulically boosted.

The F-86D was powered by a General Electric J47-GE-17 engine. This was a single-shaft, axial-flow turbojet with afterburner. The engine had a 12-stage compressor, 8 combustion chambers, and single-stage turbine. The J47-GE-17 was equipped with an electronic fuel control system which substantially reduced the pilot’s workload. It had a normal (continuous) power rating of 4,990 pounds of thrust (22.20 kilonewtons); military power, 5,425 pounds (24.13 kilonewtons) (30 minute limit), and maximum 7,500 pounds of thrust (33.36 kilonewtons) with afterburner (15 minute limit). (All power ratings at 7,950 r.p.m.) It was 18 feet, 10.0 inches (5.740 meters) long, 3 feet, 3.75 inches (1.010 meters) in diameter, and weighed 3,000 pounds (1,361 kilograms).

The maximum speed of the F-86D was 601 knots (692 miles per hour/1,113 kilometers per hour) at Sea Level, 532 knots (612 miles per hour/985 kilometers per hour) at 40,000 feet (12,192 meters), and 504 knots (580 miles per hour/933 kilometers per hour)at 47,800 feet (14,569 meters).

The F-86D had an area intercept range of 241 nautical miles (277 statute miles/446 kilometers) and a service ceiling of 49,750 feet (15,164 meters). The maximum ferry range with external tanks was 668 nautical miles (769 statute miles/1,237 kilometers). Its initial rate of climb was 12,150 feet per minute (61.7 meters per second) from Sea Level at 16,068 pounds (7,288 kilograms). From a standing start, the F-86D could reach its service ceiling in 22.2 minutes.

North American Aviation F-86D-60-NA Sabre 53-4061 firing FFARs
North American Aviation F-86D-60-NA Sabre 53-4061 firing FFARs. (U.S. Air Force)

The F-86D was armed with twenty-four 2.75-inch (69.85 millimeter) unguided Folding-Fin Aerial Rockets (FFAR) with explosive warheads. They were carried in a retractable tray, and could be fired in salvos of 6, 12, or 24 rockets. The FFAR was a solid-fuel rocket. The 7.55 pound (3.43 kilogram) warhead was proximity-fused, or could be set for contact detonation, or to explode when the rocket engine burned out.

The F-86D’s radar could detect a target at 30 miles (48 kilometers). The fire control system calculated a lead-collision-curve and provided guidance to the pilot through his radar scope. Once the interceptor was within 20 seconds of its target, the pilot selected the number of rockets to fire and pulled the trigger, which armed the system. At a range of 500 yards (457 meters), the fire control system launched the rockets.

Between December 1949 and September 1954, 2,505 F-86D Sabres (sometimes called the “Sabre Dog”) were built by North American Aviation. There were many variants (“block numbers”) and by 1955, almost all the D-models had been returned to maintenance depots or the manufacturer for standardization. 981 of these aircraft were modified to a new F-86L standard. The last F-86D was removed from U.S. Air Force service in 1961.

North American Aviation, Inc., F-86D-50-NA Sabre 52-10143.

James Slade Nash was born at Sioux City, Iowa, 26 June 1921. He was the older of two sons of Harry Slade Nash, a farmer, and Gertrude E. Parke Nash. He attended Iowa State University before entering the United States Military Academy, West Point, New York, 1 July 1942. He graduated with a Bachelor of Science degree and was commissioned as a Second Lieutenant, U.S. Army Air Corps, 5 June 1945.

Slade Nash completed flight training and was promoted to First Lieutenant, 29 April 1947. He served as a pilot with the 8th Photographic Reconnaissance Squadron at Johnson Air Base, Sayama, Japan, and the 82nd Reconnaissance Squadron at Yokota Air Base, near Tokyo, Japan, flying the Northrop RF-61C Reporter.

Northrop RF-61C  Reporter reconnaissance aircraft.

