Tag Archives: World Record for Speed Over a 15km/25km Straight Course

22 November 1961

Lieutenant Colonel Robert Bradford Robinson, Jr., U.S. Marine Corps, with the McDonnell YF4H-1 Phantom II, Bu. No. 142260, with which he set a world absolute speed record, 22 November 1961. Colonel Robinson is wearing a Goodrich Mark IV full-pressure suit for protection at high altitudes. (U.S. Navy)

22 November 1961: In recognition of the 50th Anniversary of Naval Aviation, a number of speed and altitude record attempts were planned, using the U.S. Navy’s new McDonnell YF4H-1 Phantom II fighter. On the morning of 22 November, Lieutenant Colonel Robert Bradford Robinson, Jr., United States Marine Corps, took off from Edwards Air Force Base on Operation Skyburner, an attempt to set a new World Absolute Speed Record. He was flying the second Phantom II built, Bu. No. 142260.

The Phantom carried three external fuel tanks for this flight. It had a 600-gallon (2,271.25 liter) centerline tank and two 370-gallon (1,400.6 liter) wing tanks. Robinson flew southeast toward NAS El Centro, then turned back to the northwest. Over the Salton Sea, he began to accelerate the YF4H-1 to build up speed for the record run over a measured twenty-mile course back at Edwards AFB. The Phantom’s two General Electric J79-GE-3A afterburning turbojets used a tremendous amount of fuel at full throttle and the centerline fuel tank was quickly emptied. Robinson jettisoned the empty tank over the Chocolate Mountain gunnery range. Continuing to accelerate, the two wing tanks were next jettisoned as they ran dry, this time at Bristol Dry Lake.

McDonnell YF4H-1 Phantom II, Bu. No. 142260, during Operation Skyburner, 22 November 1961. (U.S. Navy)

The Phantom entered the east end of the speed course in full afterburner. Having burned off more than 1,300 gallons of fuel, 142260 was much lighter now, and aerodynamically cleaner after dropping the external tanks. Robinson exited the west end of the 20-mile (32.2 kilometer) course in less than one minute.

Fédération Aéronautique Internationale rules require that a speed record must be made with two passes in opposite directions. The average speed of the two runs is the record speed. The Phantom was flying so fast that it covered another 105 miles (169 kilometers) before it could turn around. During the turn, it was still traveling at 0.9 Mach.

Robinson again put the engines in afterburner as he approached the course from the west. On the second run, the fighter was even lighter and its recorded speed was more than 1,700 miles per hour (2,736 kilometers per hour). The average of the two runs was calculated at 2,585.425 kilometers per hour (1,606.509 miles per hour.) This was the new FAI Absolute World Speed Record.¹

For his accomplishment, Lieutenant Colonel Robinson was awarded the Distinguished Flying Cross by Secretary of the Navy John B. Connally. The presentation took place on 25 November 1961 at Newport News, Virginia, during the commissioning of USS Enterprise CVA(N)-65.

McDonnell YF4H-1 Phantom II Bu. No. 142260 during Operation Skyburner, 1961. (U.S. Navy via FFRC Photo Collection)

In the next few weeks, the same YF4H-1 would establish a world record for sustained altitude—20,252 meters (66,444 feet).² Two years earlier, 6 December 1959, in Operation Top Flight, 142260 had established a world record for absolute altitude when it zoom-climbed to 98,557 feet (30,040 meters).³

Lieutenant Colonel Robert B. Robinson, Jr., U.S. Marine Corps, with the McDonnell YF4H-1 Phantom II Bu. No. 142260, with which he set a world absolute speed record, 22 November 1961. (U.S. Navy)

Robert Bradford Robinson, Jr., was born at Orange, California, 22 October 1923. He was the second of four children of Robert Bradford Robinson, a U.S. Postal Service mail carrier, and Golda Leutha Nordeen Robinson.

Robert B. Robinson. (Orange and White 1941)

Bob Robinson attended Orange Union High School, graduating in 1941. He participated in all varsity sports, and was selected to attend the Boys’ State leadership program. He earned a bachelor of science degree at Washington University, St. Louis, Missouri.

Robinson entered the United States Marine Corps on 26 August 1942. He received the wings of a Naval Aviator and was commissioned as a second lieutenant on 1 December 1943.

