Tag Archives: Fighter Pilot

Medal of Honor, Major Richard Ira Bong, United States Army Air Forces

Major Richard Ira Bong, Air Corps, United States Army, Leyte, 12 December 1944. Major Bong is wearing the Medal of Honor. (U.S. Air Force)

17 December 1944: Major Richard Ira Bong, United States Army Air Corps, flying a Lockheed P-38 Lighting over San José on the Island of Mindoro, Commonwealth of the Philippines, shot down an enemy Nakajima Ki-43 Hayabusa (Allied reporting name, “Oscar”).

This was Bong’s 40th confirmed aerial victory and made him the leading American fighter ace of World War II. He is officially credited with 40 aircraft destroyed, 8 probably destroyed and 7 damaged.

Five days earlier, 12 December, during a ceremony at an American airfield on the Island of Leyte, Philippine Islands, General Douglas MacArthur, United States Army, had presented Major Bong the Medal of Honor.

An Associated Press reporter quoted the General:

“Of all military attributes, that one which arouses the greatest admiration is courage. It is the basis of all successful military ventures. our forces possess it to a high degree and various awards are provided to show the public’s appreciation. The Congress of the United States has reserved to itself the honor of decorating those amongst all who stand out as the bravest of the brave. It’s this high and noble category, Bong, that you now enter as I pin upon your tunic the Medal of Honor. Wear it as a symbol of the invincible courage you have displayed so often in mortal combat. My dear boy, may a merciful God continue to protect you is the constant prayer of your commander in chief.”

[On 18 December 1944, Douglas MacArthur was promoted to General of the Army, a five-star rank held by only nine other U.S. military officers. General MacArthur was the son of a Medal of Honor recipient, and had himself been twice nominated for the Medal for his actions during the occupation of Vera Cruz (1914) and the Meuse-Argonne Offensive (1918). He was awarded the Medal of Honor for his defense of the Philippines, 1941–42.]

General Douglas MacArthur talks with Major Richard I. Bong, 12 December 1944. (U.S. Air Force)
General Douglas MacArthur talks with Major Richard I. Bong, Leyte, Philippine Islands, 12 December 1944. (U.S. Air Force)

Richard Bong’s citation reads:

MEDAL OF HONOR

The President of the United States of America, in the name of Congress, takes pleasure in presenting the Medal of Honor to Major (Air Corps) Richard Ira Bong, United States Army Air Forces, for conspicuous gallantry and intrepidity in action above and beyond the call of duty while serving with the 49th Fighter Group, V Fighter Command, Fifth Air Force, in action in the Southwest Pacific area from 10 October to 15 November 1944.

Though assigned to duty as gunnery instructor and neither required nor expected to perform combat duty, Major Bong voluntarily and at his own urgent request engaged in repeated combat missions, including unusually hazardous sorties over Balikpapan, Borneo, and in the Leyte area of the Philippines. His aggressiveness and daring resulted in his shooting down eight enemy airplanes during this period.

General Orders: War Department, General Orders No. 90, December 8, 1944
Action Date: October 10 – November 15, 1944
Service: Army Air Forces
Rank: Major
Regiment: 49th Fighter Group, V Fighter Command
Division: 5th Air Force.

Dick Bong poses with "Marge," his Lockheed P-38J Lightning. A large photograph of his fiancee, Miss Marjorie Vattendahl, is glued to the fighter's nose.
Dick Bong poses with “Marge,” his Lockheed P-38J-15-LO Lightning, 42-103993, Lockheed serial number 2827. A large photograph of his fiancée, Miss Marjorie Ann Vattendahl, is affixed to the fighter’s nose.

Major Bong flew a number of different Lockheed P-38s in combat. He is most associated, though, with P-38J-15-LO 42-103993, which he named Marge after his fiancée, Miss Marjorie Ann Vattendahl, a school teacher from Poplar, Wisconsin.

Richard Bong had flown 146 combat missions. General George C. Kenney, commanding the Far East Air Forces, relieved him from combat and ordered that he return to the United States. He was assigned to test new production P-80 Shooting Stars jet fighters being built at Lockheed Aircraft Corporation’s Burbank, California plant.