Nash began training as a test pilot at Wright-Patterson Air Force Base in September 1948. Captain Nash was then assigned to the Air Force Flight Test Center (AFFTC) at Edwards Air Force Base, and remained in that assignment for six years. He was involved in testing the delta-wing Convair XF-92 and YF-102, and flew many operational U.S. fighters and bombers.

After overseas staff assignments, Nash attended the Air Command and Staff College, Maxwell Air Force Base, Montgomery, Alabama, graduating July 1960. He served in the office of the Secretary of the Air Force until 1963, and as a liaison officer to the United States Congress. From August 1964 to October 1965, Nash attended the Army War College, Carlisle Barracks, Pennsylvania.

McDonnell F-101C Voodoo 56-0014, 81st Tactical Fighter Wing, RAF Bentwaters. circa 1965. (U.S. Air Force)
McDonnell F-101C-45-MC Voodoo 56-0014, 81st Tactical Fighter Wing, RAF Bentwaters. circa 1965. The three colors on the vertical fin identify this airplane as the wing commander’s aircraft. (U.S. Air Force)

Major Nash commanded the 92nd Tactical Fighter Squadron at RAF Bentwaters, Suffolk, England, and next was the deputy wing commander of the 81st Tactical Fighter Wing. Promoted to Lieutenant Colonel, he was assigned to Headquarters, U.S. Air Forces in Europe.

Colonel Nash served as vice commander of the 8th Tactical Fighter Wing at Ubon-Rachitani RTAFB, and flew 149 combat missions in the new gun-equipped McDonnell Douglas F-4E Phantom II.

MG James Slade, Nash, USAF, Chief, Military Assistance Advisory Group, republic of China, 1973.
MG James Slade, Nash, USAF, Chief, Military Assistance Advisory Group, Republic of China, 1973.

Nash was promoted to Brigadier General in 1969, serving as Vice Commander, Air Defense Weapons Center, Tyndall Air Force Base, Florida, and next, Vice Commander, Defense Special Projects Group. He was promoted to Major General on 1 September 1973, with date of rank retroactive to 1 February 1971.

General Nash served as Chief, Military Assistance Advisory Group to the Republic of China, and later, to Spain. From 1973 until 1976, Major General Nash was head of the Military Assistance Advisory Group to the United Kingdom. He retired from the Air Force in 1979.

During his military career, he was awarded the Distinguished Service Medal, Legion of Merit, Distinguished Flying Cross with Oak Leaf Cluster (two awards), and eight Air Medals. He was rated a command pilot with more than 6,000 flight hours.

Major General James Slade Nash died 19 March 2005 at the age of 84 years. He is buried at the United States Air Force Academy Cemetery, Colorado Springs, Colorado.

¹ FAI Record File Number 9867

© 2018, Bryan R. Swopes

19 November 1916

Ruth Bancroft Law at the controls of a Curtiss Pusher, ca. 1915. (U.S. Air Force)
Ruth Bancroft Law at the controls of a Curtiss Pusher, ca. 1915. (Lt. H.M. Benner/U.S. Air Force)

19 November 1916: Ruth Bancroft Law (Mrs. Charles Augustus Oliver) flew a Curtiss Pusher non-stop from Chicago, Illinois to Hornell, New York, a distance of 590 miles (949.5 kilometers). This exceeded the previous long distance flight record of 452 miles (727.4 kilometers) and set a new Aero Club of America record for distance.

Ruth Law departed Chicago at 8:25 a.m., in very windy conditions. After a very difficult flight, she landed at Hornell at 2:10 p.m., gliding the last two miles to a landing after the engine stopped from fuel starvation.

With her airplane refueled, Law took off from Hornell at 3:24 p.m. and flew on to Binghampton, New York, landing there at 4:20 p.m.

One the morning of 20 November, Law departed Binghampton at 7:23 a.m., finally arriving at Governor’s Island, New York City at 9:37:35 a.m. The total flight time for the 884-mile (1,422.66 kilometers) Chicago–New York City journey was 8 hours, 55 minutes, 35 seconds.

