Category Archives: Aviation

20 August 1944

A North American Mustang Mk.I of No. 168 Squadron, Royal Air Force,  banking over Pierrefitte-en-Cinglais in Normandy on a tactical reconnaissance sortie, August 1944. Allied tanks can be seen on the road below. © IWM (C 4559)

20 August 1944: At 16:26 hours, North American Aviation Mustang Mk.I AG346, assigned to No. 168 Squadron,¹ 39 (Reconnaissance) Wing, Second Tactical Air Force, Royal Air Force, took off from an advance airfield, B21, at Sainte-Honorine-des-Pertes, Normandy, France.

AG346 was the very first operational Mustang Mk.I. During this mission, it was hit by intense antiaircraft fire northeast of Gacé. The Mustang’s pilot, Flight Lieutenant Denis Clark, 119758, Royal Air Force Volunteer Reserve, bailed out. He landed safely, but was captured and taken to a German prisoner of war camp at Les Hogues, a small community east of Rouen.

Flight Lieutenant Clark, along with four other prisoners of war,² was shot and killed at the camp on the afternoon 25 August 1944. A Court of Enquiry held in August 1945 found that the five men had been murdered by SS-Obersturmfürer Eugen Gutemann. Gutemann had been captured in Italy on 28 April 1945 and was held as a prisoner of war by the American forces. It is not known if he was ever brought to trial.

Denis Clark was born 17 December 1918 at Stockton-on-Tees, County Durham, England. He was the son of Sydney Clark, an electrician in the chemical industry, and Minnie Gertrude Ritchie.

In 1939, Clark was employed as a civil service clerk. He resided at 3 Crayke Road in Stockton, with his parents and maternal grandmother.

He was married to Miss Beth Ayre of Seaton, County Durham, possibly in July 1942.

Clark entered the United States at Buffalo, New York, on 16 July 1941, having traveled from Toronto, Ontario, Canada. He was trained as a pilot at the Southern Aviation School, a military contract primary flight school in Camden, South Carolina, United States, beginning in July 1941. He was one of 297 RAF pilots to train there between 7 June 1941 and 16 February 1942.

Head stone of Flight Lieuetenant Denis Clark, RAFVR. (Find-a-Grave)

On 7 February 1942 Temporary Flight Sergeant Denis Clark 945260 was promoted to the rank of Pilot Officer on probation (Temporary) 119758.

On 1 October 1942, Pilot Officer (prob.) Denis Clark was promoted to Flying Officer on probation (war substantive).

Flying Officer Clark was later promoted to the rank of Flight Lieutenant. (Date not determined)

Flight Lieutenant Denis Clark, RAFVR, was buried at Les Hogues Communal Cemetery, along with the other four victims. His head stone is engraved

GREATER LOVE HATH NO MAN THAN THIS.
THAT A MAN LAY DOWN HIS LIFE FOR HIS FRIEND.

On 10 September 1945 a warrant was issued as a gratuity for the representatives of deceased officers in the amount of £172/13/7.

North American Aviation Mustang Mk.I AG346 (s/n 73-3099) at Mines Field, California, Summer 1941. Note the short carburetor intake, and compare to the photograph below. (North American Aviation, Inc.)

The very first operational North American Mustang, AG346 (North American Aviation serial number 73-3099) was the second airplane to come off the assembly line at Inglewood, California. North American test pilot Robert Creed Chilton took it for its first flight 3 July 1941. It was the first Mustang Mk.I to be equipped with its full armament.

During flight testing of the first Mk.I, AG345, Chilton and other test pilots heard a banging sound. This was determined to be a resonance in the carburetor intake tract. Also, at high angles of attack, air flow into the intake was decreased. The intake was lengthened. The resonance stopped and air flow to the carburetor was improved.

