Tag Archives: Fédération Aéronautique Internationale

14 July 1959

Major General Vladimir Sergeyevich Ilyushin, Hero of the Soviet Union

14 July 1959: At Podmoskovnoe, USSR, famed Soviet test pilot Vladimir Sergeyevich Ilyushin flew the Sukhoi T-43-1, a prototype of the Su-9 interceptor, to a Fédération Aéronautique Internationale (FAI) World Record for Altitude of 28,852 meters (94,659 feet).¹

Vladimir Sergeyevich Ilyushin was the son of Sergey Ilyushin, the Soviet aircraft designer. He made the first flights of many Sukhoi fighters. A Hero of the Soviet Union, he retired with the rank of major general.

Sukhoi T-43-1
Vladimir Sergeyevich Ilyushin, wearing flight suit and helmet, with a Sukhoi Su-9 in the background.
Vladimir Sergeyevich Ilyushin, wearing flight suit and helmet, with a Sukhoi Su-9 in the background.

The Sukhoi T-43-1 was the prototype for the Su-9 all-weather interceptor, a single-place, single-engine Mach 2+ fighter. It was built from the first pre-production Sukhoi T-3, with a new nose section and enlarged rear fuselage to accommodate a larger engine.

The production Su-9 is similar in appearance to the Mikoyan Gurevich MiG-21, but is much larger and heavier. It is 17.37 meters (56.99 feet) long with a wingspan of 8.43 meters (27.66 feet) and overall height of 4.88 meters (16.01 feet). The interceptor’s empty weight is 8,620 kilograms (19,004 pounds), and the maximum takeoff weight is 13,500 kilograms (29,762 pounds).

Sukhoi T-43-12 prototype.
Sukhoi T-43-12 prototype.

Both the T-43-1 prototype and the production Su-9 are powered by a Lyulka AL-7 nine-stage axial flow turbojet engine which produces 22,050 pounds of thrust with afterburner.

The Su-9 has a maximum speed of Mach 2.0 (2,135 kilometers per hour, 1,327 miles per hour). The service ceiling is 16,760 meters (54,987 feet) and range is 1,125 kilometers (699 miles).

The T-43-1 later set FAI records for sustained altitude and speed over a measured course.

Sukhoi Su-9
Sukhoi Su-9, right front quarter
Sukhoi Su-9
Sukhoi Su-9, right profile

¹ FAI Record File Number 10351

© 2017, Bryan R. Swopes

14 July 1897

The hydrogen balloon Örnen (Eagle) on the polar ice cap, 14 July 1897. (Nils Strindberg)

14 July 1897: At 8:11 p.m., G.M.T., the Andrée Arctic Expedition’s hydrogen gas balloon, Örnen (Eagle), came to rest on an ice floe in the Arctic Ocean, at N. 82° 52′, E. 29° 32′. ¹ This was the end of a planned transpolar flight and the beginning of a three-month struggle for survival.

Balloon Örnen (Eagle) in its protective enclosure, Danes Island, Spitzbergen, Norway. (Andréemuseet, Griänna, Sweden)

At 1:50 p.m., 11 July 1897, Örnen rose from its protective enclosure on Danskøya (Danes Island) in the Svalbard Archipelago of Norway. Carried aloft in the balloon’s gondola were the expedition’s leader, Salomon August Andrée, and his fellow explorers, Knut Hjakmar Ferdinand Frænkel and Nils Strindberg.

Intrepid aeronauts: Left to right, Gustav Vilhem Emanuel Swedenborg (alternate); Nils Strindberg; Knut Hjakmar Ferdinand Frænkel; Salomon August Andrée (seated). (Andréemuseet, Griänna, Sweden)

The goal of the expedition was to fly across the North Pole and onward to Alaska on the North American Continent. Andrée considered that the balloon would need to retain enough gas during the voyage to remain airborne for 30 days. Supplies for the three men for that period were carried. 36 homing pigeons would allow the explorers to report their progress to the outside world.