For a more detailed article about Ruth Law’s flight, please see:

http://www.ninety-nines.org/index.cfm/Ruth_Law.htm

Ruth Bancroft Law arrives at New York.
Ruth Bancroft Law arrives at New York City, 1916. (George Grantham Bain Collection, Library of Congress)

Ruth Bancroft Law was born at Lynn, Massachussetts, 21 March 1887. She was the third of four children of Frederick Henry Law and Sarah Bancroft Breed Law. She married Charles Augustus Oliver in 1907. He would act as her business manager during her aviation career.

Law (Mrs. Oliver) was taught to fly by Harry Nelson Atwood, chief instructor of the General Aviation Corporation, Saugus, Massachussetts, and Archibald A. Freeman, assistant instructor. She received her pilot’s certificate in November 1912.

Ruth Bancroft Law with her Wright Model B at Daytona Beach, Florida, 1916. (National Archives and Records Administration)
Ruth Bancroft Law with her Wright Model B at Daytona Beach, Florida, 1916. (National Archives and Records Administration)

Ruth Law enlisted in the Army 30 June 1917, after the United States entered World War I. Although it was her intention to serve as a pilot, she was not permitted to fly, but was assigned to the U.S. Army Accessions Command, to assist with recruiting and instruction. Law trained with the 38th Infantry Division at Camp Shelby, Mississippi. She served in Europe and held the non-commissioned officer rank of Sergeant.

Ruth Bancroft Law at Camp Shelby, Missippi, 1917. At the far right is Major General William H. Sage, with Mrs. Sage. Rutkh Law is fourth from right without a hat. (SunHerald)
Ruth Bancroft Law at Camp Shelby, Mississippi, 1917. At the far right is Major General William Hampden Sage, commanding officer, 38th Division, with his wife, Elizabeth Sage. Ruth Law is fourth from right, not wearing a hat. (Sun Herald)

Following the War, Law set several aviation records, did stunt flying and operated Ruth Law’s Flying Circus. Several sources say the she earned as much as $9,000 per week, approximately equivalent to $112,590 U.S. dollars in 2016. She retired from aviation in March 1922, saying that her husband was worried about her, and that she wanted to raise a family.

Mr. and Mrs. Oliver moved to Beverly Hills, California, living at 613, N. Roxbury Drive. Later, Mr. and Mrs. Oliver resided at 34 Rosewood Drive, San Francisco, California. Mr. Oliver died in 1947.

Ruth Bancroft Law Oliver died at Notre Dame Hospital, San Francisco, California, at 1:30 a.m., 1 December 1970, of a cerebro-vascular accident, at the age of 83 years. She was buried at Pine Grove Cemetery, Lynn, Massachussetts.

Ruth Law races Gaston Chevrolet, 1918. (Library of Congress via The Old Motor)
Ruth Law with her Curtiss Pusher races Gaston Chevrolet at the Canadian National Exhibition, Toronto, Ontario, Saturday, 29 June 1918. The race was to cover 5 laps. Chevrolet was given a 1-lap head start, and won the race by ½ a lap. (Library of Congress)

© 2016, Bryan R. Swopes

18 November 1978

The first Full Scale Development McDonnell Douglas F/A-18A-1-MC Hornet, Bu. No. 160775. (McDonnell Douglas Corporation)

18 November 1978: At Lambert Field, St, Louis, Missouri, McDonnell Douglas Corporation Chief Test Pilot John Edward (“Jack”) Krings, took the number one Full Scale Development (FSD) F/A-18A-1-MC Hornet, Bu. No. 160775, for its first flight. During the 50-minute test flight, Krings flew the Hornet to 24,000 feet (7,315 meters) before returning to STL.

The F/A-18 Hornet was developed for the United States Navy from the prototype Northrop YF-17, a competitor for a U.S. Air Force fighter program. (The rival General Dynamics F-16 was selected for production.) Initially, it was planned that there would be fighter variant, the F-18, and a ground attack version, the A-18. The Navy and manufacturers determined that a single airplane could perform both assignments. The Hornet was produced by McDonnell Douglas, with Northrop Corporation as the prime subcontractor.

