Category Archives: Aviation

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

11 December 1951

Test pilot William R. Murray at the control of Kaman K-225, Bu. No. 125477, with a Boeing 502-2 gas turbine engine installed. (U.S. Navy)

11 December 1951: The first helicopter powered by a gas turbine engine made its first flight at the Kaman Aircraft Company plant at Bloomfield, Connecticut. Using a K-225 tandem rotor helicopter delivered to the U.S. Navy in 1949, Bureau of Aeronautics serial number (“Bu. No.”) 125477, Kaman replaced the 220 horsepower Lycoming O-435-A2 reciprocating engine with a Boeing 502-2E turboshaft engine. This engine could produce 175 continuous horsepower at 2,900 r.p.m. at Sea Level, less than the piston engine it replaced, but it also weighed considerably less.

K-225 Bu. No. 125477 was the first helicopter to perform an intentional loop, when it was delivered to the Navy at NATC Patuxent River by factory test pilot William R. Murray. It was placed in storage at Bradley Field, Windsor Locks, Connecticut until 1957. The gas turbine had been removed. When the helicopter was transferred to the Smithsonian Institution in 1957, a similar-appearing Boeing YT-50-BO-2 gas turbine engine was installed.

The K-225 was a two-place, single-engine helicopter using Kaman’s unique system of counter-rotating, intermeshing rotors (“synchropter”). Each rotor cancelled the torque reaction of the other, eliminating the need for a tail rotor. In a conventional single-rotor helicopter, up to 30% of the engine power is required to drive the tail rotor. With the counter-rotating design, the total engine power is available for lift and thrust.

K-225 Bu. No. 125477 is 22 feet, 5 inches (6.83 meters) long. Each rotor has a diameter of 38 feet (11.58 meters). It stands 11 feet, 6 inches (3.51 meters) high. The helicopter has an empty weight of 1,800 pounds (816 kilograms) and a maximum gross weight of 2,700 pounds (1,225 kilograms). It is a slow helicopter, with a never-exceed (VNE) limit of 70 miles per hour (112.7 kilometers per hour). This historic helicopter is on display at the Smithsonian Institution National Air and Space Museum, Steven F. Udvar-Hazy Center in Chantilly, Virginia.

Kaman K-225, Bu. No. 125477, the first gas turbine-powered helicopter, at the Vertical Flight Gallery, Steven F. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum, Chantilly, Virginia. (NASM)
Kaman K-225, Bu. No. 125477, the first gas turbine-powered helicopter, at the Vertical Flight Gallery, Steven F. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum, Chantilly, Virginia. (NASM)

© 2016, Bryan R. Swopes

11 December 1945

Bell-Atlanta B-29B-60-BA Superfortress 44-84061, the Pacusan Dreamboat. (U.S. Air Force)
Bell-Atlanta B-29B-60-BA Superfortress 44-84061, the Pacusan Dreamboat. (U.S. Air Force)

11 December 1945: Three days after Lieutenant Colonel Henry E. Warden and Captain Glen W. Edwards set a transcontinental speed record flying a prototype Douglas XB-42 from Long Beach, California, to Washington, D.C., in 5 hours, 17 minutes, Colonel Clarence S. Irvine and the crew of the B-29 Pacusan Dreamboat also set a record, flying from Burbank, California to overhead Floyd Bennett Field, New York, in 5 hours, 27 minutes, 8 seconds. The average speed for the 2,464-mile flight was 450.38 miles per hour (724.82 kilometers per hour).

Lieutenant General Clarence S. Irvine, U.S. Air Force

Irvine was Deputy Chief of Staff, Pacific Air Command, 1944–1947. He flew the Pacusan Dreamboat on several record-setting flights, including Guam to Washington, D.C., and Honolulu, Hawaii to Cairo, Egypt. He rose to the rank of lieutenant general in the United States Air Force, and served as Deputy Chief of Staff for Materiel.

Pacusan Dreamboat was a Bell Aircraft Corporation B-29B-60-BA Superfortress, built at Marietta, Georgia. The B-29B was a lightweight variant of the B-29, intended for operation at lower altitudes. It did not have the four power gun turrets and their .50-caliber machine guns. A radar-directed 20 mm cannon and two .50-caliber machine guns in the tail were the only defensive weapons. Much of the standard armor plate was also deleted. Pacusan Dreamboat was further lightened. The tail guns were removed and the tail reshaped.

