Category Archives: Aviation

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 1968

General Dynamics FB-111A 67-0159, the first production aircraft. (U.S. Air Force)

13 July 1968: The first production General Dynamics FB-111A supersonic strategic bomber successfully completed a 30-minute maiden flight at Carswell Air Force Base, Fort Worth, Texas. The FB-111A differed from the F-111A fighter bomber with the substitution of a larger wing, originally designed for the F-111B, giving the bomber a 7 foot (2.134 meter) increase in wingspan. The landing gear was strengthened, the bomb bay enlarged, and it had more powerful engines.

Aardvark (Orycteropus afer)

The airplane’s very long nose earned the nickname “Aardvark,” but this did not become official until 1996.

67-0159 was delivered to the U.S. Air Force 4 September 1968 and assigned to the Air Force Flight Test Center, Edwards Air Force Base, California. (The first six production airplanes were used for flight testing.)

67-0159 was later converted to the F-111G configuration. In 1980 it was sent to the Sacramento Air Logistics Center to test weapons modifications and received a spectacular white and orange paint scheme. It was retired in 1990. 67-0159 is in the collection of the National Museum of the United States Air Force. It is on loan and now on display at the Aerospace Museum of California, Sacramento, California.

General Dynamics FB-111A-CF (F-111G) 67-159

The General Dynamics FB-111A is a two-place, twin-engine, strategic bomber with variable-sweep wings, assigned to the Strategic Air Command. It is 73.54 feet (22.415 meters) long. The wingspan varies from a maximum 70.0 feet (21.336 meters) when fully extended, and a minimum 33.96 feet (10.351 meters) when swept fully aft. Overall height is 17.04 feet (5.194 meters).

The wings of the FB-111A have a total area of 550 square feet (51.10 square meters). When fully extended, the wings’ leading edges are swept aft to 16.0°. The angle of incidence at the root is +1° and -3° at the tip. There is 1.0° dihedral.

The Aardvark’s empty weight is 47,481 pounds (21,537 kilograms). Normal maximum takeoff weight is 116,115 pounds (52,669 kilograms), and the maximum overload takeoff weight is or 119,243 pounds (54,088 kilograms).

The aircraft is powered by two Pratt & Whitney TF30-P-107 engines. This is a two-spool axial-flow turbofan engine with afterburner. It has a 3-stage fan section, 13-stage compressor section (6 low- and 7 high-pressure stages) and 4-stage turbine (1 high- and 3 low-pressure stages). The -107 has a maximum continuous power rating of 10,800 pounds of thrust (48.041 kilonewtons) at 14,150 r.p.m., N2 (static thrust, at Sea Level), and a maximum power rating of 20,350 pounds (90.521 kilonewtons) at 14,550 r.p.m., N2 (45 minute limit) The T30-P-107 is 3 feet, 2.12 inches (0.968 meters) in diameter, 20 feet, 1.4 inches (6.132 meters) long,  and weighs 4,121 pounds (1,869 kilograms).

The FB-111A has an average cruise speed of 415–442 knots (478–509 miles per hour/769-819 kilometers per hour), depending on the mission profile. It’s maximum speed at 50,000 feet (15,240 meters) is 1,262 knots (1,452 miles per hour/2,337 kilometers per hour)—Mach 2.20. The bomber’s service ceiling varies from 50,390 feet to 56,380 feet (15,359–17,185 meters), again, depending on the mission profile. The maximum combat range is 4,920 nautical miles (5,662 statute miles/9,112 kilometers). The airplane can carry as many as six 600 gallon (2,271 liter) external tanks on underwing pylons. This gives the Aardvark a maximum ferry range of 4,313 nautical miles (4,963 statute miles/7,988 kilometers).

General Dynamics FB-111A 67-0159. (fb111.net)
General Dynamics F-111A 66-0011, a test airplane in the FB-111A program, loaded with four AGM-69 SRAM missiles. The dots on the missiles and airplane are for precise tracking from ground stations. (U.S. Air Force)

The FB-111A could carry weapons in an internal bomb bay or on underwing hardpoints. It could be armed with up to 37,500 pounds (17,010 kilograms) of conventional bombs; or six AGM-69A Short Range Attack Missiles (SRAM). The Aardvark could carry maximum of six nuclear weapons (B-43, B-57 or B-61).

General Dynamics YFB-111A 63-9783, the prototype strategic bomber variant. (U.S. Air Force)

In addition to a prototype (63-9783, which was converted from the last production F-111A) General Dynamics built 76 FB-111A strategic bombers. With the introduction of the Rockwell B-1B Lancer, the FB-111As remaining in service were converted to F-111G tactical fighter bombers. They were retired by 2003.

The Royal Australian Air Force bought 15 of the F-111Gs. By 2007, these had also been taken out of service.

Two General Dynamics FB-111As in formation, 1 December 1983. (MSGT Buster Kellum, U.S. Air Force)

© 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

13 July 1916

Colonel Raynal Cawthorne Bolling, Signal Corps, U.S. Army
Lieutenant Colonel Raynal Cawthorne Bolling, Signal Corps, U.S. Army Reserve
1st Aero Squadron, New York National Guard, mobilized for Federal Service, 13 July 1916.
1st Aero Squadron, New York National Guard, mobilized for Federal Service, 13 July 1916.

13 July 1916: The 1st Aero Company, New York National Guard, under the command of Captain Raynal Cawthorne Bolling, became the first national guard unit to be mobilized into federal service in answer to the border crisis with Mexico. The unit trained at Mineola, New York, along the 2nd Aero Company, but did not deploy to the border.

Bolling was promoted to the rank of Colonel, Signal Corps, United States Army, 8 August 1917. Colonel Bolling was killed in action near Estrées-Deniécourt, France, 26 March 1918. As of that time, he was the highest-ranking U.S. officer to be lost during World War I. Bolling Field, the Air Corps station at Washington, D.C., was named in his honor.

The 1st Aero Company is the oldest Air National Guard unit. Today, it is 102nd Rescue Squadron, New York Air National Guard.

© 2016, Bryan R. Swopes