2nd Lieutenant Robinson married Miss Lavonne Jean David at Nueces, Texas, 23 December 1943. They would later have a son, Robert Bradford Robinson III (and a grandson, Robert Bradford Robinson IV)

During the Battle of Okinawa, Lieutenant Robinson flew the radar-equipped Grumman F6F-3N Hellcat night fighter with VMF(N)-543.

A Grumman F6F-3N Hellcat night fighter of VMF(N)-543, circa 1944. The radome is at the far end of the airplane’s right wing. (U.S. Navy)

Lieutenant Robinson was promoted to the rank of first lieutenant, 31 March 1945. Following World War II, Lieutenant Robinson was assigned to VMF-311, and became one of the first Naval Aviators to qualify in turbojet-powered aircraft. The squadron initially flew the Lockheed TO-1 Shooting Star (P-80), and later transitioned to the Grumman F9F Panther.

A Lockheed TO-1 Shooting Star  Bu. No. 33822 (P-80C 47-219) of VMF-311, circa 1948. (NNAM.1996.488.163.012)

Lieutenant Robinson was promoted to the rank of captain 1 April 1950. VMF-311 was sent to the Korean war zone in November 1950, initially operating from Yokosuka Air Base in Japan. The squadron flew close air support missions in support of the amphibious assault of Inchon, and at the Battle of the Chosin Reservoir. Captain Robinson returned to night fighter operations when he joined Marine All-Weather Squadron 513 (VMF(N)-513) on 13 January 1951. The unit which was equipped with Grumman F7F-3N Tigercats and Chance Vought F4U-5N Corsairs.

Two Grumman F9F-2 Panthers of VMF-311 being refueled at K-3, Republic of South Korea, circa 1951. The aircraft closest to the camera is an F9F-2B, Bu. No. 123602. (Department of Defense HD-SN-99-03071)

Captain Robinson was promoted to the rank of major, 31 December 1954. He completed the six-month course at the Naval Test Pilot School, NAS Patuxent River, Maryland, graduating in March 1959 (Class 21).

In 1963, Lieutenant Colonel Robinson retired from the Marine Corps after 20 years’ service. He was then employed as a test pilot for the McDonnell Aircraft Corporation at St. Louis, Missouri. He remained with the company for 30 years.

Mrs. Robinson died 7 February 1997, after 53 years of marriage. Bob Robinson later married Mrs. Julian Brady (née Elizabeth Catchings), the widow of a long-time friend.

Robert Bradford Robinson, Jr., died 28 September 2005 at McComb, Mississippi. He was buried at the Hollywood Cemetery in McComb.

¹ FAI Record File Number 9060

² FAI Record File Number 8535

³ FAI Record File Number 10352

© 2018, Bryan R. Swopes

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17 November 1954

Fairey Aviation Co., Ltd., Delta 2 WG774. (Unattributed)
Fairey Aviation Co., Ltd., Delta 2 WG774. (Wikipedia)
Lieutenant-Commander Lionel Peter Twiss, OBE, DSC and Bar. (The Telegraph)
Lieutenant-Commander Lionel Peter Twiss, O.B.E., D.S.C. and Bar. (The Telegraph)

17 November 1954: Lionel Peter Twiss, Chief Test Pilot for Fairey Aviation Company Ltd., was flying the company’s experimental supersonic airplane, the Fairey Delta 2, WG774, from the aircraft test center at RAF Boscombe Down, Salisbury, Wiltshire, England. This was the FD.2’s fourteenth flight.

When about 30 miles (48 kilometers) from the airfield and climbing through 30,000 feet (9,144 meters), the airplane’s fuel supply was interrupted and the engine flamed out.

Unwilling to lose a valuable research aircraft, Twiss decided to stay with the Delta 2 rather than ejecting, and he glided back to Boscombe Down, descending through a layer of cloud at 2,500 feet (762 meters). Without the engine running, the aircraft had insufficient hydraulic pressure to completely lower the landing gear and only the nosewheel strut locked in place. The FD.2 touched down at 170 miles per hour (274 kilometers per hour) and was seriously damaged.

WG774 was out of service for nearly a year. The wings had to be replaced and those which had originally been built for structural tests were used.

Damaged Fairey Delta 2 WG774 at Boscombe Down. (Prototypes.com)

For his effort to save a valuable research aircraft, Peter Twiss was awarded the Queen’s Commendation for Valuable Service in the Air. Notice of the award was published in The London Gazette, 22 February 1955, at Page 1094:

Lionel Peter Twiss, Test Pilot, Fairey Aviation Company Ltd. (Hillingdon, Middlesex.)