This would be the expedition’s second attempt. The previous year, adverse winds forced the aeronauts to abandon the flight.

Balloon Örnen in its protective enclosure, Danes Island, Spitzbergen, Norway. (Andréemuseet, Griänna, Sweden)
Henri Lachambre

Örnen had been designed and manufactured by Henri Lachambre at his balloon factory at Vaugirard, a suburb on the Left Bank of the Seine, Paris, France. The envelope was assembled from approximately 3,360 pieces of a thin woven Chinese silk fabric called pongee, stitched by hand. The seams were covered by glued strips of pongee. The upper two-thirds of the gas bag had three layers of fabric, while the lower one-third had two plies. It is estimated that 8 million stitches were required. Once completed, the envelope was covered with varnish.

The gondola was constructed of wood and wicker. It had an upper, observation, deck, and an enclosed lower sleeping quarters/darkroom.

A net made of more than 300 hemp ropes covered the balloon, and were braided into twelve ropes which were attached to a lifting ring. The gondola was suspended below this. At Sea Level, the inflated balloon with its gondola were approximately 97 feet (29.6 meters) high, and 68 feet (20.7 meters) in diameter. Its total volume is estimated at 4,800 cubic meters (approximately 170,000 cubic feet).

Buoyancy was provided by hydrogen gas which was produced on site at Danskøya. Hydrogen is the lightest element, and gaseous hydrogen has just 7% of the density of air. This provides greater buoyancy for lighter-than-air vehicles than other gases, but hydrogen gas molecules are also the smallest and they diffuse through fabric barriers more easily than any other gas. (Tests before Örnen was launched found that the balloon was losing about 35 cubic meters/1,236 cubic feet of hydrogen each day.)

Balloons have a disadvantage in that they go where the wind takes them. They are not steerable like dirigibles. So, steady southerly winds would be needed to carry Örnen to the North Pole, and northerly winds to travel from there to Alaska. Andrée had a theory that he believed would allow him to steer his balloon as much as 30° to either side of the prevailing wind.

Andrée’s idea was that if several long, heavy ropes were dragged behind the balloon, their weight and friction would cause the balloon to travel slower than the wind was blowing. He could then use two small sails to steer.

Örnen with guide ropes dragging in the water.

Also, these ropes could be used to control the balloon’s altitude. By pulling the ropes in, the weight supported by the balloon would increase, and it would descend. Letting more rope out would mean that the extra weight would be transferred to the surface, and the balloon would rise.

Altitude was critical. Andrée planned to maintain about 150 meters (approximately 500 feet). As the balloon ascended, atmospheric pressure on the envelope decreased. The pressure differential between the atmosphere and the hydrogen would increase, forcing the hydrogen to pass through the envelope more quickly. Any hydrogen loss was permanent, and the balloon’s buoyancy would decrease.

Balloon Örnen airborne, around 2:00 p.m., 11 July 1897. The wake of the steering ropes can be seen on the surface of the sea. (Andréemuseet, Griänna, Sweden)

Problems began immediately. As the guide ropes dragged through the water, they became heavier. They pulled the balloon down to the surface and the gondola actually touched the water. The aeronauts frantically began dumping ballast. Three of the four ropes became entangled and were pulled loose. Örnen began to rise again, but having lost ballast and the weight of the three guide ropes, it climbed to about 1,600 feet (490 meters). The loss of hydrogen accelerated.

The Eagle floated northward above a fog bank. It sank into the fog and sunlight shining on the envelope decreased. The balloon cooled and the gas inside began to contract. Buoancy decreased and the balloon sank further into the fog.

An alternating pattern of rising and falling developed. After the explorers passed into the Arctic ice pack, the gondola would alternately bounce across the broken ice, then rise again into the sky. At about 10:00 p.m., July 12, the gondola settled on to the ice and remained there for the next thirteen hours.

