Category Archives: Aviation

8 October 1883

Tissandier
Gaston Tissandier (left) and Albert Charles Tissandier (Fine Art America)

8 October 1883: The first airship powered by an electric motor was flown by brothers Albert-Charles Tissandier (1839–1906) and Gaston Tissandier (1843–1899) at at Auteuil, a suburb of Paris, France.

The brothers were experienced aeronauts, having designed and built a number of balloons.

Gaston Tissandier described the event in La Nature:

     From the end of September the gas apparatus was ready to operate., the balloon was stretched out upon the ground, under a long movable tent, so that it could be at once inflated; the car and motor were stored away under a shed, and my brother and I awaited fine weather in order to perform our experiment.

     On Saturday, the 6th, a high barometer was noted, and on Sunday, the 7th, the weather became fine, with a slight wind, and we therefore decided that the experiment should be made the next day, Monday, October 8.

     The inflating of the balloon was begun at 8 o’clock in the morning, and was continued uninterruptedly until half-past two in the afternoon. This operation was facilitated by the equatorial cords which hung from the right and left of the balloon, and along which were let down the bags of ballast. These cords are shown in Fig. 2, which gives a front view of the balloon. The aerial ship having been completely inflated, the car was at once fixed in place along with the ebonite reservoirs, each containing 30 liters of acid solution of bichromate of potash. At twenty minutes past three, after piling up the ballast in the car and balancing the latter, we slowly ascended into the air through a slight E.S.E. wind.

     At the surface the wind was nearly null, but, as frequently happens, it increased in velocity with altitude, and we ascertained by the movement of the balloon over the earth that it attained at a height of 500 meters a velocity of 3 meters per second.

     My brother was specially occupied in regulating the ballast in order to keep the balloon at a constant altitude, and not far from the surface of the earth. The balloon hovered over the earth very regularly at a height of four or five hundred meters. It remained constantly inflated, and the gas in excess escaped through expansion by opening, under its pressure, the lower automatic safety valve, the operation of which was very regular. . .

At thirty-five minutes past four we effected our descent upon a large plain in the neighborhood of Croissy-sur-Seine, where the maneuvers connected with landing were performed by my brother with complete success. We left the balloon inflated all night, and, on the next morning, it was found not to have lost the least quantity of gas, but was as fully inflated as on the preceding eve. . . .

—Translation of La Nature article published in Scientific American Supplement, Vol. XVI., No. 416, 22 December 1883, at Pages 6632–6634

This engraving by E.A. Tilly depicts Albert Tissandier (left) and Gaston Tissandier (right) in the gondola of their airship. A an unidentified third man is above. (Library of Congress Prints and Photographs Division)

The Tissandier brothers’ dirigible was the first to be powered by electricity. A 1.5 horsepower Siemens electric motor, turning 180 r.p.m., drove a two-bladed propeller through a reduction gear, producing 26 pounds of thrust (116 newtons). 24 bichromate of potash (potassium bichromate) cells provided electricity for the motor, which propelled the airship at 3 miles per hour (4.8 kilometers per hour).

The airship was 28 meters (91 feet, 10 inches) long with a maximum diameter of 9.2 meters (30 feet, 2 inches). Its gas capacity was 1,060 cubic meters (37,434 cubic feet). The total weight of the airship, with “two excursionists,” instruments and ballast, was 1,240 kilograms (2,734 pounds).

Scientific American described the airship:

“. . . It was constructed by Mr. Albert Tissandier, who very happily replaced the usual netting by a suspension covering formed of ribbons sewed to the longitudinal elliptical strips, according to the geometrical diagram. This suspension covering is fixed upon the sides of the balloon to two flexible rods which accurately adapt themselves to its form from one extremity to the other, and keep the entire affair in shape. To the lower part of the suspension covering there is attached a netting that terminates in twenty suspension ropes which support the car by its four upper corners.