On 6 August 1945, the fuel pump of the new P-80 Bong was flying failed just after takeoff. The engine failed from fuel starvation and the airplane crashed into a residential area of North Hollywood, California. Major Richard Ira Bong was killed.

Nakajima Ki-43 Type 1 Army Fighter (AvionsLegendaires.net)

The Nakajima Ki-43 Type 1 Hayabusa was a single-place, single-engine fighter manufactured by Nakajima Hikoki K.K. for the Imperial Japanese Army Air Service. The light weight fighter was very maneuverable and was a deadly opponent. It was identified as “Oscar” by Allied forces. The Ki-43 shot down more Allied airplanes during World War II than any other Japanese fighter.

The Ki-43 was 29.2 feet (8.90 meters) long, with a wingspan of 35.6 feet (10.85 meters) and height of 9 feet (2.74 meters). Its empty weight was 4,170 pounds (1,878 kilograms) and gross weight  was 5,500 pounds (2,495 kilograms).

The Ki-43 Type 1 Army Fighter was powered by an air-cooled, supercharged Nakajima Ha-115 Toku two-row, 14-cylinder radial engine which produced 925 horsepower at 9,350 feet (2,850 meters), 800 horsepower  at 20,000 feet (6,096 meters), and 1,105 horsepower at Sea Level for takeoff. The engine drove a three-bladed constant-speed propeller with a diameter of 9.2 feet (2.80 meters).

Nakajima Ki-43 Type 1 Army Fighter, called “Oscar” by the Allied forces. (The Java Gold’s Blog)

Compared to American fighters, the Oscar was lightly armed with just two synchronized 7.7 mm × 58 mm Type 89 or 12.7 mm × 81 mm Type 1 machine guns, or a combination of one 7.7 mm and one 12.7 mm gun. The 12.7 machine gun could fire explosive ammunition. (The Type 89 was a licensed version of the Vickers .303-caliber machine gun, while the design of the Type 1 was based on the Browning M1921 .50-caliber machine gun.)

The Oscar’s maximum speed was 295 miles per hour (475 kilometers per hour) at Sea Level, and 347 miles per hour (558 kilometers per hour) at 20,000 feet (6,096 meters). Its service ceiling was 37,100 feet (11,308 meters). The maximum range with a normal fuel load of 149 U.S. gallons (564 liters) was 1,180 miles (1,899 kilometers) at 1,500 feet (457 meters).

Lockheed P-38J-10-LO Lightning 42-68008, Lockheed serial number 2519. (Lockheed Martin)

The Lockheed P-38 lightning is a single-place, mid-wing, twin-engine fighter. It is an unusual configuration, with the cockpit, weapons and nose landing gear in a central nacelle, and engines, turbochargers, cooling system and main landing gear in outer “booms.” The airplane was originally designed by Clarence L. “Kelly” Johnson.

The P-38J is 37 feet, 10 inches (11.532 meters) long, with a wingspan of 52 feet, 0 inches (15.850 meters) and overall height of 9 feet, 9-11/16 inches (2.989 meters). The fighter has an empty weight of 12,700 pounds (5,761 kilograms) and maximum gross weight of 21,600 pounds (9,798 kilograms).

The P-38J was powered by two liquid-cooled, turbosupercharged 1,710.597-cubic-inch displacement (28.032 liter) Allison Engineering Company V-1710-F-17R and -F17L (V-1710-89 and -91, respectively) single overhead cam (SOHC) 60° V-12 engines with a continuous power rating of 1,100 horsepower at 2,600 r,p.m., to 30,000 feet (9,144 meters), and a takeoff/military power rating of 1,425 horsepower at 3,000 r.p.m. The counter-rotating engines drove 11 feet, 6 inches (3.505 meters) diameter, three-bladed Curtiss Electric full-feathering constant-speed propellers through a 2.00:1 gear reduction. The engines were 7 feet, 1.34 inches (2.168 meters) long, 3 feet, 0.75 inches (0.933 meters) high, 2 feet, 5.28 inches (0.744 meters) wide, and weighed 1,350 pounds (612 kilograms).

A flight of two camouflaged Lockheed P-38J Lightnings, circa 1943. Dick Bong is flying the closer airplane, P-38J-5-LO 42-67183. (Lockheed Martin)

The P-38J had a maximum speed of 420 miles per hour (676 kilometers per hour) at 26,500 feet (8,077 meters). The service ceiling was 44,000 feet (13,411 meters). Carrying external fuel tanks, the Lightning had a maximum range of 2,260 miles (3,637 kilometers).