At 10:55 a.m., 13 July, once again airborne, the balloon continued on its flight. Drizzle and fog caused ice to form on the envelope. The gondola dragged behind. After jettisoning hundreds of pounds of ballast and equipment, Örnen rose higher, but again settled toward the ice. The remaining guide rope was lost. Realizing that the end of the flight was inevitable, the crew opened to valves to release the hydrogen. The balloon settled to the ice, and at 8:11 p.m., 14 July 1897, the crew climbed down from the gondola onto the ice floe.

Örnen on the arctic ice, 14 July 1897 (Nils Strindberg)

The total elapsed time of the journey was 65 hours, 35 minutes. In that time, Andrée, Frænkel and Strindberg had traveled 295 miles (475 kilometers) from their starting point on Danskøya.

The next three months were a courageous battle for survival as the three explorers tried to make their way back to civilization. They reached Kvitøya (White Island), an ice-covered island at the northeast of the Svalbard Archipelago. Andrée’s final journal entry was made on 17 October.

The bodies of the three men were discovered in 1930. Their remains were taken to Sweden.

There is much speculation as to the cause of their deaths, ranging from exposure, exhaustion, illness, suicide, or bear attack.

Track of the 1897 Andrée Arctic Expedition.

The expedition left behind journals with detailed meteorological data and other observations. More than 200 photographic images were left on film negatives protected in metal canisters.

The 1897 Andrée Arctic Expedition is the subject of books, newspaper and magazine articles, at least one motion picture, as well as many Internet articles of varying detail. The images taken by Nils Strindberg are available on the Internet and tell of their experiences.

Salomon August Andrée (18 October 1854–1897)

¹ Geographic location of Örnen‘s landing site from the Comité International d’Aérostation (CIA, the Fédération Aéronautique Internationale Ballooning Commission).

© 2018, Bryan R. Swopes

13 July 1928

Maryse Bastie
Maryse Bastie (FAI)

13 July 1928, Mme Maryse Bastié flew her Caudron C. 109, F-AHFE, from Le Bourget airport, Paris, France, to Trzebiatów, Pomeranina, a distance of 1,058 kilometers (657.4 statute miles). (The Fédération Aéronautique Internationale records database does not show this record.) Mme Bastié is credited with eight FAI world records.

An FAI news article dated 28 July 2019 credits Maryse Bastié with being the first woman to have held a world record in aviation.¹

Maryse Bastié’s Caudron C. 109, F-AHFE. (FAI)

Mme Bastié’s airplane was a two-place, single-engine, Caudron C. 109 parasol-wing monoplane, F-AHFE, serial number 5804.1.

The C. 109 had a length of 6.440 meters (21 feet, 1.5 inches), wing span of 11.50 meters (37 feet, 8.8 inches) and height of 2.530 meters (8 feet, 3.6 inches). Its empty weight was 330 kilograms (727.525 pounds) and gross weight, 532 kilograms (1,173 pounds).

The standard C. 109 had a fuel capacity of 57 liters (15 U.S. gallons), and carried 15 litres (4 U.S. gallons) of lubricating oil for the engine. Its maximum speed was 120 kilometers per hour (75 miles per hour).

F-AHFE was powered by a naturally aspirated, air-cooled, 2,959.8 cubic centimeter (180.62 cubic inches) Société des Moteurs Salmson 9AD nine cylinder radial engine. The 9AD had a cylinder bore diameter of 69.9 millimeters (2.752 inches), and piston stroke of 85.7 millimeters (3.374 inches). It was rated at 45 ch at 2,000 r.p.m. The engine was 69.1 centimeters (27.20472 inches long and 63 centimeters (24.8031 inches) in diameter. It weighed 69.9 kilograms (154.1 pounds).