     “The car is in the shape of a cage and is constructed of bamboos, which are strengthened by cords and gutta-percha-covered copper wires. The suspension ropes are connected together horizontally by a ring formed of cordage fixed two meters above the car. To this ring, which distributes the traction equally during a descent, are attached the stoppage apparatus—the guide rope and the anchor-line. The rudder which consists of a large surface of unvarnished silk held in place by a bamboo rod, is also fitted to the stern. The car contains the motor, which is formed of 24 bichromate of potash elements that actuate a Siemens dynamo which is connected with the helix through the intermedium gearing. The motor has a power of 100 kilogrammeters, equivalent to that of 10 meu, and drives the helix, which is about 3 meters [9 feet, 10 inches] in diameter, at the rate of 180 revolutions per minute.”

Scientific American Supplement, Vol. XVI., No. 416, 22 December 1883, at Page 6631

This engraving by E.A. Tilly depicts the Tissandier electric airship departing Auteuil, Paris, 8 October 1883. (Library of Congress Prints and Photographs Division)
This engraving by E.A. Tilly depicts the Tissandier electric airship departing Auteuil, Paris, 8 October 1883. (Library of Congress Prints and Photographs Division)

© 2018, Bryan R. Swopes

7 October 1963

Prototype Learjet 23 N801L, first flight, 7 October 1963. (Lear)
Prototype Learjet 23, N801L, first flight, 7 October 1963. (Lear Jet Corporation)

7 October 1963: The first of two Learjet 23 prototypes, N801L, makes its first flight at Wichita, Kansas, with test pilots Henry Grady (“Hank”) Beaird, Jr., and Robert S. Hagan. A light twin-engine business jet, the Learjet 23 is considered a “first” because it was designed from the start as a civil aircraft.

The Learjet 23 is operated by two pilots and can carry six passengers. It is 43 feet, 3 inches (13.183 meters) long with a wingspan of 35 feet, 7 inches (10.846 meters) and overall height of 12 feet, 7 inches (3.835 meters). It has an empty weight of 6,150 pounds (2,790 kilograms) and maximum takeoff weight of 12,499 pounds (5,670 kilograms).

A characteristic of all Learjets is the 13° sweep of their wings’ leading edges, and the straight trailing edge.

Learjet 23 N802L was the second prototype. This airplane is in the collection of the Smithsonian Instititution National Air and Space Museum. (NASM 9A11735)

The airplane was powered by two General Electric CJ610-4 turbojet engines. The CJ610 is a single-shaft axial-flow turbojet with an 8-stage compressor and 2-stage turbine. The CJ610-4 has a maximum continuous power rating of 2,700 pounds (12.010 kilonewtons) at 16,500 r.p.m. at Sea Level, and 2,850 pounds of thrust (12.677 kilonewtons) at 16,700 r.p.m., for takeoff (5 minute limit). The engine is 3 feet, 4.50 inches (1.029 meters) long, 1 foot, 5.56 inches (0.446 meters) in diameter, and weighs 403 pounds (183 kilograms).

The Learjet 23 has a cruise speed of 518 miles per hour (834 kilometers per hour) at 40,000 feet (12,192 meters) and a maximum speed of 561 miles per hour (903 kilometers per hour), 0.82 Mach, at 24,000 feet (7,315 meters). The service ceiling is 45,000 feet (13,716 meters) and its maximum range is 1,830 miles (2,945 kilometers).

Lear Jet Corporation built approximately 100 Learjet 23s.

The first prototype was damaged beyond economical repair while simulating an engine failure on takeoff during flight testing, 4 June 1964. The accident was attributed to pilot error. N801L had accumulated just 194 flight hours.

© 2018, Bryan R. Swopes

7 October 1919

Anthony Plesman
Albert Plesman, founder of Koninklijke Luchtvaart Maatschappij N.V. (KLM)

7 October 1919: Koninklijke Luchtvaart Maatschappij N.V., operating under the name KLM Royal Dutch Airlines, was founded on 7 October 1919 by Albert Plesman, making it the oldest carrier in the world still operating under its original name, though the company stopped operating during the Second World War—apart from the operations in the Dutch Antilles in the Caribbean.