After flight testing by North American’s test pilots and Royal Air Force fighter pilots Wing Commander Chris Clarkson and Squadron Leader Michael N. (“Red Knight”) Crossley, AG346 was disassembled and crated, then shipped from the port of Long Beach, California, through the Panama Canal and on to England, arriving at Liverpool, 24 October 1941. It was taken to the Lockheed facility at Speke Aerodrome (now, Liverpool John Lennon Airport, LPL) where it was reassembled and put through additional performance and flight tests. Up to 20,000 feet (6,096 meters), AG346 was faster than any other British fighter then in service. A Mk.II reflector gun sight was installed (the same type used in the Supermarine Spitfire), as well as a British VHF radio.

North American Aviation Mustang Mk.I AG346 at Speke Aerodrome, November 1941. Note the lengthened carburetor intake, and compare to the photograph above. © IWM (ATP 10608C)

AG346 was publicly displayed for the British news media at Speke Aerodrome on 5 December 1941.

AG346 was then assigned to an operational RAF fighter squadron. It served with Nos. 225, 63 and 26 Squadrons before being assigned to No. 41 Operations Training Unit. AG346 was returned to operations with No. 16 Squadron, and finally, No. 168 Squadron.

North American Aviation Inc. Mustang Mk.I fighter, AG348, built for the Royal Air Force, at Mines Field, Los Angeles, California, 1941. North American Aviation, Inc., photograph. (Ray Wagner Collection/SDASM)

The Mustang Mk.I was a new fighter built by North American Aviation, Inc., for the Royal Air Force. The British Purchasing Commission asked North American Aviation in Los Angeles, California, to build additional Tomahawks (the RAF variant of the Curtiss-Wright P-40 Warhawk) under license from Curtiss-Wright.

North American countered with a proposal to design a completely new and superior fighter around the P-40’s liquid-cooled Allison V-12 engine, and to begin production in no more time than it would take to get a P-40 production line up and running. The Purchasing Commission agreed, and with a letter of understanding, North American began work on the NA-73X on 1 May 1940. They were to produce 320 fighters before 30 September 1941—approximately 50 per month—at a total price of $14,746,964.35.

Edgar Schmued with P-51-NA 41-37322 (Mustang Mk.IA) (San Diego Air and Space Museum Archives Catalog #: 02-S-00192)

Designed by a team led by Edgar Schmued, the prototype North American Aviation Model NA-73X, serial number 73-3097, registered NX19998, was completed 9 September 1940. After a delay waiting for the Allison V-1710 to arrive, the prototype made its first flight 26 October 1940 with free lance test pilot Vance Breese in the cockpit. This was only 179 days since work began on the project.

In a contract amendment dated 9 December 1940, the British Purchasing Commission directed that the NA-73 would be identified by the name, “Mustang.”

The Mustang Mk.I (NAA Model NA-73) was a single-place, single-engine fighter primarily of metal construction with fabric control surfaces. It was 32 feet, 3 inches (9.830 meters) long with a wingspan of 37 feet, 5/16-inches (11.373 meters) and height of 12 feet, 2½ inches (3.721 meters). The airplane’s empty weight was 6,280 pounds (2,849 kilograms) and loaded weight was 8,400 pounds (3,810 kilograms).

The Mustang Mk.I was powered by a liquid-cooled, supercharged 1,710.597-cubic-inch-displacement (28.032 liter) Allison Engineering Company V-1710-F3R (V-1710-39) single overhead camshaft (SOHC) 60° V-12 engine with four valves per cylinder and a compression ratio of 6.65:1. The engine had a takeoff rating of 1,150 horsepower at 3,000 r.p.m. at Sea Level with 45.5 inches of manifold pressure (1.51 Bar), and a war emergency rating of 1,490 horsepower with 56 inches of manifold pressure (1.90 Bar). The Allison drove a 10 foot, 9 inch (3.277 meter) diameter, three-bladed, Curtiss Electric constant-speed propeller through a 2.00:1 gear reduction. The V-1710-39 was 7 feet, 4.38 inches (2.245 meters) long, 3 feet, 0.54 inches (0.928 meters) high, and 2 feet, 5.29 inches (0.744 meters) wide. It weighed 1,310 pounds (594 kilograms).

Allison V-1710-39 (F3R) V-12 aircraft engine.

