23 September 1913: Pioneering aviator Eugène Adrien Roland Georges Garros (6 October 1888–5 October 1918) was the first pilot to fly across the Mediterranean Sea.
At 5:47 a.m., he departed Fréjus, Côte d’Azur, France, in a Morane-Saulnier G and flew to Bizerte, Tunisia, 470 miles (756 kilometers) to the south-southeast. He arrived at 1:40 p.m., having been airborne 7 hours, 53 minutes.
Reportedly, the airplane carried sufficient fuel for just 8 hours of flight. According to a contemporary report, only 5 liters (1.32 U.S. gallons) of fuel remained when he landed.
Garros flew on to Kassar Said Aerodrome the following day. His airplane was then dismantled and shipped back to France.
On 15 October 1913, Roland Garros was appointed Chevalier de la légion d’honneur.
The Aéroplanes Morane-Saulnier Type G was a two-place, single-engine monoplane, which had first flown in 1912. The airplane used wing-warping for roll control. It’s landing gear consisted of two wheels and a tail skid. The wooden framework was primarily ash and was covered in fabric. The airplane was 21 feet, 6 inches (6.553 meters) long with a wingspan of 30 feet, 6 inches (9.296 meters). The wing had a chord of 6 feet, 0 inches (1.829 meters), no dihedral, and the wingtips were swept. The airplane had an empty weight of 680 pounds ( 308 kilograms) and a maximum weight of 1,166 pounds (529 kilograms).
The pilot’s instrument panel had a revolution indicator (tachometer), a barograph, and a compass.
The Morane-Saulnier G was powered by an air-cooled 11.835 liter (722.22 cubic inches) Société des Moteurs Gnome Lamda seven-cylinder rotary engine with a single Bosch magneto, with a nominal rating of 80 horsepower (one source indicates that the engine actually produced 67.5 horsepower at 1,250 r.p.m.), and driving a laminated walnut Chauvière Hélice Intégrale fixed-pitch propeller which had a diameter of 7 feet, 10 inches (2.570meters).
The airplane had a 14 gallon ¹ (63.65 liters) main fuel tank near the engine, and a second 8 gallon (36.37 liters) tank in the cockpit. Fuel had to be transferred forward by using a hand-operated pump. A 5 gallon (22.73 liters) tank for lubricating oil was adjacent to the main fuel tank.
Garros’ airplane maintained an average speed of 59.5 miles per hour (96 kilometers per hour) for this flight. The Morane-Saulnier G had a maximum speed of 76 miles per hour (122 kilometers per hour).
The Morane-Saulnier G was produced under license by Grahame-White Aviation Company, Hendon Aerodrome, London, England, and by Dux at Moscow, Russia. More than 150 Type Gs were built.
Roland Garros was born 6 October 1988 at Saint-Denis, Réunion (an island in the Indian Ocean). He was the son of Antoine Georges Garros and Maria Clara Emma Faure Garros. Garros was a racer and test pilot who had set many aviation records, including a Fédération Aéronautique Internationale World Altitude Record of 5,610 meters (18,406 feet), set 11 September 1912 at Saint-Brieuc, France. ²
Garros flew in World War I as a fighter pilot for France and shot down a total four enemy airplanes. Garros’ airplane went down behind enemy lines and he was captured, 18 April 1915. He escaped nearly three years later and returned to France. For his military service, he was promoted to Officier de la Légion d’honneur, 6 March 1917. He was also awarded the Croix de Guerre.
Lieutenant d’infantrie Eugène Adrien Roland Georges Garros, Officier de la Légion d’honneur, Aéronautique Militaire, flying a SPAD S.XIII C.1, Nº. 15403, was shot down by the German ace, Leutnant Hermann Habich, near Vouziers, France, 5 October 1918. He was killed one day before his 30th birthday.
Stade Roland Garros in Paris, the tennis stadium where the French Open is held, was named in honor the pioneering aviator.
¹ Fuel and oil capacities from a British publication, so quantities are presumably Imperial gallons.
21 September 1937: Jackie Cochran flew the Seversky Aircraft Corporation SEV-1XP, registered R18Y, over a 3 kilometer (1.864 statute miles) course at Detroit Wayne County Airport, Romulus, Michigan. The average speed for six passes was 470.40 kilometers per hour (292.29 miles per hour). This was a new Fédération Aéronautique Internationale (FAI) world speed record.¹
The Lansing, Michigan, State Journal reported:
New York Aviatrix Smashes the Feminine World’s Speed Record at Detroit
BETTERS MARK SET BY FRENCH WOMAN
Jacqueline Cochran Averages Speed of 293.05 M.P.H. In 3-Kilometer Flight
DETROIT, Sept. 21 (AP)—Jacqueline Cochran, New York aviatrix, averaged 293.05 miles an hour in four flights over a three-kilometer course Tuesday, bettering the women’s land plane speed record of 276.527 miles an hour established in 1934 by the late Helene Boucher of France.