P-38s were armed with one 20 mm Hispano M2 aircraft autocannon with 150 rounds of ammunition, and four air-cooled Browning AN-M2 .50-caliber machine guns with 500 rounds per gun. All guns are grouped close together in the nose and aimed straight ahead.

A Lockheed P-38 Lighning test fires its guns. (Lockheed Martin)

Between 1939 and 1945, Lockheed Aircraft Corporation built 10,037 P-38 Lightnings at Burbank, California. 2,970 of these were P-38Js.

Major Richard Ira Bong, Air Corps, United States Army. (Richard I. Bong Veterans Historical Center/National Endowment for the Humanities)

© 2018, Bryan R. Swopes

14 December 1931

Sir Douglas Robert Stewart Bader, 12 May 1970,by Godfrey Argent, 12 May 1970. (© National Portrait Gallery, London)
Group Captain Sir Douglas Robert Steuart Bader, C.B.E., D.S.O. and Bar, D.F.C. and Bar, F.R.Ae.S., D.L.,  photographed by Godfrey Argent, 12 May 1970. (© National Portrait Gallery, London)

“On 14 December 1931, Douglas Bader flew to Woodley airfield near Reading. After lunch someone said, ‘I bet you won’t roll at nought feet.’ Bader did, and the graceful little Bulldog ended up in a shapeless ball of twisted metal. After hovering at death’s door Bader lost both legs. At Cranwell he remembered the Commandant had admonished him, ‘The RAF needs men, not schoolboys.’ Now he was neither, and the RAF would not need him anymore.”

Duel of Eagles by Group Captain Peter Wooldridge Townsend, CVO, DSO, DFC and Bar, RAF, Castle Books, Edison, New Jersey, 2003. Chapter 6 at Page 82.

Left to right, Pilot Officer Douglas R.S. Bader, Flight Lieutenant Harry Day and Flying Officer Geoffrey Stephenson during training for the 1932 Hendon Airshow, with a Bristol Bulldog. (RAF Museum)
Left to right, Pilot Officer Douglas R.S. Bader, Flight Lieutenant Harry Day and Flying Officer Geoffrey Stephenson during training for the 1932 Hendon Airshow, with a Gloster Gamecock. (RAF Museum)

Pilot Officer Douglas Robert Steuart Bader, Royal Air Force, caught the wingtip of his Bristol Bulldog Mk.IIA, K-1676, and crashed at Woodley Aerodrome, approximately four miles east of Reading, Berkshire, England. The airplane was damaged beyond repair.

Bader suffered major injuries requiring amputation of his right leg, followed by amputation of his left leg several days later. He was fitted with prosthetic legs with which he was soon able to walk without assistance. Pilot Officer Bader was medically retired and received a 100% disability pension.

Bristol Bulldog Mk.IIA K-1676. This is the airplane that Douglas Bader was flying when he crashed at Woodley, 14 December 1931. (Royal Air Force)
Bristol Bulldog Mk.IIA K-1675. This is a sister ship of the airplane that Douglas Bader was flying when he crashed at Woodley Aerodrome, 14 December 1931. (Royal Air Force)

In 1939, feeling that war with Germany was imminent, Bader applied to the Air Ministry for reinstatement. He was turned down, but was told that if there was a war his request might be reconsidered.

The Air Ministry did reconsider Douglas Bader’s request for reinstatement and after a medical evaluation and other tests, he was sent to refresher flight training where he was evaluated as “Exceptional,” a very rare qualification.

A page from Douglas bader's pilot log book, showing his "exceptional' evaluation. (Royal Air Force Museum)
A page from Douglas Bader’s pilot log book, showing his “Exceptional” evaluation. (Royal Air Force Museum)

Group Captain Sir Douglas R. S. Bader, Royal Air Force, C.B.E., D.S.O. and Bar, D.F.C. and Bar, F.R.Ae.S., D.L., a legendary fighter pilot of the Royal Air Force during World War II, was born at St. John’s Wood, London, England. He joined the Royal Air Force in 1928 as a cadet at the Royal Air Force College Cranwell and was commissioned as a Pilot Officer in July 1930.