     For services when an aircraft, undergoing tests, sustained damage in the air.

Her Majesty and Prince Phillip look over the Fairey Delta 2 with Lieutenant-Commander Peter Twiss.
Her Majesty and Prince Phillip look over a Fairey Delta 2 with Lieutenant-Commander Peter Twiss in 1956. (Daily Mail)

On 10 March 1956, Peter Twiss flew WG774 to set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15km/25km Straight Course at an average speed over a 9-mile course, flown between Chichester and Portsmouth at and altitude of 38,000 feet (11,582 meters). Two runs over the course were made, with first averaging 1,117 miles per hour (1,798 kilometers per hour) and the second, in the opposite direction, was 1,147 miles per hour. (1,846 kilometers per hour). The FD.2 had averaged 1,822 Kilometers per hour (1,132 miles per hour)—Mach 1.731. ¹

Twiss had broken the previous record of 1,323.312 kilometers per hour (822.268 miles per hour) which had been set by Colonel Horace A. Hanes, U.S.Air Force, flying a North American Aviation F-100C Super Sabre over Edwards Air Force Base, California. ²

Test Pilot Peter Twist shakes hands with Robert L. Lickey, designer of the Fairey Delta 2. (The New York Times)
Test Pilot Lieutenant-Commander Lionel Peter Twiss, D.S.C. and Bar, shakes hands with Robert Lang Lickley, Chief Engineer of Fairey Aviation Co., Ltd., and designer of the Fairey Delta 2. (The New York Times)

Peter Twiss was the first British pilot, and the FD.2 the first British airplane, to exceed 1,000 miles per hour (1,609 kilometers per hour) in level flight. Twiss is also the last British pilot to have held a World Absolute Speed Record.

For his services as a test pilot, Lieutenant-Commander Lionel Peter Twiss, D.F.C. and Bar, was appointed Officer of the Most Excellent Order of the British Empire, 13 June 1957.

Fairey Delta 2 (FD.2) WG774. (Unattributed)
Fairey Delta 2 (FD.2) WG774, 13 March 1956. (Unattributed)

The Fairey Aviation Company, Ltd., Delta 2 WG774 (c/n F9421) is the first of two single-place, single-engine delta-wing research aircraft which had been designed and built to investigate transonic and supersonic speeds. It first flew 6 October 1953 with Chief Test Pilot Peter Twiss in the cockpit.

In its original configuration, the FD.2 is 51 feet, 7½ inches (15.735 meters) long with a wingspan of 26 feet, 10 inches (8.179 meters) and overall height of 11 feet (3.353 meters). The wings’ leading edge were swept to 59.9° with an angle of incidence of +1.5°. Ailerons and flaps were at the trailing edge and acted in place of elevators. In its original configuration it had an empty weight of approximately 11,000 pounds (4,990 kilograms) and the all-up weight at takeoff was 14,109 pounds (6,400 kilograms).

The FD.2 was powered by a Rolls-Royce Avon RA.28R afterburning turbojet engine which produced 9,530 pounds of thrust (42.392 kilonewtons), or 11,820 pounds (52.578 kilonewtons) with afterburner (“reheat”). This was a single-shaft axial-flow turbojet with a 15-stage compressor and 2-stage turbine. The RA.28 was 10 feet, 3.0 inches (3.124 meters) long, 3 feet, 5.5 inches (1.054 meters) in diameter, and weighed 2,869 pounds (1,301 kilograms).

WG774 and its sistership, WG777, were used for flight testing throughout the 1960s. WG774 was modified as a test aircraft to study various features of the planned British Aerospace Concorde. The landing gear struts were lengthened and the fuselage extended by six feet. It received a “drooped” nose section for improved pilot visibility during takeoff and landings. New wings were installed which had an ogee-curved leading edge. With these modifications WG774 was redesignated BAC 221. In this configuration, WG774 was tested to Mach 1.65 at 40,000 feet (12,192 meters).

WG774 was retired in the early 1970s. It is on display at the Fleet Air Arm Museum, Yeovilton, Somerset, England.

Fairey Aviation FD.2 WG7774. (Unattributed)
Fairey Aviation FD.2 WG774, 2 September 1955. (Unattributed)

Peter Lionel Winterton Twiss ³ was born 23 July 1921 at Lindfield, Sussex, England. He was the son of Colonel Dudley Cyril Twiss, M.C., a British Army officer, and Laura Georgina Chapman Twiss. Peter was educated at the Sherborne School, a prestigious boarding school for boys, in Dorset.