The Airco DH.16, G-EALU, with which KLM flew its first scheduled passeneger service.
KLM flew its first scheduled passenger service with this Airco DH.16, G-EALU, from Croydon to Amsterdam, 17 May 1920. (Unattributed)

The first KLM flight was on 17 May 1920, from Croydon Airport, London, to Amsterdam, The Netherlands, carrying two British journalists and a number of newspapers. It was flown by an Airco DH.16, registration G-EALU, piloted by Henry (“Jerry”) Shaw.¹ This airplane, named Arras, was leased from Aircraft Transport and Travel Limited, a British company. Shaw was that company’s chief pilot.

In 1920 KLM carried 440 passengers and 22 tons of freight. In 1921 KLM started scheduled services.

As of 31 December 2023, KLM’s fleet included 238 aircraft. The airline had approximately 35,145 employees.

A KLM Boeng 787 Dreamliner. (KLM)
A KLM Boeing 787 Dreamliner. (KLM)

¹ Please see Henry “Jerry” Shaw (1892–1977), an article by Katy Whitaker, English Heritage, 2014, at Britain from Above: http://britainfromabove.org.uk/sites/default/files/Shaw_Final.pdf

© 2024, Bryan R. Swopes

6 October 1983

A flight of two U.S. Army OH-58D Kiowa Warrior scout helicopters. (Bell Helicopter)
A flight of two U.S. Army OH-58D Kiowa Warrior scout helicopters. (Bell Helicopter)

6 October 1983: First flight of the Bell Helicopter Company Model 406/OH-58D Kiowa reconnaissance helicopter. Developed from the earlier Model 206/OH-58A and OH-58C Kiowa, the D model features a four-blade composite main rotor, an upgraded engine and transmission, and improved avionics. The most visible features are the spherical mast-mounted sighting system above the main rotor and much larger engine/transmission cowling, or “dog house.”

The helicopter was designed with very low level, “nap-of-the-Earth,” (NOE) flight, using terrain and trees for cover. The four-bladed rotor provides more lift and increased responsiveness over the two-bladed semi-rigid rotor of the OH-58A and C.

The mast-mounted sight allows the helicopter to hover behind terrain or trees with just the sight exposed. The sight contains television, thermal imaging and laser range-finding and target designation equipment.

The instrument panel of a Bell OH-58D Kiowa. (Bell helicopter)
The instrument panel of a Bell OH-58D Kiowa. (Bell Helicopter)

Operated by two pilots, the Bell OH-58D Kiowa is 42 feet, 2 inches (12.852 meters) long, with rotors turning. The four-bladed composite main rotor has a diameter of 35 feet (10.668 meters). As is customary with American-designed helicopters, the main rotor turn counter-clockwise as seen from above. (The advancing blade is on the right side of the aircraft.) The two-blade semi-rigid tail rotor is mounted on the left side of the tail boom and turns clockwise when seen from the left. (The advancing blade is below the tail boom.) The overall height of the OH-58D is 12 feet, 10–5/8 inches (3.928 meters). Empty weight of the helicopter is about 3,500 pounds (1,588 kilograms), depending on installed equipment. This is approximately 15% greater than the maximum gross weight of the OH-58A. The OH-58D has a maximum gross weight of 5,500 pounds (2,495 kilograms).

Power for the Kiowa is supplied by a Rolls-Royce T703-AD-700A (Allison 250-C30R3) turboshaft engine which produces 750 shaft horsepower. The main transmission is limited to transient input of 637 shaft horsepower.

The helicopter can be armed with a fixed, remotely-fired, M3P .50-caliber (12.7 mm) machine gun, a pod carrying seven 2.75-inch (70 mm) rockets, or two AGM-114 Hellfire antitank guided missiles.

The OH-58D has a cruise speed of 95 knots (109 miles per hour/176 kilometers per hour) when armed. Its range is 140 nautical miles (161 miles/259 kilometers). The hover ceiling in ground effect (HOGE) at +15 °C. is 7,500 feet MSL (2,286 meters).