Credited with more than 20 aerial victories while flying Hawker Hurricane and Supermarine Spitfire fighters, Bader was himself shot down while flying his Spitfire Mk Va, serial W3185, marked “D B”. His prosthetic legs caught in the cockpit and made it difficult for him to escape, but he finally broke free and parachuted to safety.

Bader was captured and held as a prisoner of war. He was initially held at a hospital in occupied France and it was there that he met and became a life long friend of Adolf Galland, also a legendary fighter pilot—but for the other side! After arrangements were made for replacement legs, Bader escaped. He was recaptured and taken to the notorious Offizierslager IV-C at Colditz Castle where he was held for three years.

Prisoners of War held at Colditz Castle, a maximum security prison during World War II. Squadron Leader Douglas Bader is seated, center.

Douglas Bader is the subject of Reach For The Sky, a biography by Paul Brickhill, and a movie based on that book which starred Kenneth More.

Sir Douglas was invested Knight Bachelor, 12 June 1976, for his service to the disabled. He died suddenly of a heart attack, 5 September 1982.

Douglas Bader with a Hawker Hurricane of No. 242 Squadron.
Douglas Bader with a Hawker Hurricane of No. 242 Squadron, September 1940. Photograph by F/O S. A. Devon, Royal Air Force. © IWM (CH 1406)

The Bristol Type 105 Bulldog was a single-place, single-engine biplane fighter which served with the Royal Air Force from 1928 to 1938. It was constructed of a riveted framework of rolled steel strips. The forward fuselage was covered with light weight sheet metal, while the wings and aft fuselage were covered with doped fabric. The Bulldog Mk.IIA was 25 feet, 2 inches (7.671 meters) long with a wingspan of 33 feet, 10 inches (10.312 meters) and height of 8 feet, 9 inches (2.667 meters). It had and empty weight of 2,222 pounds (1,008 kilograms) and maximum takeoff weight of 3,660 pounds (1,660 kilograms).

The Bristol Bulldog Mk.IIA was powered by an air-cooled, supercharged, 1,752.79-cubic-inch-displacement (28.72 liter) Bristol Jupiter VIIF nine-cylinder radial engine which was rated at 440 horsepower up to 12,000 feet (3,658 meters). This was a left-hand tractor engine which drove a wooden two-bladed fixed-pitch propeller through a 2:1 gear reduction.

The airplane had a maximum speed of 174 miles per hour (280 kilometers per hour) at 10,000 feet (3,048 meters) and a service ceiling of 29,300 feet (8,931 meters).

The Bristol Bulldog Mk.IIA was armed with two synchronized Vickers .303-caliber machine guns with 600 rounds of ammunition per gun.

Bristol Bulldog Mk.IIA K-2227, the same type airplane flown by Pilot Officer Bader when he crashed 14 December 1931. K-2227 is in the collection of the Royal Air Force Museum. (Unattributed)
Bristol Bulldog Mk.IIA K-2227, the same type airplane flown by Pilot Officer Bader when he crashed 14 December 1931. K-2227 is in the collection of the Royal Air Force Museum. (Royal Air Force)

© 2018, Bryan R. Swopes

13 December 1951

Major George Andrew Davis, Jr., United states Air Force, 334th Fighter Interceptor Squadron, 4th Fighter Interceptor Wing, Korea, 1951. (U.S. Air Force)
Major George Andrew Davis, Jr., United States Air Force, Commanding Officer, 334th Fighter Interceptor Squadron, 4th Fighter Interceptor Wing, Korea, 1951. (U.S. Air Force)

13 December 1951: Major George Andrew Davis, Jr., United States Air Force, commanding officer of the 334th Fighter Interceptor Squadron, 4th Fighter Interceptor Wing, flying a North American F-86E-10-NA Sabre, serial number 51-2752, led his unit on two “MiG Sweeps.”