Salmson 9AD (NASM 2022-01819)

F-AHFE had set two FAI world records. On 25 October 1927, Raymond Delmotte flew over a closed circuit from Villacoublay to Saran in France, for a total distance of 1 535,20 kilometers (953.93 statute miles).² Two days later, 27 October 1927, Max Knipping flew from Le Bourget, Paris, France, to Königsberg, Germany, a distance of 1 581,84 kilometers.³

The airplane was first registered to M. Cuadron as F-ESDE, 06.11.25. It was the sold to M. Bastié at Issy. Later, Guy Bart, Chennevieres-sur-Marne; André Lemoine, Reims; and Pierre Gaston Lapanne at Nancy.

¹ The earliest record credited to Mme Bastié in the FAI online records database is Number 10446, 28 July 1929.  However, the database shows a number of earlier records credited to women: 12219, 2 January 1929, Evelyn Trout; 12216, 31 January 1929, Elinor Smith; 12220, 11 February 1929, Evelyn Trout; 12223, 17 March 1929, Louise McPhetridge; 12217, 24 April 1929, Elinor Smith; 12206, 28 May 1929, Marvel Crosson; 12214, 20 December 1928, Viola Gentry; 12221, 7 December 1928, Louise McPhetridge; 12212, 2 December 1928, Jane Heath; and 8221, 5 July 1927, The Hon. Bailey.

² FAI Record Number 9185

³ FAI Record 9166

© 2023, Bryan R. Swopes

13 July 1919

Airship R 34 over Pulham Airship Station, Norfolk, England, 1919.

13 July 1919: The Royal Air Force rigid airship R 34 completed its two-way crossing of the Atlantic Ocean and at 6:57 a.m. landed at Pulham Airship Station, Norfolk, England. The airship was under the command of Major George Herbert Scott, A.F.C., R.A.F. The total complement, including passengers, was 30 persons.

The return flight from Mineola, Long Island, New York took 73 hours, 3 minutes. According to records of the Fédération Aéronautique Internationale, the distance flown by R 34 on the return flight was 6,138 kilometers (3,814 miles).

This was the first “double crossing” by an aircraft. The round trip flight began at East Fortune Airship Station near Edinburgh, Scotland, on 2 July. The East-to-West crossing took 108 hours, 12 minutes.

Major Scott was appointed Commander of the Most Excellent Order of the British Empire.

This map shows the outbound and return tracks of His Majesty's Airship R 34, 2–13 July 1919.
This map shows the outbound and return tracks of His Majesty’s Airship R 34, 2–13 July 1919.

During the return flight on of the airship’s five engines suffered a broken connecting rod which damaged the cylinder block. It could not be repaired.

R 34 was based on extensive study of the captured German Zeppelin, L-33. It was built for the Royal Naval Air Service by William Beardmore and Company, Inchinnan, Renfrewshire, Scotland, but with the end of World War I, the RNAS and Royal Flying Corps were merged to become the Royal Air Force. 643 feet long (196 meters), with a maximum diameter of 78 feet, 9 inches (24 meters), the dirigible had a total volume of 1,950,000 cubic feet (55,218 cubic meters). The airship had a light weight metal structure covered with doped fabric. Buoyancy was provided by 55,185 cubic meters (1,948,840 cubic feet) of gaseous hydrogen contained in 19 gas bags inside the airship’s envelope. R 34 had a gross lift capacity of 59 tons. Useful lift was 58,240 pounds (26,417 kilograms).

The airship was powered by five water-cooled, normally-aspirated, 15.395-liter (989.483-cubic-inch-displacement) Sunbeam Maori Mk.IV dual overhead cam (DOHC) 60° V-12 engines with four valves per cylinder. The Mk.IV’s cylinder bore had been increased from 100 millimeters to 110 millimeters (3.94 to 4.33 inches), resulting in a larger displacement than previous Maori variants. The Maori Mk.IV was a direct-drive engine which produced 275 horsepower at 2,000 r.p.m. Each engine turned a two-bladed, 17 foot diameter (5.182 meter) propellers through a remote gearbox with a 0.257:1 reduction. The two wing engines were equipped with reversible gearboxes. With the engines turning 1,800 r.p.m., the R 34 had a cruising speed of 47 knots (54 miles per hour/87 kilometers per hour) and consumed 65 gallons (246 liters) of fuel per hour.