Midshipman Lionel Peter Twiss, Royal Navy Volunteer Reserve.

Twiss briefly worked as a tea taster for Brooke Bond & Company, but in 1939 enlisted as a Naval Airman, 2nd class, Royal Navy Volunteer Reserve. He trained at HMS St Vincent, a training school for the Fleet Air Arm at Gosport, Hampshire. He was appointed a Temporary Mishipman (Probationary), 26 August 1940. He was assigned to 771 Squadron, 27 January 1941, and was trained as a fighter pilot. Midshipman Twiss was commissioned as a Temporary Sub-Lieutenant (A), 23 July 1942.

Twiss was variously assigned to HMS Sparrowhawk, a Naval Air Station in the Orkney Islands, where he flew target tugs for gunnery training; HMS Daedalus, at Lee-on-Solent, Hampshire, England; and HMS Saker, a Royal Navy accounting base located in the United States.

Temporary Sub-Lieutenant (A) Lionel Peter Twiss, R.N.V.R., was assigned as the pilot of a Hawker Hurricane Mk.I with the Merchant Ship Fighter Unit. (Hurricanes could be launched by catapult from merchant ships to defend against Luftwaffe Focke-Wulf Fw 200 Condor reconnaissance bombers.)

A Hawker Hurricane Mk.IA, NJ L, mounted on a merchant ship’s catapult. (Lt. J.A. Hampton, RAF) © IWM (A 9421)

He next flew the Fairey Fulmar fighter with No. 807 Squadron from HMS Argus (I49), in support of Malta in the Mediterranean Sea. Sub-Lieutenant Twiss is credited with shooting down one enemy fighter and damaging a bomber. He was awarded the Distinguished Service Cross, 22 September 1942. He and his squadron transitioned to the Supermarine Seafire aboard HMS Furious (47) and were in action during the invasion of North Africa. He was awarded a Bar, denoting a second award, to his D.S.C., 16 March 1943.

Sub-Lieutenant Twiss, D.S.C. and Bar, was promoted to the rank of Temporary Lieutenant, 17 August 1943. After returning to England, Twiss was trained as a night fighter pilot. He flew the de Havilland DH.98 Mosquito with an RAF night fighter unit on intruder missions over France. In 1944 he shot down two more enemy airplanes.

Mosquito Mk.VI night intruder, 1944. © IWM (HU 107770)

Later in 1944, Twiss was sent to the United States to work with the British Air Commission. In this position, he was able to fly various U.S. fighter aircraft, including the turbojet-powered Bell P-59 Airacomet.

Lieutenant-Commander Twiss was in the third class of the Empire Test Pilots’ School and after graduation he was assigned to Fairey Aviation for duty as a test pilot.

With the end of World War II, Lieutenant-Commander Twiss left the Royal Navy and continued working as a civilian test pilot at Fairey. He became to the company’s chief test pilot in 1954.

Peter Twiss with a scale model of the Fairey Delta 2. (The Scotsman)

For his record-setting flight, in 1956 Twiss was awarded The Segrave Trophy of the Royal Automobile Club.

Lionel Peter Twiss,O.B.E., D.S.C. and Bar, at Buckingham Palace, 1957, following his investiture. He is accompanied by his step-daughter, Gillian, and his second wife, Vera Maguire Twiss.

In the Queen’s Birthday Honours, 13 June 1957, Lionel Peter Twiss, Esq., D.S.C., Chief Test Pilot, Fairey Aviation Company, Ltd.,, was appointed an Ordinary Officer of the Civil Division of the Most Excellent Order of the British Empire (O.B.E.). His investiture took place at Buckingham Palace.

In 1958, The Royal Aeronautical Society awarded its George Taylor Gold Medal to Peter Twiss.

Peter Twiss ended his career testing aircraft in 1959, having flown more than 4,500 hours in nearly 150 different aircraft. His autobiography, Faster than the Sun, was published by Macdonald, London, in 1963.

He later worked for Fairey Marine.

Peter Twiss drove the villain Morzeny’s speed boat in “From Russia With Love.”