Film from the gun camera of Major Davis’ F-86E Sabre 51-2752 shows a MiG 15 smoking after being hit, 13 December 1951. (U.S. Air Force)
Film from the gun camera of Major Davis’ F-86E Sabre 51-2752 shows a MiG 15 smoking after being hit, 13 December 1951. (U.S. Air Force)

During the mid-day fighter sweep, the 334th encountered Mikoyan Gurevich MiG 15 fighters of the 18th GIAP, 303rd IAD,  Voyenno-Vozdushnye Sily (the Soviet Air Force), and an air battle ensued. Major Davis was credited with shooting down two of the Russian fighters. The pilot of one of the MiGs, I.A. Gorsky, was killed. The identity and fate of the second Soviet pilot is not known.

During a second sweep in mid-afternoon, George Davis and the 334th again encountered enemy MiG 15s of the 40th Regiment, 14th Division, of the Peoples Liberation Army Air Force (Chinese Air Force). At 3:52 p.m. (1352) Davis shot down one of the Chinese MiG 15s. One minute later, he shot down another, his fourth aerial victory for the day.

These frames of film from the gun camera of Davis’ F-86 Sabre show a MiG 15 trailing smoke after being hit by the Sabre’s six .50-caliber machine guns. Chinese sources confirmed the loss of two MiG 15s, but again, the identities of the pilots and whether or not they survived is not known.

This North American Aviation F-86E-10-NA Sabre, 51-2849, seen here in flight over Edwards Air Force base, california, is the same type fighter that was flown by Major George Davis, 13 December 1951. (U.S. Air Force)
This North American Aviation F-86E-10-NA Sabre, 51-2849, seen here in flight near Edwards Air Force Base, California, is the same type fighter that was flown by Major George A. Davis, Jr., 13 December 1951. (U.S. Air Force)

© 2015, Bryan R. Swopes

12 December 1957

Major Adrian E. Drew, U.S. Air Force, 1920–1985. (Photograph courtesy of Neil Corbett, Test & Research Pilots, Flight Test Engineers)

12 December 1957: Major Adrian Eason Drew, U.S. Air Force, commanding officer, 481st Fighter Bomber Squadron, 27th Fighter Bomber Wing, Tactical Air Command, set a new Fédération Aéronautique Internationale (FAI) absolute speed record over the 15/25 kilometer course at Edwards Air Force Base, California.¹ Major Drew flew a modified McDonnell F-101A-5-MC Voodoo, serial number 53-2426.

The Voodoo, the ninth production F-101A, had been bailed to Pratt & Whitney by the Air Force to test a new J57-P-55 afterburning turbojet engine intended for the F-101B Voodoo, and it was redesignated JF-101A. The new engine produced 16,000 pounds of thrust with afterburner. The modified aircraft had longer jet exhaust tubes, and air scoops were installed in the belly to provide additional cooling air for the afterburners.

McDonnell JF-101A Voodoo 53-2426, takes off at Edwards Air Force Base on Operation Fire Wall, 12 December 1957. (U.S. Air Force)
McDonnell JF-101A Voodoo 53-2426, takes off at Edwards Air Force Base on Operation Fire Wall, 12 December 1957. (U.S. Air Force)
Thompson Trophy. (NASM)

At 39,000 feet (11,887 meters), Major Drew accelerated for 65 miles (105 kilometers) before entering the 10.1 statute mile (16.25 kilometers) course. He made one pass in each direction. Actual time on course, each way, was 29.8 seconds. The official average speed for the two passes is 1,943.5 kilometers per hour (1,207.64 miles per hour). Although the air temperature was -79 °F. (-62 °C.), frictional heating brought the Voodoo’s skin temperature to 190 °F. (88 °C.), high enough to blister the airplane’s paint.

Major Drew was awarded the Distinguished Flying Cross and the Thompson Trophy for 1957.

Major Adrian E. Drew, 481st Fighter Bomber Squadron, 27th Fighter Bomber Wing, U.S. Air Force, at Edwards AFB, 12 December 1957. (U.S. Air Force via Jet Pilot Overseas)
Major Adrian E. Drew, U.S. Air Force, at Edwards AFB, 12 December 1957.  At right is McDonnell Aircraft Corporation test pilot William S. Ross. In 1986, Ross was appointed president of the Aircraft Division of McDonnell Douglas Corporation. (U.S. Air Force via Jet Pilot Overseas)

Adrian Eason Drew was born 8 October 1920 in Georgia, the first of six children of John Robert Drew, a farmer, and Ada Elma Eason Drew.