This engine gave the Mustang Mk.I a maximum speed of 382 miles per hour (615 kilometers per hour) and cruise speed of 300 miles per hour (483 kilometers per hour). The service ceiling was 30,800 feet (9,388 meters) and range was 750 miles (1,207 kilometers).

North American Aviation Mustang Mk.I AG365 of the Air Fighting Development Unit at Duxford, Cambridgeshire, February 1942. © IWM (CH17966)

The Mustang Mk.I was equipped with four Browning AN-M2 .50-caliber machine guns, with one in each wing and two mounted in the nose under the engine and four Browning .303 Mk.II machine guns, two in each wing. The airplane carried 300 rounds of ammunition for each of the .50-caliber guns. Each of the inboard .303s were supplied with 932 rounds; and the outboard .303s, 814 rounds, each.³

The British would recommend that the Allison engine be replaced by the Rolls Royce Merlin V-12. This became the Mustang Mk.III and the U.S.A.A.F. P-51B. Eventually, over 15,000 Mustangs were built, and it was a highly successful combat aircraft.

Today, after 85 years, the Mustang is one of the most recognizable of all airplanes.

Mustang Mk.1 of No. 168 Squadron, Royal Air Force. (RAF)
Mustang Mk.I of No. 168 Squadron, Royal Air Force. (RAF)

¹ No. 168 Squadron was a reconnaissance unit. Its motto was Rerum cognoscere causas (“To know the cause of things”)

² Warrant Officer Griffin James Young R85855, Royal Canadian Air Force, a Spitfire pilot who had been shot down 13 August 1944; Lead Bombardier Jack Martin 976272, 65th Anti-Tank Unit (The Norfolk Yeomanry), Royal Artillery, captured 21 August; an unidentified Gunner, Royal Artillery; and Private Gordon Lafayette Bryant 6969514, 117th Infantry Regiment, 30th Infantry Division, United States Army.

³ Crazy Horse Aviation Photography: https://crazyhorseap.be/mustangs/birth-of-a-legend/A-36.html

© 2025, Bryan R. Swopes

20 August 1940

The Few. RAF fighter pilots run toward their Hawker Hurricanes. © IWM (HU 49253)

20 August 1940: During World War II, at the height of the Battle of Britain, Prime Minister Winston Churchill spoke to the House of Commons on the state of the war. As he talked about the role of the Royal Air Force in the defense of England, he said,

Never in the field of human conflict was so much owed by so many to so few.

(Printed for H.M. Stationery Office by Lowe & Brydon Printers, Ltd.)

To this day, the RAF is known as The Few.

A full transcript of the Prime Minister’s speech can be found at:

https://web.archive.org/web/20161114105625/http://www.winstonchurchill.org:80/resources/speeches/1940-the-finest-hour/113-the-few

Prime Minister Winston Churchill addresses Parliament.

© 2016, Bryan R. Swopes

20 August 1919

The DELAG airship Bodensee, LZ 120, at Friederichshafen, October 1919. (Library of Congress)

20 August 1919: The first airship built after World War I, Bodensee, LZ 120, made its first flight at Friedrichshafen, Germany, with Captain Bernard Lau in command. LZ 120 was built for Deutsche Luftschiffahrts-Aktiengesellschaft, DELAG, (German Airship Travel Corporation) especially to carry a small complement of passengers. It was hoped that this would generate favorable publicity and help to restart intercity travel by air.

Bodensee was the first fully-streamlined airship. Its teardrop shape was developed by engineer Paul Jaray and had no cylindrical sections. The shape had been tested with scale models in a wind tunnel. LZ 120 was the first airship to have the gondola was attached directly to the bottom of the envelope, decreasing aerodynamic drag.

Scale model of LZ 120 in a wind tunnel at Göttingen, Germany
Scale model of LZ 120 in a wind tunnel at Göttingen, Germany

LZ 120 was a rigid airship, or dirigible, with a metal skeleton structure covered with a cotton fabric envelope. Twelve hydrogen-filled buoyancy tanks were contained within the structure.  A crew of 12 operated the airship and it could carry 20 passengers.