The F/A-18 remains in production as the Boeing F/A-18 Block III Super Hornet. Current orders should keep the Hornet in production until 2025.

McDonnell Douglas F/A-18A-1-MC Hornet Bu. No. 160775 is on static display at Naval Air Warfare Center Weapons Division (NAWCWD) China Lake, near Ridgecrest, California.

McDonnell Douglas F/A-18 Full Scale Development aircraft, Bu. No. 160775.
Jack Krings

John Edward (“Jack”) Krings was born 2 April 1930 at Pittsburgh, Pennsylvania. He was the son of John J. Krings, a refrigeration salesman, and Jean Molamphy Krings. Jack Krings attended Central Catholic High School, in Pittsburgh, graduating in 1948. He then attended Louisiana State University, graduating in 1952 with a Bachelor of Science Degree in Chemistry and Physics, with a minor in mathematics. While at LSU, Krings played football and was a member of the Phi Chapter of the Sigma Nu fraternity.

On 27 December 1952, Krings married Miss Marilyn Dill at Kirkwood, a suburb of St. Louis. They would have several children, but later divorced.

After graduating from LSU, Krings joined the United States Air Force and was trained as a fighter pilot. He flew the Republic F-84 and served in combat during the Korean War. In 1956, Krings left the Air Force and was employed as an engineer at the McDonnell Corporation in St. Louis, Missouri. He continued to serve with the Air National Guard until 1966.

Krings was sent to the U.S. Naval Test Pilot School at NAS Patuxent River. He was a production test pilot and then moved on to development programs. He flew the F3H Demon, and F4H Phantom II. In 1962, Jack Krings was promoted to Chief Test Pilot. For his work as project pilot on the F-15A Eagle test program, Krings won the Iven C. Kincheloe Award of the Society of Experimental Test Pilots for 1975, and in 1979, the Jack Northrop Award and Ray E. Tenhoff Award for for the most outstanding technical paper. In 1986, the SETP presented Krings with its J.H. Doolittle Award for outstanding technical management of engineering achievement in aerospace technology.

On 27 March 1980, Kring married Joan Christian at St. Louis. It was the second marriage for both. They divorced 22 July 1988.

In 1985, Jack Krings retired from McDonnell Douglas. He then went to work in the U.S. Department of Defense as Director of Operational Test and Evaluation. He was twice warded the Department of Defense Medal for Distinguished Public Service. In 1989, he left the Pentagon and formed a consulting company, Krings Corporation.

Jack Kring married his third wife, Barbara Lynn McKemie, at Arlington, Virginia, 7 October 1988.

John Edward Krings died at Austin, Texas, 7 March 2014, at the age of 83 years. he was buried at Cook Walden Forest Oaks Cemetery in Austin.

© 2018, Bryan R. Swopes

18 November 1966

Major William J. Knight, U.S. Air Force, with the modified X-15A-2, 56-6671, at Edwards Air Force Base, California. Knight is wearing a David Clark Co. MC-2 full-pressure suit with an MA-3 helmet. (U.S. Air Force)
Major William J. Knight, U.S. Air Force, with the modified X-15A-2, 56-6671, at Edwards Air Force Base, California. Knight is wearing a David Clark Co. MC-2 full-pressure suit with an MA-3 helmet. (U.S. Air Force)

18 November 1966: On Flight 175 of the research program, Major William J. (“Pete”) Knight, U.S. Air Force, flew the newly-modified North American Aviation X-15A-2, 56-6671, to Mach 6.33 (4,261 miles per hour/6,857 kilometers per hour) at 98,900 feet (30,245 meters). This is just 11 years, to the day, since Pete Everest made the first powered flight in the Bell Aircraft Corporation X-2 rocketplane, with more than 6 times an increase in speed.