Twiss made a brief appearance in the 1960 20th Century Fox motion picture, “Sink the Bismarck!” He portrayed the pilot of a Fairey Swordfish torpedo bomber which attacked the enemy battleship. In 1963, Peter Twiss appeared in the Eon Productions James Bond movie, “From Russia With Love.” He piloted one of the SPECTRE speedboats, which were chasing Bond and Tatiana Romanova.

Peter Twiss was married five times. His first wife was Constance A. Tomkinson.⁴ The marriage ended in divorce.

In the summer of 1950, Twiss married Vera Maguire at Wycombe, Buckinghamshire. They would have a daughter, Sarah. Their marriage also ended in divorce.

Mrs. Twiss III (Photographed by Mary Evans)

In June 1960, Twiss married Miss Cherry Felicity Huggins, a fashion model, actress, fashion magazine editor, pilot and race car driver, at Westminster, Middlesex, Their daughter Miranda was born in 1961. For a third time, Twiss’s marriage ended with a divorce. (Mrs. Twiss III would later marry Lord Charles Hambro, and become Lady Hambro.)

Twiss married his fourth wife, Mrs. Heather Danby (née Heather Linda Goldingham) at Gosport, Hampshire, on 4 November 1964. Mrs. Twiss IV died in 1988.

Finally, in December 2002, Peter Twiss married Jane M. de Lucey. They remained together until his death.

Lieutenant-Commander Lionel Peter Twiss, O.B.E., D.F.C. and Bar, died 31 August 2011 at the age of 90 years.

Lionel Peter Twiss, February 2002. (Dan Patterson/National Portrait Gallery NPG x126203)

¹ FAI Record File Number 8866

² FAI Record File Number 8867

³ England and Wales, Civil Registration Birth Index, July, August and September 1921, at Page 868. Birth registered as “Twiss, Peter L. W.” Mother’s maiden name, “Chapman.”

⁴ A marriage license was issued to Lionel P. Twiss and Constance A. Tomkinson in New York City, New York, U.S.A., 24 October 1944.

© 2018, Bryan R. Swopes

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31 October 1959

Colonel Georgy Konstantinovich Mosolov
Colonel Georgy Konstantinovich Mosolov

31 October 1959: At Joukovski-Petrovskoe, U.S.S.R., Гео́ргий Константи́нович Мосоло́в (Georgy Konstantinovich Mosolov), chief test pilot for Mikoyan-Gurevich, flew a prototype of the MiG-21 interceptor identified as the E-66, to set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15/25 Kilometer Straight Course. His speed averaged 2,388 kilometers per hour (1,483.8 miles per hour).¹

The МиГ-21 prototype identified by the symbol E-66  is known at the Mikoyan Design Bureau as the E-6\3. Its first flight took place in December 1958. It is powered by a Tumansky 11F-300 afterburning turbojet engine. (A Wikipedia article suggests that this airplane was rebuilt to different configurations several times, with designations changed accordingly.)

Mosolov’s FAI altitude record of 28 April 1961 was also flown in a MiG-21 prototype called E-66. (FAI Record File # 8661) Photographs and motion picture film of that airplane show it marked with red numerals “31” on the forward fuselage.

This photograph from the web site Wings of Russia is described as showing the Mikoyan-Gurevich Ye-6T/1 prototype, "31 Red", flown to a world record altitude, 28 April 1961.
The airplane in this  photograph from the web site “Wings of Russia” is described as showing the Mikoyan-Gurevich E-6T\1 prototype, “31 Red,” flown to a world record altitude by Colonel Mosolov, 28 April 1961.

Colonel Mosolov was interviewed for an article in Air & Space Smithsonian Magazine. He told writer Tony Reichhardt that after completing the speed record course, he was 125 miles (201 kilometers) from base at 44,000 feet (13,411 meters). Low on fuel, he shut down the turbojet engine and began a long glide. He twice unsuccessfully attempted to restart the engine for the landing, but was forced to glide all the way to the runway. After landing, the fuel system was drained. Only 8 liters (2.1 gallons) remained.

Colonel Georgy K. Mosolv, Soviet Air Forces. Hero of the Soviet Union.
Colonel Georgy Konstantinovich Mosolov, Soviet Air Forces. Hero of the Soviet Union.