After one year of college, Adrian Drew enlisted as a private in the U.S. Army Air Corps, 31 March 1942, at Fort McClellan, Alabama. He was 5 feet, 8 inches (1.73 meters) tall and weighed 143 pounds (64.9 kilograms).

On 14 November 1942, Drew married Miss Sarah B. Kaylor in Pinellas County, Florida. They would have three daughters, Nancy, Bonnie and Jo Anne.

Colonel Drew was a combat pilot during World War II, the Korean War and the Vietnam War. He commanded the 309th Strategic Fighter Squadron from January to October 1955, flying the Republic F-84 Thunderjet. In August 1957, he became the first commanding officer of the 481st Fighter Bomber Squadron at Bergstom Air Force Base,  Austin, Texas. Lieutenant Colonel Drew commanded the 354th Tactical Fighter Squadron at George Air Force Base, California, from 1962 to 1964, flying the Republic F-105D Thunderchief, and briefly commanded the 355th Tactical Fighter Wing.

Two weeks before a scheduled promotion to Brigadier General, Colonel Drew suffered a major heart attack and was forced to retire from the Air Force. He died 27 July 1985 at the age of 64 years. He was buried at Shawnee View Gardens Cemetery, Cumming, Georgia.

McDonnell JF-101A Voodoo 53-2426, holder of the World Absolute Speed Record, 1957. (U.S. Air Force)

The McDonnell F-101 Voodoo was originally designed as a single-seat, twin-engine long range bomber escort, or “penetration fighter” for the Strategic Air Command, but was developed as a fighter bomber and reconnaissance airplane. The Voodoo first flew 29 September 1954, and the first F-101A was delivered to the Air Force 2 May 1957.

The F-101A was 67 feet, 5 inches (20.549 meters) long with a wingspan of 39 feet, 8 inches (12.090 meters). It was 18 feet (5.486 meters) high. The Voodoo weighed 24,970 pounds (11,245 kilograms) empty and had a maximum takeoff weight of 50,000 pounds (22,680 kilograms).

The standard F-101A was equipped with two Pratt & Whitney J57-P-13 afterburning turbojet engines. The J57 was a two-spool axial-flow turbojet which had a 16-stage compressor (9 low- and 7 high-pressure stages), and a 3-stage turbine (1 high- and 2 low-pressure stages). The J57-P-13 was rated at 10,200 pounds of thrust (45.37, and 15,800 pounds (70.28 kilonewtons) with afterburner.

The J57-P-55 engines installed in the JF-101A were rated at 10,700 pounds of thrust (49.60 kilonewtons), and 16,900 pounds (75.18 kilonewtons) with afterburner. They were 20 feet,  11.93 inches (6.399 meters) long, 3 feet, 4.5 inches (1.029 meters) in diameter, and weighed 5,215 pounds (2,365 kilograms).

The maximum speed of the F-101A was 1,009 miles per hour (1,624 kilometers per hour) at 35,000 feet (10,668 meters). Its service ceiling was 55,800 feet (17,008 meters). It carried 2,341 gallons (8,862 liters) of fuel internally. With external tanks, the fighter bomber had a maximum range of 2,925 miles (4,707.3 kilometers).

The F-101A was armed with four 20mm Pontiac M39 single-barreled revolver cannon, with 200 rounds per gun. It could carry a Mark 28 bomb on a centerline mount.

McDonnell JF-101A Voodoo 53-2426 is on static display at Cannon Air Force Base, New Mexico.

McDonnell JF-101A Voodoo 53-2426, FAI World Speed Record Holder and Thompson Trophy winner, Operation Fire Wall, landing at Edwards Air Force Base, 12 December 1957. (U.S. Air Force)
McDonnell JF-101A Voodoo 53-2426, FAI World Speed Record Holder and Thompson Trophy winner, Operation Fire Wall, landing at Edwards Air Force Base, 12 December 1957. (U.S. Air Force)

A McDonnell Aircraft Corporation film about Operations Sun Run and Fire Wall is available of YouTube:

¹ FAI Record File Number 9064

© 2017, Bryan R. Swopes

11 December 1959

Lieutenant General Joseph H. Moore (1914–2007)
Lieutenant General Joseph H. Moore, United States Air Force

11 December 1959: Brigadier General Joseph H. Moore, U.S. Air Force, Wing Commander, 4th Tactical Fighter Wing at Seymour Johnson Air Force Base, North Carolina, set a Fédération Aéronautique Internationale (FAI) World Speed Record when he flew a Republic F-105B-20-RE Thunderchief, serial number 57-5812, over a closed 100-kilometer (62.137 miles) closed course at Edwards Air Force Base, California. The Thunderchief averaged 1,878.67 kilometers per hour (1,167.35 miles per hour).¹ General Moore’s fighter bomber was a standard production aircraft and it was armed with a full load of ammunition for the M61 cannon.