LZ 120 was 396.33 feet (120.8 meters) in length, with a diameter of 61.38 feet (18.71 meters). The airship had a volume of approximately 20,000 cubic meters (706,000 cubic feet). The airship had an empty weight of 13,646 kilograms (36,698 pounds) and a gross weight of 23,239 kilograms (51,233 pounds).

Maybach Mb IVa at the Smithsonian Institution National Air and Space Museum.
Maybach Mb IVa at the Smithsonian Institution National Air and Space Museum.

LZ 120 was powered by four water-cooled, normally-aspirated, 23.093 liter (1,409.2 cubic inches) Maybach Motorenbau GmbH Mb IVa single overhead cam (SOHC) vertical inline six-cylinder engines with a compression ratio of 6.08:1 and four valves per cylinder. The Mb IVa produced 302 horsepower at 1,700 r.p.m., but was derated to 245 horsepower. Two engines were mounted in the aft centerline engine car and drove a two-bladed propeller with a diameter of 5.2 meters (17.1 feet) through a reversible gear train. Each of the other engines were mounted near the center of the airship, outboard. They each turned a two-bladed propeller with a diameter of 3.2 meters (10.5 feet), which were also reversible.

LZ 120 had a maximum speed of 82 miles per hour (132 kilometers per hour).

After two test flights under Captain Lau, Bodensee entered scheduled passenger service on 24 August 1919 under the command of Dr. Hugo Eckener. It flew from Friedrichshafen to the Oberwiesenfeld at Munich, then on to Berlin-Staaken.

In 1921, Bodensee was turned over to Italy as war reparations. It was renamed Esperia and continued in operation until 1928.

© 2016, Bryan R. Swopes

19 August 1960

A Fairchild C-119J, 51-8039, recovers a Discovery Satellite Reentry Vehicle. (U.S. Air Force)

19 August 1960: Discoverer XIV was a Keyhole KH-1 reconnaissance satellite of Project CORONA. Mission 9009 was launched by a Thor-Agena A two-stage liquid fueled rocket from Vandenberg Air Force Base, California, at 11:55 p.m. Pacific Standard Time, 18 August 1960 (19:55:00 UTC).¹ The Agena A entered a 186 kilometer × 805 kilometer (115.6 miles × 500.2 miles) elliptical orbit, inclined 79.650°, and the satellite took 1 hour, 34 minutes, 33 seconds to complete each orbit.

After 17 orbits, 7 of which crossed over “denied territory,” the Discoverer Satellite Rentry Vehicle (SRV) was ejected from the Agena A and de-orbited. This ejection took place within 5 seconds of the planned time.

On 19 August, a Fairchild C-119J Flying Boxcar, 51-8037, call sign Pelican 9, of the 6593rd Test Squadron, Hickham Air Force Base, Hawaii, was sent to recover the satellite as it descended through the lower atmosphere by parachute. The air crew sighted the parachute at about 8,000 feet (2,438 meters), 360 miles (580 kilometers) southwest of Hawaii. On their third attempt, they were able to snag the satellite and parachute with recovery equipment deployed under the transport, and then pull it inside. This was the first time that film from a satellite had been recovered.

Corona 1 photographic image of Mys Shmidta Air Field, USSR. This image, taken 18 August 1960, has a resolution of 40 feet x 40 feet ( meters). (National Reconnaissance Office)
Corona 1 photographic image of Mys Shmidta Air Field, Chukotka, Russia, USSR, an intercontinental bomber staging base built in 1954. This image, taken 18 August 1960, has a resolution of 40 feet × 40 feet (12.2 meters × 12.2 meters). The runway is 2,450 meters (8,038 feet) long. (National Reconnaissance Office)

Pelican 9’s pilot, Captain Harold Ellis Mitchell (22 June 1925–14 February 2013) was awarded the Distinguished Flying Cross. The other members of the crew received the Air Medal.