Georgy Konstantinovich Mosolov was born 3 May 1926 at Ufa, Bashkortostan, Union of Soviet Socialist Republics. He was educated at the Central Aviation Club, where he graduated in 1943, and then went to the Special Air Forces School. In 1945 he completed the Primary Pilot School and was an instructor at the Chuguev Military Aviation School (Kharkiv, Ukraine). In 1953 Mosolov was sent to the Ministry of Industrial Aviation Test Pilot School at Ramenskoye Airport, southeast of Moscow, and 6 years later, to the Moscow Aviation Institute. He was a test pilot at the Mikoyan Experimental Design Bureau from 1953 to 1959, when he became the chief test pilot.

Georgy Mosolov set six world speed and altitude records. He was named a Hero of the Soviet Union, 5 October 1960.

On 11 September 1962, an aircraft that Colonel Mosolov was flying suffered a catastrophic compressor failure at Mach 2.15 and began to break apart. Severely injured, Mosolov ejected from the doomed airplane at Mach 1.78. He survived but his test flying career was over. His recovery took more than a year, and though he was able to fly again, he could not resume his duties as a test pilot.

Mikoyan-Gurevich Ye-152A, one of the MiG-21 prototypes flown by Georgy Mosolov.
This Mikoyan-Gurevich E-152A, NATO code name  “Flipper,” is one of the many MiG-21 prototypes flown by Georgy Mosolov.

¹ FAI Record File Number 9062

© 2017, Bryan R. Swopes

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29 October 1953

North American Aviation YF-100A Super Sabre 52-5754 during speed record attempt at the Salton Sea, 29 October 1953. (San Diego Air and Space Museum Archives)
North American Aviation YF-100A Super Sabre 52-5754 during a speed record attempt at the Salton Sea, 29 October 1953. (San Diego Air and Space Museum Archives)

29 October 1953: Lieutenant Colonel Frank Kendall (“Pete”) Everest, United States Air Force, flew a new prototype air superiority fighter, North American Aviation’s YF-100A Super Sabre, serial number 52-5754, over the 3 kilometer and 15 kilometer courses at the Salton Sea, in the Colorado Desert of southeastern California.

Flying four runs over the short course, Everest averaged 757.75 miles per hour (1,219.48 kilometers per hour). Although this was 4.80 miles per hour (7.725 kilometers per hour) faster than the FAI record set three weeks earlier by Lieutenant Commander James B. Verdin, U.S. Navy, with a Douglas XA4D-1 Skyray,¹ it was not fast enough to establish a new world record under FAI rules, which required that a new record exceed the previous record by 1%.

Lieutenant Colonel Frank Kendall Everest, Jr., United States Air Force.

Next came four speed runs over the 15/25 kilometer course. All runs were made with the Super Sabre flying within 100 feet (30 meters) of the ground. The official Fédération Aéronautique Internationale (FAI) average speed was 1,215.298 kilometers per hour (755.151 miles per hour)—0.99 Mach. ²

The course at the Salton Sea was used because its surface lies 235 feet (72 meters) below Sea Level. The denser air causes undesired transonic effects to occur at lower speeds, but the higher air temperatures help to delay them, allowing the pilot a greater margin of control during the speed record runs.

Lieutenant Colonel Frank K. Everest and the North American Aviation YF-100A Super Sabre, 52-5754, 29 October 1953. (San Diego Air and Space Museum Archives)

Frank Kendall (“Pete”) Everest, Jr., was born 10 Aug 1920, at Fairmont, Marion County, West Virginia. He was the first of two children of Frank Kendall Everest, an electrical contractor, and Phyllis Gail Walker Everest. Attended Fairmont Senior High School, Fairmont, West Virginia, graduating in 1939. He studied at Fairmont State Teachers College, also in Fairmont, West Virginia, and then studied engineering at the University of West Virginia in Morgantown.

Pete Everest enlisted as an aviation cadet in the United States Army Air Corps at Fort Hayes, Columbus, Ohio, 7 November 1941, shortly before the United States entered World War II. His enlistment records indicate that he was 5 feet, 7 inches (1.703 meters) tall and weighed 132 pounds (59.9 kilograms). He graduated from pilot training and was commissioned as a second lieutenant, Air Reserve, 3 July 1942.

Lieutenant Frank Kendall Everest, Jr. (schultzy)

2nd Lieutenant Everest married Miss Avis June Mason in Marion, West Virginia, 8 July 1942. they would have three children.

He was promoted to 1st Lieutenant, Army of the United States, 11 November 1942. He was assigned as a Curtiss-Wright P-40 Warhawk pilot, flying 94 combat missions in North Africa, Sicily and Italy. He was credited with shooting down two German airplanes and damaging a third. Everest was promoted to the rank of Captain, 17 August 1943.