Airship R 34 landing at Pulham, Norfolk, 13 Juky 1919. (Getty Images/Jimmy Sime)
Airship R 34 landing at Pulham, Norfolk, 13 July 1919. (Getty Images/Jimmy Sime)

© 2017, Bryan R. Swopes

12 July 1956

U.S. Army Sikorsky H-34A Chocktaw, 56-4303, MSN 58-671. (Sikorsky Archives)

12 July 1956: Starting at 5:29 a.m., 12 July 1956, a Sikorsky H-34 Chocktaw, the U.S. Army variant of the S-58, flown by Captains Claude E. Hargett and Ellis D. Hill, near Milford, Connecticut, set three Fédération Aéronautique Internationale (FAI) world records for speed: over a 100 kilometers (62.1 statute miles) without payload, 228,39 kilometers per hour (141.92 miles per hour/123.32 knots);¹ 500 kilometers (310.7 statute miles) without payload, 218,89 kilometers per hour (136.01 miles per hour/118.19 knots);² and 1,000 kilometer (621.4 statute miles) circuit without payload, 213,45 kilometers per hour (132.63 miles per hour/115.3 knots).³ Captain Hargett was awarded a bronze oak leak cluster in lieu of a second award of the Distinguished Flying Cross. Captain Hill was awarded the Legion of Merit.

Captains Claude E. Hargett and Ellis D. Hill, U.S. Army, with a Sikorsky H-34A Chocktaw. (FAI)

The Dothan Eagle reported:

“RECORD HOLDERS—Captain Claude E. Hargett (left) of New Bern, N. C., and Ellis De. Hill of Birmingham [Alabama], both stationed at Fort Rucker are shown in the cockpit of an Army H-54 Sikorsky helicopter which they piloted to break three world speed records last month in a closed-circuit course at Milford, Conn. Both pilots, assigned to the Continental Army Command’s Board No. Six, reside at Enterprise.” (The Dothan Eagle)

Rucker Pilots Set 3 World Records

     FORT RUCKER — The establishment of three new world helicopter records by Fort Rucker Army pilots was announced yesterday by the Department of the Army. Flying an Army H-34 Sikorsky helicopter on July 12, over a course bordering a section of the southern Connecticut shore, Army aviators set a new closed-circuit record for 100, 500 and 1,000 kilometers. The old record had stood for a period of 10 years.

     The H-34, assigned to the Army Board Six of the Continental Army Command at Fort Rucker and piloted by Capt. Claude E. Hargett of New Bern, N. C., and Capt. Ellis D. Hill, Birmingham, set marks of 141.9 miles per hour for the 100 kilometer course, 136 for the 500 kilometers course, and 132.5 for the 1,000 kilometer course.

     Previous records for the same distances are 122.7, set in 1949 by a Sikorsky S-55; 66.6 mph set by a French SE 3-120 in 1950 and 66.6 mph in a Sikorsky R-5 in 1946.

     The special speed run was conducted by the Army under the supervision of Charles S. Logsdon, of the National Aeronautics Association in Washington, D.C.

     The records are subject to confirmation and acceptance by the Federation Aeronautique Internationale which is represented in the U. S. by the NAA.

     Recent reports indicate that Russia flew the 500-kilometer course at a speed of 116.2 miles an hour, approximately 20 miles an hour slower than the U. S. Army achieved.

     The USSR claim for the “hound helicopter” has been authenticated by the FAI in Paris, the world wide governing body for sporting aviation. The stock production model, the record H-34, is known commercially as the Sikorsky S-58.

     Capt. Hargett and Hill are presently stationed at Fort Rucker and both reside in Enterprise.