Flight Crew of Fairchild C-119J 51-8037, circa 1960. Front row, left to right: Captain Harold Ellis Mitchell, Captain David Torgerson, 1st Lieutenant Robert Counts, Staff Sergeant Arthur Hurst, Airman Second Class Thierry Franc; back row: Technical Sergeant Louis Bannick, Staff Sergeant Algaene Harmon, A2C George Donohou, A2C Lester Beale and A2C Daniel Hill. (U.S. Air Force)

The Agena A remained in orbit until 16 September 1960.

Mission 9009 photographed 1.5 million square miles (3.9 million square kilometers) of Soviet and Eastern Europe countries.

The mission summary reads:

     Mission 9009 was accomplished on 18 August 1960. It consists of eight north-south passes over the USSR and includes portions of China, the Satellites and Yugoslavia (see accompanying coverage map).

     Approximately 25 percent of the coverage is cloud free, with light-scattered to heavy clouds covering the remainder of the photography. The PI quality of the unobscured coverage ranges from good to very good.

     The scale of the photography is estimated to range from 1:300,000 to 1:450,000.

     Major items of intelligence significance covered by Mission 9009 incluse the Kapsutin Yar Missile lTest Range (KYMTR), the western portion of the presumed 1,050 nm impact area of the KYMTR, 20 newly identified hexadic SA-2 surface to air missile sites and six possible SA-2 sites under construction, the Sarova Nuclear Weapons Research and Development Center, several new airfields, and numerous urban complexes.

CORONA: America’s First Satellite Program, Kevin C. Ruffner, Editor, and CIA History Staff. Center of the Study of Intelligence, Central Intelligence Agency, Washington, D.C., 1995, at  Page 120

The mission report contains a lengthy list of airfields and military installations of intelligence interest to the United States.

Project CORONA had been proposed by the Advanced Research Projects Agency (ARPA) and was managed by the Central Intelligence Agency and the United States Air Force. The Discoverer program was publicly explained as an Earth sciences research project, with some carrying live monkeys, but was actually a Central Intelligence Agency program for the reconnaissance of the Soviet Union and China.

Lockheed Missiles and Space Company at Sunnyvale, California, was the prime contractor, while Fairchild Camera and Instrument Co. was responsible for the KH-1 camera system. General Electric built the Satellite Reentry Vehicle (SRV).

Lockheed RM-81 Agena A. (U.S. Air Force via Drew ex Machina)
Internal Arrangement of Corona spacecraft. (Drew ex Machina)

The Discoverer reconnaissance payload was carried into orbit by a Lockheed RM-81 Agena A. This was a liquid-fueled rocket used as a second stage for the Thor first stage booster. The Agena A was 15.51 feet (4.73 meters) long and 4.98 feet (1.52 meters) in diameter. It had an empty weight of 1,951 pounds (885 kilograms) and maximum weight of 8,350 pounds (3,790 kilograms).

Early Agena As were powered by a single Bell 8001 (XLR81-BA-3) rocket engine which had originally been developed as a Rocket Assisted Takeoff (RATO) unit for the Convair B-58A Hustler Mach 3 strategic bomber. This was upgraded to the Bell 8048 (XLR81-BA-5) for most Agena As. This engine weighed 279 pounds (126.6 kilograms). Burning Nitric Acid and UDMH, it produced 15,589 pounds of thrust (69.343 kilonewtons). The engine had a burn time of 120 seconds. The engine nozzle was gimballed for pitch and yaw control.

Bell Model 8048 (XLR81-BA-5) rocket engine in the collection of the National Museum of the United States Air Force. (U.S Air Force)

The Agena A nose cone carried a Fairchild Camera and Instrument Co. KH-1 panoramic camera system. It used 20 pounds (kilograms) of 70 mm film. The camera used an ITEK Corporation HYAK B lens with an f/5.0 aperture and focal length of 61 centimeters. Its ground resolution was 11.7 meters. The camera transferred the film to the reentry vehicle.

Resolution was not as good as could be obtained by a Lockheed U-2 reconnaissance plane, but the Discoverer XIV was able to cover areas that the U-2 never reached.

The Agena A orbiter also had a TOD-4 navigation payload.