Pete Everest with his Curtiss-Wright P-40 Warhawk, North Africa, circa 1943.

In 1944, 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 flew 67 missions and shot down four Japanese airplanes. Everest was appointed commanding officer of the 29th Fighter Squadron (Provisional), 5th Fighter Group (Provisional) at Chihkiang, China, in April 1945. 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. He was promoted to the rank of major, 1 July 1945. He was returned to the United States military 3 October 1945.

Following World War II, Major 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.

Major Everest was returned to the permanent rank of first lieutenant, Air Corps, 19 June 1947, with date of rank retroactive to 3 July 1945.

At Edwards, Pete Everest 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.” He was the test pilot on thirteen of the twenty X-2 flights.

In 1957, Lieutenant Colonel Everest was awarded the Harmon Trophy “for the most outstanding international achievements in the arts and/or science of aeronautics for the preceding year,” and also received the Octave Chanute Award “for an outstanding contribution made by a pilot to the art, science and technology of aeronautics.”

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, 1956. (U.S. Air Force)

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, Missouri, to MacDill Air Force Base, Tampa, Florida.

In 1965, Pete Everest was promoted to the rank of brigadier general. He was assigned as commander of the Aerospace Rescue and Recovery Service. General Everest retired from the Air Force in 1973 after 33 years of service.

Shortly after he retired from the Air Force, on 5 April 1973, Sikorsky Aircraft appointed General Everest its Chief Test Pilot. The manufacturer was developing the S-70 Black Hawk and S-76 commercial helicopters at the time.

During his military career General Everest was awarded the Air Force Distinguished Service Medal; Legion of Merit with two oak leaf clusters (three awards); Distinguished Flying Cross with two oak leaf clusters (three awards); Purple Heart; Air Medal with one silver and two bronze oak leaf clusters (seven awards); Air Force Commendation Medal with one oak leaf cluster (two awards); Presidential Unit Citation with two bronze oak leaf clusters (three awards); Air Force Gallant Unit Citation; Prisoner of War Medal; American Campaign Medal; European-African-Middle Eastern Campaign medal with four bronze stars; Asiatic-Pacific Campaign Medal with two bronze stars; World War II Victory Medal; National Defense Service Medal; Armed Forces Expeditionary Medal; Vietnam Service Medal; Air Force Longevity Service Award with one silver and two bronze oak leaf clusters (seven awards); Air Force Small Arms Expert Marksmanship Ribbon; and the Republic of Vietnam Campaign Medal with 1960– device. General Everest was rated as a Command Pilot, and a Basic Parachutist.

Brigadier General Frank Kendall Everest, Jr. United States Air Force (Retired), died at Tucson, Arizona, 1 October 2004 at the age of 84 years.

Brigadier General Frank Kendall Everest, Jr., United States Air Force

The North American Aviation F-100 Super Sabre was designed as a supersonic day fighter. Initially intended as an improved F-86D and F-86E, the “Sabre 45” soon developed into an almost completely new airplane.

The Super Sabre had a 49° 2′ sweep to the leading edges of the wings and horizontal stabilizer. The total wing area was 385.2 square feet (35.79 square meters). The wings had an angle of incidence of 0°, with no twist or dihedral. The ailerons were placed inboard on the wings and there were no flaps, resulting in a high stall speed in landing configuration. The horizontal stabilizer was moved to the bottom of the fuselage to keep it out of the turbulence created by the wings at high angles of attack. The F-100A had a distinctively shorter vertical fin than the YF-100A. The upper segment of the vertical fin was swept 49° 43′.

There were two service test prototypes, designated YF-100A, followed by the production F-100A series. The first ten production aircraft (all of the Block 1 variants) were used in the flight testing program.

The F-100A Super Sabre was 47 feet, 1¼ inches (14.357 meters) long with a wingspan of 36 feet, 6 inches (11.125 meters). With the shorter vertical fin, the initial F-100As had an overall height of 13 feet, 4 inches (4.064 meters), 11 inches (27.9 centimeters) less than the YF-100A.

North American Aviation Chief Test Pilot George S. Welch in the cockpit of the YF-100A, 52-5754, at Los Angeles International Airport. (North American Aviation, Inc.)
North American Aviation Chief Test Pilot George S. Welch in the cockpit of the YF-100A, 52-5754, at Los Angeles International Airport. (North American Aviation, Inc.)