     The two record holders said they started the run at 5:20 a.m. near Milford, Conn. They flew about five hours at a height of 50 feet, with ninety per cent of the run made over water. An additional 3,000 pounds of gas was aboard the craft during the run.

     Both captains praise the Coast Guard which provided an auxiliary craft which followed the helicopter in the water as an added safety measure.

     Both are veterans of World War II and Korea. Hill has logged approximately 3,500 hours of flying time, Hargett, approximately 3,000 hours.

The Dothan Eagle, Vol. 48, No. 276, Tuesday, 7 August 1956, Page 8, Column 5

A U.S. Army Sikorsky H-34A Cocktaw, s/n 54-2873, landing at Fitzsimons Army Hospital, Aurora, Colorado. (Vertipedia)

The H-34A Chocktaw is a U.S. Army variant of the Sikorsky Model S-58, which had been developed as an internal project by Sikorsky, using the company’s own money. It was a major improvement of the earlier Model S-55 (H-19 Chickasaw/HO4S). The S-58 (a U.S. Navy XHSS-1 Seabat) first flew 8 March 1954.

The S-58 followed the single main rotor/tail (anti-torque) rotor configuration pioneered by Sikorsky with the Vought-Sikorsky VS-300 in 1939. The helicopter was designed to be flown by two pilots in a cockpit above the main cabin. Like the S-55, the engine was placed in the nose, installed at a 35° angle, and driving the transmission located behind the cockpit. For maintenance the engine could be accessed through two large clam shell doors in the nose. The wheeled landing gear was conventional, with two main wheels forward, and a tail wheel.

The S-58 fuselage had been designed using wind tunnel testing. The helicopter was built primarily of aluminum but the fuselage incorporated magnesium skin panels. The helicopter would be equipped with Automatic Stabilization Equipment (ASE), an autopilot system specifically for helicopters.

Sikorsky S-58 three-view illustration with dimensions. (Sikorsky)

The production H-34A was powered by an air-cooled, supercharged, Wright R-1820-84 nine-cylinder radial engine with a compression ratio of 6.80:1. It was rated at 1,525 horsepower at 2,800 r.p.m. for takeoff; 1,425 horsepower at 2,700 r.p.m., 30-minute limit; and 1,275 horsepower at 2,500 r.p.m., continuous. The R-1820-84 was 4 feet, 4.00 inches (1.321 meters) long, 4 feet, 7.74 inches (1.416 meters) in diameter and weighed 1,405 pounds (627 kilograms). The engine required 115/145 octane aviation gasoline.

The R-1820-84 drove the transmission through a 0.5625:1 gear reduction. The transmission had a gear reduction ratio of 11.293:1. Maximum main rotor speed was 258 r.p.m. (2,914 engine r.p.m.)

A U.S. Army Sikorsky H-34A Chocktaw, s/n 54-3033, MSN 58386.

The H-34 had an empty weight of 8,400 pounds (3,810 kilograms), and maximum takeoff weight of 13,300 pounds (6,032 kilograms). Its fuel capacity was 307 U.S. gallons (1,162 liters).

The helicopter had a cruise speed of 84 knots (97 miles per hour/156 kilometers per hour), and a maximum speed of 126 knots (145 miles per hour/233 kilometers per hour) at Sea Level. Its service ceiling was 17,600 feet (5,364 meters), and the hovering ceiling, out of ground effect, was 9,900 feet (3,018 meters) at takeoff power. The range was 227 nautical miles (261 statute miles/420 kilometers).

In transport configuration the S-58 could carry 16 troops or 6 litters and medical attendant.

The S-58 was built in a number of military and civil variants. Sikorsky built more than 1,800 S-58 series helicopters. Another 600 were produced by licensed manufacturers.

U.S. Army Sikorsky H-34A Chocktaw, s/n 57-1687.

¹ FAI Record File Number 13068

² FAI Record File Number 2155

³ FAI Record File Number 2154

© 2023, Bryan R. Swopes