An OH-58D Kiowa decelerates as it approaches trees at Fort Lewis, Washington.( U.S. Army)
An OH-58D Kiowa decelerates as it approaches trees during gunnery exercises at Fort Lewis, Washington. A .50-caliber machine gun is mounted on the left side of the helicopter. (U.S. Army)

© 2015, Bryan R. Swopes

6 October 1977

The first prototype Mikoyan MiG 29A, 9-01, ("01 Blue") on display at the Central Air Force Museum, Monino. (Detail from image by AVIA BavARia/Wikipedia)
The first prototype Mikoyan MiG 29A, 9-01, (“01 Blue”) on display at the Central Air Force Museum, Monino. (Detail from image by AVIA BavARia/Wikipedia)
Alexander Vasilyevich Fedotov (1932–1982)
Alexander Vasilievich Fedotov

6 October 1977: The first of eleven prototypes of the Mikoyan MiG 29A fighter, 9-01, made its first flight at Ramenskoye Airfield with Chief Test Pilot Alexander Vasilievich Fedotov, Hero of the Soviet Union, in the cockpit.

Fedotov had been a test pilot at A.I. Mikoyan EDB since 1958 and set eighteen speed and altitude world records flying high performance aircraft. He was killed while testing the MiG 31 in 1984.

The MiG 29A is a fourth generation, single-seat, twin-engine, Mach 2+ air superiority fighter built by the Mikoyan Design Bureau. It entered service with the Soviet Union in 1983 and has been widely exported to many other nations. The MiG 29A is 13.37 meters (57 feet) long and has a wing span of 11.4 meters (37 feet, 3 inches). Its empty weight is 11,000 kilograms (24,250 pounds) and the maximum takeoff weight (MTOW) is 20,000 kilograms (44,100 pounds). The fighter is powered by two Klimov RD-33 turbofan engines which produce 11,240 pounds of thrust, or 18,277 pounds of thrust with afterburner. It has a maximum speed of Mach 2.25 (1,490 miles per hour/2,400 kilometers per hour) and a service ceiling of 59,100 feet (18,013 meters). Maximum range with internal fuel is 1,430 kilometers (888 miles).

Armament consists of one Gryazev-Shipunov GSh-301 30mm autocannon with 150 rounds of ammunition and a combination of air-to-air missiles, rockets or bombs carried on underwing pylons or fuselage hard points.

More than 1,600 MiG 29s have been built.

Mikoyan MiG 29SMT RF-92934 ("22 Red"),Russian Air Force. (Alex Beltyukov/Wikipedia)
Mikoyan MiG 29SMT RF-92934 (“22 Red”), Russian Air Force. (Alex Beltyukov/Wikipedia)

Alexander Vasilievich Fedotov born 23 June 1932 at Stalingrad, Russia (renamed Volgograd in 1961). He graduated from the Air Force Special School at Stalingrad,  and in 1950, entered the Soviet Army. Fedotov attended the Armavir Military Aviation School of Pilots at Amravir, Krasnodar Krai, Russia, graduating in 1952, and then became a flight instructor. In 1958 he attended the Ministry of Indutrial Aviation Test Pilot School at Zhukovsky. He was a test pilot for the Mikoyan Experimental Design Bureau from 1958 to 1984. In 1983, Alexander Fedotov was promoted to the rank of Major General in the Soviet Air Force.

On 22 July 1966, Fedotov was honored as a Hero of the Soviet Union. He was named an Honored Test Pilot of the Soviet Union, 21 February 1969. He was qualified as a Military Pilot 1st Class. Fedotov was twice awarded the order of Lenin, and also held the Order of the Red Banner and the Order of the Red Banner of Labor.

During his career as a test pilot, Major General Fedotov had been forced to eject from an airplane three times. He had also set 15 Fédération Aéronautique Internationale world records for speed, altitude and time to altitude. One of these, FAI Record File Number 2825, in which he flew a Mikoyan E-266M to 37,650 meters (123,534 feet), 31 August 1977, remains the current record. The FAI has also honored him three times (1961, 1973 and 1977) with The De la Vaulx Medal, and in 1976 awarded him the FAI’s Gold Air Medal.

Major General Alexander Vasilyevich Fedotov and his navigator, Valerie Sergeyvich Zaytevym, were killed when the second MiG 31 prototype, number 83/2, crashed during a test flight. Neither airman was able to eject.

Major General Federov
Major General Alexander Vasilyevich Federov, Hero of the Soviet Union

© 2016, Bryan R. Swopes