FAI Record File Num #8873 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 100 km without payload
Performance: 1 878.67 km/h
Date: 1959-12-11
Course/Location: Edwards AFB, CA (USA)
Claimant Joseph H. Moore (USA)
Aeroplane: Republic F-105B
Engine: 1 Pratt & Whitney J-75

U.S. Air Force General Claims Air Speed Record Of 1,216 MPH

     LOS ANGELES (UPI)—Brig. Gen. Joseph H. Moore, a grandfather twice over, yesterday claimed a new world air speed record of 1,216 mph for the U.S. Air Force.

     Piloting a Republic F-105 Thunderchief jet, combat equipped, Moore broke the French record of 1,100.426 mph ² over a 100-kilometer closed course at Edwards Air force Base Friday.

     Moore emphasized at a press conference yesterday morning at International Airport here that the new mark has not yet been officially verified by the National Aeronautic Association.

      HE SAID he would attempt the flight again if the NAA does not recognize the new mark.

The general, a combat pilot with 100 missions during World War II who holds many decorations, said he broke the record twice Friday. His “slowest” speed was 1,170 miles an hour, some 70 miles an hour over the French record.

The record was run over the closed course which measured 100 kilometers, or 62.14 miles. He made most of the run at an altitude of 38,000 feet. The French run was made at about 2,500 feet,

     MOORE, 40, soft spoken with a faint Southern drawl, was met at the airport yesterday by his son, 1st Lt. Joseph Moore, a gunnery instructor with the Air Force at Williams Air Force Base, Ariz.

     The general stressed that his plane was a production model, equipped with ammunition and cannon just as it would be in combat. He said that some of the plane’s instruments had been removed to make room for scientific equipment.

     According to Moore, he actually hit a top speed of 1,400 miles an hour in “coming through the gate” at the end of his run around the circular course, about which he was guided by radio and scientific instruments.

The Arizona Republic, Sunday, December 13, 1959, Page 16, Columns 1-3

Republic F-105B-1-RE Thunderchief 54-102. (U.S. Air Force)
Republic F-105B-1-RE Thunderchief 54-102. (U.S. Air Force)

The F-105 was the largest single-seat, single-engine combat aircraft in history. It was designed as a tactical nuclear strike aircraft and fighter-bomber. The fuselage of the F-105B incorporated the “area rule” which gave the Thunderchief its characteristic “wasp waist” shape. The Thunderchief was 63 feet, 1 inch (19.228 meters) long with a wingspan of 34 feet, 11 inches (10.643 meters). It was 19 feet, 8 inches high (5.994 meters). wings were swept 45° at 25% chord. The angle of incidence was 0° and there was no twist. The wings had 3° 30′ anhedral. The total wing area was 385 square feet (35.8 square meters). The F-105 had an empty weight of 25,855 pounds (11,728 kilograms) and a maximum takeoff weight of 50,000 pounds (22,680 kilograms).

Brigadier General Joseph H. Moore with a Republic F-105 Thunderchief.
Brigadier General Joseph H. Moore with a Republic F-105 Thunderchief.

Early production F-105Bs had the Pratt & Whitney J75-P-5 axial-flow turbojet engine. Beginning with the Block 20 aircraft, the more powerful J75-P-19 was installed. The -19 engine was retrofitted to the earlier aircraft. The Thunderchief was powered by one Pratt & Whitney J75-P-19W engine. The J75 is a two-spool axial-flow afterburning turbojet with water injection. It has a 15-stage compressor section (8 low- and and 7 high-pressure stages) and 3-stage turbine section (1 high- and 2 low-pressure stages.) The J75-P-19W is rated at 14,300 pounds of thrust (63.61 kilonewtons), continuous power; 16,100 pounds (71.62 kilonewtons), Military Power (30-minute limit); and Maximum Power rating of 24,500 pounds (108.98 kilonewtons) with afterburner (15-minute limit). The engine could produce 26,500 pounds of thrust (117.88 kilonewtons) with water injection, for takeoff. The J75-P-19W is 21 feet, 7.3 inches (6.586 meters) long, 3 feet, 7.0 inches (1.092 meters) in diameter, and weighs 5,960 pounds (2,703 kilograms).