The B-29B was equipped with four air-cooled, fuel-injected Wright R-3350-CA-2 Duplex Cyclone two-row 18 cylinder radial engines and specially-designed propellers. The engine nacelles were modified for improved cooling.

The Superfortress had been lightened to an empty weight of 66,000 pounds (29,937 kilograms). A standard B-29B weighed 69,000 pounds (31,298 kilograms) empty and 137,000 pounds (62,142 kilograms) fully loaded. Additional fuel tanks installed on the Dreamboat were able to carry 10,000 gallons (37,854 liters) of gasoline.

Colonel Clarence S. Irvine (standing, left) with the crew of Pacusan Dreamboat: W.J.Benett, G.F.Broughton, Dock West, W.S. O’Hara, F.S. O’Leary, K.L. Royer, F.J.Shannon, J.A. Shinnault, G.R. Stanley. (FAI)
Colonel Clarence S. Irvine (standing, left) with the crew of Pacusan Dreamboat: W.J. Benett, G.F. Broughton, Dock West, W.S. O’Hara, F.S. O’Leary, K.L. Royer, F.J. Shannon, J.A. Shinnault, G.R. Stanley. (FAI)

© 2015, Bryan R. Swopes

11 December 1941

Captain Henry Talmage Elrod, USMC. (1905–1941). Awarded the Medal of Honor, posthumously, for his actions in the defense of Wake Island.
Captain Henry Talmage Elrod, United States Marine Corps, was awarded the Medal of Honor, posthumously, for his actions in the defense of Wake Island. (U.S. Navy)

Continue reading 11 December 1941

11 December 1941

Pilot Officer John Gillespie Magee, Jr., Royal Canadian Air Force.

11 December 1941: Pilot Officer John Gillespie Magee, Jr., Royal Canadian Air Force, an American serving in England before the United States entered World War II, was killed when his Supermarine Spitfire collided with another airplane in clouds over the village of Roxholm, Lincolnshire, England. He was only 19 years old.

Magee was born in China, the son of Anglican missionaries. His father was an American, giving him American citizenship, and his mother was from England. He was educated in the missionary schools until 1931 when his mother took him to England to continue his education at the Rugby School in Wawickshire.

In 1939, Magee traveled to the United States to visit his father’s family in Pittsburgh, but because of the outbreak of World War II, he was unable to return to England. While in America, he continued his schooling at the Avon Old Farms School in Connecticut and won a scholarship to Yale University.

Group Captain Wilfred A. Curtiss presents pilot’s wings to Pilot Officer John Gillespie Magee, Jr., at Ottawa, Ontario, Canada, 14 April 1941. (Royal Canadian Air Force)

Instead of studying at Yale, in 1941, John Magee enlisted in the Royal Canadian Air Force. After completing flight training, he was sent to England. Once there he went through operational training in the Supermarine Spitfire and was assigned to No. 412 (Fighter) Squadron at RAF Digby, Scopwick Heath, and then at RAF Wellingore, Navenby, both in Lincolnshire.

Pilot Officer John Gillespie Magee, Jr., in the cockpit of his Supermarine Spitfire, No. 412 Squadron, Royal Canadian Air Force.
Pilot Officer John Gillespie Magee, Jr., in the cockpit of a Supermarine Spitfire, No. 412 Squadron, Royal Canadian Air Force.

At approximately 11:30 a.m., 11 December 1941, Pilot Officer Magee was flying his Supermarine Spitfire Mk.Vb, AD291, squadron markings VZ-H. He and three other pilots from No. 412 Squadron descended through a hole in the clouds. At 1,400 feet (427 meters), Magee’s Spitfire collided with an Airspeed A.S. 10 Oxford twin-engine trainer, T1052.

A witness said that he saw the Spitfire pilot struggle to open the airplane’s canopy, then stand up in the cockpit and jump from the doomed fighter. The pilot was too close to the ground for his parachute to open.

Both airplanes crashed. Pilot Officer John Gillespie Magee, Jr. was killed, as was the pilot of the other airplane, Leading Aircraftman Ernest Aubrey Griffin.