On this date, NASA made an attempt to launch two X-15s, -671 and -672, using the NB-52A 52-003 and NB-52B 52-008. However -672, the number three ship, had to abort the mission.

At the left, Boeing NB-52A 52-003 carries X-15 56-6670 while on the right, NB-52B 52-008 carries X-15 56-6671.(NASA)
At the left, Boeing NB-52A 52-003 carries X-15 56-6670 while on the right, NB-52B 52-008 carries X-15 56-6671.(NASA)

Balls 8, the NB-52B, flown by NASA test pilot Fitz Fulton and Colonel Joe Cotton, USAF, carried 56-6671 to the launch point over Mud Lake, Nevada, approximately 200 miles to the north of Edwards AFB. (This was the lake where -671 was severely damaged in an emergency landing, 9 November 1962. It was returned to North American to be rebuilt to the X-15A-2 configuration and returned to flight operation 19 months later.)

At 1:24:07.2 p.m. local time, Pete Knight and the X-15 were dropped from the pylon under the right wing of the B-52. He ignited the Reaction Motors XLR99-RM-1 and began to accelerate with its 57,000 pounds of thrust (253.549 kilonewtons).

Since this was to be a high temperature test flight, it was planned to fly no higher than 100,000 feet (30,480 meters). The denser atmosphere would result in greater aerodynamic heating of the rocketplane.

With the two external propellant tanks carrying an additional 1,800 gallons (6,814 liters) of liquid ammonia and liquid oxygen, the engine ran for 2 minutes, 16.4 seconds. The rocketplane had accelerated to Mach 2. The external tanks emptied in about 60 seconds and were jettisoned. The tanks were equipped with parachutes. They were recovered to be reused on later flights.

The X-15, now about 25,000 pounds (11,340 kilograms) lighter and without the aerodynamic drag of the tanks, continued to accelerate. At its highest speed, the rocketplane was travelling approximately 6,500 feet per second (1,981 meters per second), more than twice as fast as a high-powered rifle bullet. Its surface temperatures exceeded 1,200 °F. (649 °C.)

Knight landed the X-15 on Rogers Dry Lake at Edwards Air Force Base. The duration of this flight had been 8 minutes, 26.8 seconds.

The modified North American Aviation X-15A-2, 56-6671, with external propellant tanks mounted. (NASA)
The modified North American Aviation X-15A-2, 56-6671, with external propellant tanks mounted. (NASA)

© 2016, Bryan R. Swopes

18 November 1955

Major Frank Kendall Everest, Jr., U.S. Air Force, with the Bell X-2 supersonic research rocketplane, on Rogers Dry Lake at Edwards AFB, California, 1955. (U.S. Air Force)
Major Frank Kendall Everest, Jr., U.S. Air Force, with the Bell X-2 supersonic research rocketplane, on Rogers Dry Lake at Edwards AFB, California, 1955. (U.S. Air Force)

18 November 1955: Major Frank Kendall Everest, Jr., USAF, makes the first powered flight in the Bell X-2 research rocketplane, 46-674, at Edwards AFB, California. The rocketplane was airdropped from a Boeing EB-50D Superfortress, 48-096. Only one 5,000-lb. thrust rocket tube ignited, but that was enough to accelerate “Pete” Everest to Mach 0.992 (655.4 miles per hour/1,054.5 kilometers per hour) at 35,000 feet (10,668 meters).

The X-2 was a joint project of the U.S. Air Force and NACA (the National Advisory Committee on Aeronautics, the predecessor of NASA). The rocketplane was designed and built by Bell Aircraft Corporation of Buffalo, New York, to explore supersonic flight at speeds beyond the capabilities of the earlier Bell X-1 and Douglas D-558-II Skyrocket.

In addition to the aerodynamic effects of speeds in the Mach 2.0–Mach 3.0 range, engineers knew that the high temperatures created by aerodynamic friction would be a problem, so the aircraft was built from stainless steel and K-Monel, a copper-nickel alloy.