The F-100A had an empty weight of 18,135 pounds (8,226 kilograms), and its maximum takeoff weight was 28,971 pounds (13,141 kilograms). It had an internal fuel capacity of 744 gallons (2,816 liters) and could carry two 275 gallon (1,041 liter) external fuel tanks.

The new air superiority fighter was powered by a Pratt & Whitney Turbo Wasp J57-P-7 engine. The J57 was a two-spool axial-flow turbojet which had a 16-stage compressor section (9 low- and 7 high-pressure stages) and a 3-stage turbine (2 high- and 1 low-pressure stages). Its continuous power rating was 8,000 pounds of thrust (35.586 kilonewtons). The Military Power rating was 9,700 pounds (43.148 kilonewtons) (30-minute limit). Maximum power was 14,800 pounds (43.148 kilonewtons) with afterburner (5-minute limit). The engine was 20 feet, 9.7 inches (6.342 meters) long, 3 feet, 3.9 inches (1.014 meters) in diameter, and weighed 5,075 pounds (2,303 kilograms). Later production aircraft used a J57-P-39 engine, which had the same ratings.

North American Aviation YF-100 Super Sabre 754 parked on the dry lake at Edwards Air Force Base, California. (U.S. Air Force)

The Super Sabre was the first U.S. Air Force fighter capable of supersonic speed in level flight.

The YF-100A had a maximum speed of 660 miles per hour (1,062 kilometers per hour) at 43,350 feet (13,213 meters). During testing, 52-5754 reached Mach 1.44 in a dive. The service ceiling was 52,600 feet (16,033 meters). Range with internal fuel was 422 miles (679 kilometers).

North American Aviation YF-100A Super Sabre 52-5754 over Edwards Air Force Base, California, 25 May 1953. (North American Aviation, Inc.)

The production F-100 was armed with four M39 20 mm autocannons, capable of firing at a rate of 1,500 rounds per minute. The ammunition capacity of the F-100 was 200 rounds per gun.

North American Aviation built 199 F-100A Super Sabres at its Inglewood, California, plant before production shifted to the F-100C fighter bomber variant. Approximately 25% of all F-100As were lost in accidents.

North American Aviation YF-100A Super Sabre 52-5754 banks away from a chase plane during a flight test. (U.S. Air Force)

¹ FAI Record File Number 9871

² FAI Record File Number 8868

© 2019, Bryan R. Swopes

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2 September 1953

Colonel J. Stanley Holtoner with his FAI record-setting F-86D Sabre, 51-6168. (FAI)

2 September 1953: Colonel J. Stanley Holtoner, U.S. Air Force, flew a production North American Aviation F-86D-35-NA Sabre, serial number 51-6168, to a Fédération Aéronautique Internationale (FAI) World Speed Record over a 100 kilometer course at Vandalia, Ohio, averaging 1,110.75 kilometers per hour (690.188 miles per hour).¹ Colonel Holtoner was the commanding officer of the Air Force Flight Test Center, Edwards Air Force Base, California. He was awarded the Thompson Trophy.

On the previous day, Captain Harold E. Collins flew another F-86D Sabre, 51-6145, setting an FAI World Speed Record over a 15 kilometer straight course of 1,139.219 kilometers per hour (707.878 miles per hour).²

North American Aviation F-86D-35-NA Sabre 51-6168, FAI World Speed Record holder. (FAI)

The The North American Aviation, Inc. F-86D Sabre was an all-weather interceptor developed from 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-1-NA Sabre 50-463, the eighth production aircraft. (North American Aviation, Inc.)

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 overal 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. A “clamshell” canopy replaced the sliding unit of earlier models.

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).

North American Aviation, Inc., F-86-50-NA Sabre 52-10143 banks toward the camera.

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.

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.

North American Aviation F-86D-60-NA Sabre 53-4061 firing a salvo of FFARs.

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.

After its service with the United States Air Force, F-86D 51-6168 was transferred to the Greek Air Force. In 2009, it was photographed, stripped and sitting on its belly, at Agrinion Airport (AGQ), Greece.

North American Aviation, Inc., F-86-50-NA Sabre 52-10143, right roll over Malibu CA

¹ FAI Record File Number 10428

² FAI Record File Number 8868

© 2018, Bryan R. Swopes

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