Armament consisted of one 20 mm General Electric M61 Vulcan six-barreled Gatling gun with 1,080 rounds of ammunition. It had an internal bomb bay and could carry bombs, missiles or fuel tanks on under wing and centerline hardpoints. The maximum bomb load consisted of fourteen 750-pound (340 kilogram) bombs. For tactical nuclear strike missions, the F-105B could carry one Mk 28 “special store” in the internal bomb bay.

The F-105B had a maximum speed of 737 knots (848 miles/1,364 kilometers per hour) at Sea Level, and 1,204 knots (1,386 miles per hour/2,230 kilometers per hour) at 35,000 feet (10,668 meters). The service ceiling was 45,700 feet (13,929 meters). Maximum range was 2,006 nautical miles (2,308 statute miles/3,715 kilometers).

Republic Aircraft Corporation built 833 Thunderchiefs for the U.S. Air Force. 75 of those were F-105Bs. 372 F-105s were lost to enemy action in South East Asia.

Republic F-105B-20-RE Thunderchief 57-5812 served with the 119th Tactical Fighter Squadron, New Jersey Air National Guard, and was later assigned to the 466th Tactical Fighter Squadron, 508th Tactical Fighter Wing at Hill Air Force Base, Utah. One source indicates that the the record-setting F-105B was used as a battle damage repair trainer at McClellan Air Force Base, Sacramento, California, from October 1980.

Six F-105B-10-REs (6 of 9 block 10 aircraft built) of General Moore's 4th Tactical Fighter Wing parked on the ramp. The stripes on the nose and vertical fin are green. Aircraft are (nearest to farthest) S/N 57-5779, -5780, -5782, -5784, -5781, -5778. (U.S. Air Force photo)
Six F-105B-10-REs (6 of 9 block 10 aircraft built) of General Moore’s 4th Tactical Fighter Wing parked on the ramp. The stripes on the nose and vertical fin are green. Aircraft are (nearest to farthest) 57-5779, -5780, -5782, -5784, -5781, -5778. (U.S. Air Force)
Three Republic F-105B-20-RE Thunderchiefs, serial numbers 57-5815, 57-5807 and 57-5822, begin their takeoff roll. This is the same block number as the F-105B flown by General Moore for the FAI World Speed Record. (U.S. Air Force)
Three Republic F-105B-20-RE Thunderchiefs, serial numbers 57-5815, 57-5807 and 57-5822, begin their takeoff roll. These are from the same production block as the F-105B flown by General Moore for the FAI World Speed Record. (U.S. Air Force)
Republic F-105B-20-RE Thunderchief 57-5812, assigned to the 466th Tactical Fighter Squadron. (Million Monkey Theater)
The World Speed Record holder, Republic F-105B-20-RE Thunderchief 57-5812, assigned to the 466th Tactical Fighter Squadron, 508th Tactical Fighter Wing, Hill Air Force Base, Utah. (Million Monkey Theater)

¹ Many sources, including the newspaper article quoted above, cite General Moore’s World Record Speed for the 100-kilometer closed course at 1,216.48 miles per hour (1,957.745 kilometers per hour). The FAI’s official web site gives General Moore’s speed as 1,878.67 kilometers per hour (1,167.35 miles per hour). (See above.) Also, many sources (including General Moore’s official Air Force biography) state that General Moore won the Bendix Trophy for this flight. The Bendix Trophy was awarded to the winner of an annual West-to-East transcontinental air race. The Smithsonian Institution indicates that the Bendix Trophy was not awarded for the years 1958, 1959 or 1960.

² FAI Record File Number 8874, 1 771 km/h, set 18 June 1959 by Gérard Muselli, flying a Dassault Mirage III A over Brétigny-sur Orge, France.

© 2018, Bryan R. Swopes