Pilot Officer John Gillespie Magee, Jr., No. 412 Squadron, Royal Canadian Air Force

Pilot Officer Magee is best known for his poem, High Flight:

Oh! I have slipped the surly bonds of Earth 
And danced the skies on laughter-silvered wings; 
Sunward I’ve climbed, and joined the tumbling mirth 
of sun-split clouds,—and done a hundred things 
You have not dreamed of—wheeled and soared and swung 
High in the sunlit silence. Hov’ring there, 
I’ve chased the shouting wind along, and flung 
My eager craft through footless halls of air. . . . 

Up, up the long, delirious, burning blue 
I’ve topped the wind-swept heights with easy grace 
Where never lark nor ever eagle flew— 
And, while with silent lifting mind I’ve trod 
The high untrespassed sanctity of space, 
Put out my hand, and touched the face of God

"On Laughter-Silvered Wings", by Keith Ferris, 1995. © by the artist. The original of this painting, depicting John Gillespie Magee’s Supermarine Spitfire, is on loan to the George Bush Presidential Library and Museum, College Station, Texas.
“On Laughter-Silvered Wings”, by Keith Ferris, 1995. © by the artist. The original of this painting, depicting John Gillespie Magee’s Supermarine Spitfire, is on loan to the George Bush Presidential Library and Museum, College Station, Texas.

A less well-know poem by Magee is Per Ardua, written after his first combat mission, 8 November 1941.

(To those who gave their lives to England during the Battle of Britain and
left such a shining example for us to follow, these lines are dedicated.)

They must have climbed the white mists of the morning;
They that have soared, before the world’s awake,
To herald up their foemen to them, scorning
The thin dawn’s rest their weary folk might take;

Some that left other mouths to tell the story
Of high blue battle,—quite young limbs that bled;
How they had thundered up the clouds to glory
Or fallen to an English field stained red;

Because my faltering feet would fail I find them
Laughing beside me, steadying the hand
That seeks their deadly courage—yet behind them
The cold light dies in that once brilliant land …

Do these, who help the quickened pulse run slowly,
Whose stern remembered image cools the brow—
To the far dawn of Victory know only
Night’s darkness, and Valhalla’s silence now?

Supermarine Spitfire F. Mk.Vb R6923 (QJ-S) of No. 92 Squadron, 19 May 1941. © IWM (CH 2929)

John Magee’s fighter was a Supermarine Spitfire F. Mk Vb, built at the Castle Bromwich Aircraft Factory, at Warwickshire, West Midlands, and delivered to the 45th Maintenance Unit at RAF Kinloss, Scotland, on 27 September 1941. The new airplane was assigned to No. 412 Squadron on 14 October.

The Supermarine Spitfire was a single-place, single-engine low-wing monoplane of all-metal construction with retractable landing gear. The fighter had been designed by Reginald Joseph Mitchell CBE. The prototype first flew 5 March 1936.

The Spitfire F. Mk Vb was 29 feet, 11 inches (9.119 meters) long with a wingspan of 36 feet, 10 inches (11.227 meters) and overall height of 11 feet, 5 inches (3.480 meters). It had an empty weight of 4,963 pounds (2,129 kilograms) and gross weight of 6,525 pounds (2,960 kilograms).

The Spitfire Vb was powered a liquid-cooled, supercharged, 1,648.959-cubic-inch-displacement (27.022 liters) Rolls-Royce Merlin 45 single overhead camshaft (SOHC) 60° V-12 engine with a single-speed, single-stage supercharger. It was rated at 1,185 horsepower at 3,000 r.p.m., at 11,500 feet (3,505 meters). The Merlin 45 drove a three-bladed Rotol constant-speed propeller with a diameter of 10 feet, 9 inches (3.277 meters).

The Spitfire Vb had a maximum speed of 371 miles per hour (597 kilometers per hour) at  20,100 feet (6,126 meters). It could reach 20,000 feet (6,096 meters) in 6 minutes, 24 seconds, and 30,000 feet (9,144 meters) in 12 minutes, 12 seconds. The Vb’s service ceiling 37,500 feet (11,430 meters), and its range was 470 miles (756 kilometers).

The Spitfire F. Mk Vb was armed with two 20-milimeter Hispano Mk.II autocannon, with 60 rounds of ammunition per gun, and four Browning .303-caliber Mark II machine guns, with 350 rounds per gun.

Supermarine Spitfire F.Mk Vb,, similar to Magee’s fighter, photographed 19 October 1941. (Royal Canadian Air Force

© 2016, Bryan R. Swopes