The Bell Aircraft Corporation X-2 was 37 feet, 10 inches (11.532 meters) long with a wingspan of 32 feet, 3 inches (9.830 meters) and height of 11 feet, 10 inches (3.607 meters). Its empty weight was 12,375 pounds (5,613 kilograms) and loaded weight was 24,910 pounds (11,299 kilograms).

The Bell X-2 being loaded into the EB-50D Superfortress "mothership" at Edwards AFB, California. (LIFE Magazine)
The Bell X-2 being loaded into the EB-50D Superfortress “mothership” at Edwards AFB, California. (LIFE Magazine)

The X-2 was powered by a throttleable two-chamber Curtiss-Wright XLR25-CW-1 rocket engine that produced 2,500–15,000 pounds of thrust (11.12–66.72 kilonewtons)

Rather than use its limited fuel capacity to take off and climb to altitude, the X-2 was dropped from a modified heavy bomber as had been the earlier rocketplanes. A four-engine Boeing B-50D-95-BO Superfortress bomber, serial number 48-096, was modified as the drop ship and redesignated EB-50D.

The launch altitude was 30,000 feet (9,144 meters). After the fuel was exhausted, the X-2 glided to a touchdown on Rogers Dry Lake at Edwards Air Force Base.

The Bell X-2 and Boeing EB-50D Superfortress in flight. (U.S. Air Force)
The Bell X-2 and Boeing EB-50D Superfortress in flight. (U.S. Air Force)

Pete Everest joined the United States Army Air Corps shortly before the United States entered World War II. He graduated from pilot training in 1942 and was assigned as a P-40 Warhawk pilot, flying combat missions in North Africa, Sicily and Italy. He was credited with shooting down two German airplanes and damaging a third.

Everest was returned to the United States to serve as a flight instructor. He requested a return to combat and was then sent to the China-Burma-India theater of operations where he shot down four Japanese airplanes. He was himself shot down by ground fire in May 1945. Everest was captured by the Japanese and suffered torture and inhumane conditions before being freed at the end of the war.

The Bell X-2 was dropped from a Boeing EB-50D Superfortress, 48-096. (U.S. Air Force)

After the war, Everest was assigned as a test pilot at Wright-Patterson Air Force Base, Ohio, before going west to the Air Force Flight Test Center at Edwards Air Force Base, California. At Edwards, he was involved in nearly every flight test program, flying the F-88, F-92, F-100, F-101, F-102, F-104 and F-105 fighters, the XB-51, YB-52, B-57 and B-66 bombers. He also flew the pure research aircraft, the “X planes:” the X-1, X-1B, X-2, X-3, X-4 and X-5. Pete Everest flew the X-1B to Mach 2.3, and he set a world speed record with the X-2 at Mach 2.9 (1,957 miles per hour, 3,149.5 kilometers per hour) which earned him the title, “The Fastest Man Alive.”

Pete Everest gives some technical advice to William Holden ("Major Lincoln Bond"), with Bell X-2 46-674, on the set of "Toward The Unknown", 1956.
Pete Everest gives some technical advice to actor William Holden (“Major Lincoln Bond”), with Bell X-2 46-674, on the set of “Toward The Unknown,” 1956. (Toluca Productions)

Frank Everest returned to operational assignments and commanded a fighter squadron, two combat crew training wings, and was assigned staff positions at the Pentagon. On 20 November 1963, Colonel Everest, commanding the 4453rd Combat Crew Training Squadron, flew one of the first two operational McDonnell F-4C Phantom II fighters from the factory in St. Louis to MacDill Air Force Base. In 1965, Pete Everest was promoted to the rank of brigadier general. He was commander of the Aerospace Rescue and Recovery Service. He retired from the Air Force in 1973 after 33 years of service. General Everest died in 2004.

Brigadier General Frank Kendall Everest, Jr., United States Air Force, 1920–2004. (U.S. Air Force)
Brigadier General Frank Kendall Everest, Jr., United States Air Force, 1920–2004. (U.S. Air Force)

© 2016, Bryan R. Swopes