Internal arrangement of Discoverer photographic system. (Drew ex Machina)

When it was time to eject the SRV, the Agena A pitched down 60°. The SRV was spin-stabilized by small rockets, and then a retro rocket fired to decelerate it into a descent trajectory.

Fairchild C-119J-FA Flying Boxcar 51-8037 at the National Air and Space Museum, Wright Patterson Air Force Base, Ohio. (U.S. Air Force)

51-8037 had been built as a C-119F Packet “Flying Boxcar” and delivered to the U.S. Air Force on 2 June 1953. It was converted to a C-119J at the Birmingham Modification Center in Birmingham, Alabama, during October 1956. From September 1958 to November 1959, it was further modified specifically to recover space capsules. The satellite recovery airplane is in the collection of the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.

The C-119F Flying Boxcar is a large twin-engine transport aircraft with a distinctive twin boom configuration. It has a high wing and retractable tricycle landing gear. It normally carried a flight crew of five, consisting of two pilots, a navigator, radio operator and crew chief. It could carry 42 troops, or a maximum of 62 troops for emergency evacuation. Alternatively, it could transport 35 litter patients and 4 attendants. The airplane is 86.5 feet (26.365 meters) long with a wingspan of 109.3 feet (33.315 meters) and overall height of 26.5 feet (8.077 meters. It has a total wing area of 1,447.2 square feet (134.45 square meters). The C-119F has an empty weight of 40,118 pounds (18,197 kilograms), and takeoff weight of 77,000 pounds (34,927 kilograms). The cargo payload is 20,650 pounds (9,367 kilograms).

The C-119F was powered by two air-cooled, supercharged and fuel injected, 3,347.66 cubic-inch displacement (543.858 liter) Wright 868TC18DB1 Cyclone 18 (R-3350-85) two-row, 18-cylinder radial engines. These engines were also known as the Duplex-Cyclone. They had a compression ratio of 6.7:1 and required 115/145 octane aviation gasoline. The Normal Power rating was 2,650 horsepower at 2,650 r.p.m. (continuous); Takeoff Power rating, 3,500 horsepower at 2,900 horsepower at 2,900 r.p.m. at Sea Level (5 minute limit); and Military Power rating of 3,500 horsepower at 2,900 r.p.m. at 4,500 feet (1,372 meters) with a 30 minute limit. This decreased to 2,550 horsepower at 15,400 feet (4,694 meters), and retained the 30 minute limit. The R-3350-85 had a length of 90.80 inches (2.306 meters), diameter of 56.59 inches (1.437 meters), and weighed 3,472 pounds (1,575 kilograms. It used a 0.4375:1 gear reduction. 2,395 of these engines were produced between September 1951 and 1954.

This airplane had a maximum speed of 265 knots (305 miles per hour/491 kilometers per hour) at 17,900 feet (5,456 meters) at maximum power. Its cruise speed was 248 knots (285 miles per hour/459 kilometers per hour) at 5,000 feet (1,524 meters).

The C-119F could takeoff after a ground run of 3,875 feet (1,181 meters), and had a rate of climb of 795 feet per minute (4.04 meters per second) at Sea Level with Normal Power at its takeoff weight of 77,000 pounds (34,927 kilograms). At a combat weight of 49,360 pounds (22,389 kilograms) and using maximum power, it could climb at 2,320 feet per minute (11.8 meters per second). Its service ceiling was 26,600 feet (8,108 meters) at maximum power.

With a maximum fuel capacity of 2,590 gallons (9,804 liters) and maximum payload, the C-119F had a combat range of 1,462 nautical miles (1,682 statute miles/2,708 kilometers) at 158 knots (182 miles per hour/292 kilometers per hour).

Fairchild produced 1,183 C-119s between 1949 and 1955.

¹ Launch windows were scheduled to avoid the passage of Southern Pacific Railroad passenger trains which ran along the coast at Vandenberg, to prevent the spacecraft being seen by the public. Sometime only a few minutes were available between passing trains.

© 2024, Bryan R. Swopes