Miss Cochran made six flights, three east and three west, over the course, but only four of the flights were included in the official computation. She was timed at 304.62 miles an hour in her fastest dash, an eastward flight. Her speed on the slowest flight was 282.06 miles an hour.
All of the flights were at altitudes of between 100 and 150 feet, thus complying with a National Aeronautics association [sic] rule that flights for records must be made below 250 feet.
Miss Cochran flew a Seversky military pursuit demonstrator, with a 1,200 horsepower engine. The plane is of a type similar to a fleet soon to be put in use at Selfridge field, Mt. Clemens, Mich.
“Ever since I started flying, five years ago, I’ve dreamed of doing this,” Miss Cochran said when she was notified of her record speed.
Her record attempt, made at the Wayne county airport, was postponed four times by adverse winds. She had perfect weather conditions Tuesday.
Airport officials said Miss Cochran’s flights were the fastest ever flown at the airport, by either a man or a woman.
—The State Journal, Vol. 83, Tuesday, 21 September 1937, Page 8, Column 1
For this and her other accomplishments, Ms. Cochran was awarded the Harmon International Aviatrix Trophy by Mrs. Franklin D. Roosevelt in a ceremony in New York City, 4 April 1938.
The Seversky SEV-1XP (also called the “SEV-S1 Executive”) was the original prototype for a fly-off against the Curtiss-Wright Model 75 Hawk and Northrop 3A improved version of the P-35 fighter, which was designed by Alexander Kartveli. The P-35 was the first U.S. Army Air Corps single-engine airplane to feature all-metal construction, an enclosed cockpit and retractable landing gear.
The airplane had originally been built as a single-place, open cockpit monoplane with fixed landing gear. It was designated the Seversky II X, s/n 2, and given the experimental registration mark X18Y. In order to compete for the Army Air Corps pursuit contract of 1935, X18Y was modified into a two-place fighter with an enclosed canopy. It was armed with two machine guns mounted in the engine cowling, while a gunner sat behind the pilot with a third machine gun on a flexible mount. Still officially the Seversky II X, the company called it the SEV-2XP.
In this configuration, X18Y was powered by an experimental air-cooled, supercharged, Wright Aeronautical Division GR1670A1 Whirlwind. This was a two-row, 14-cylinder radial engine with a displacement of 1,666.860 cubic inches (27.315 liters). It had a compression ratio of 6.75:1 and required 87-octane gasoline. The GR1670A1 had a normal power rating of 775 horsepower at 2,400 r.p.m., and 830 horsepower at 2,400 r.p.m. for takeoff. It drove an experimental three-bladed Hamilton Standard constant-speed propeller through a 16:11 gear reduction. The GR1670A1 was 45 inches (1.143 meters) in diameter, 52-25/32 inches (1.341 meters) long, and weighed 1,160 pounds (526 kilograms).
In mid-May 1935, Major de Seversky flew the prototype from the factory at Farmingdale, New York, toward Wright Field, Dayton, Ohio. The engine overheated, then seized, and Seversky made a forced landing on a small hilltop airfield near St. Clairsville, Ohio. X18Y suffered slight damage. A local pilot flew Seversky on to the meeting at Wright. Once there, he saw the Curtiss-Wright and Northrop competition, both single-place pursuits with retractable landing gear. The SEV-2XP was outclassed.
After repairs, on 20 June Seversky flew X18Y out of the small field and returned it to Farmingdale. It was extensively reconfigured as a single-place airplane. A new wing with retractable landing gear was installed, as were new tail surfaces. A Wright Cyclone R-1820G4 9-cylinder radial engine replaced the experimental GR1670A1. The G4 had a normal power rating of 810 horsepower at 2,100 r.p.m., and 1,000 horsepower at 2,200 r.p.m., using 87-octane gasoline. Seversky redesignated X18Y as the SEV-1XP. After a fly off with the modified prototype, the Air Corps placed an order for 100 Seversky P-35s.
Seversky continued to experiment with new engines, installing a GR-1820G5. In January 1937, a change was made to the Pratt & Whitney Twin Wasp R-1830-13, the same engine being installed in production Curtiss-Wright P-36 Hawks. This was a two-row, supercharged 14-cylinder radial engine with a normal power rating of 900 horsepower at 2,550 r.p.m. to an altitude of 10,000 feet (3,048 meters), and 1,050 horsepower at 2,700 r.p.m. for takeoff. The airplane retained the same three-bladed constant -speed Hamilton Standard propeller which had been used with the Wright Cyclone engine. It was driven through a 3:2 gear reduction.
X18Y was reconfigured as a two-place civilian transport, with a small passenger cabin below and behind the cockpit. There were two fixed windows on the left side of the fuselage, and the passenger entered through a hatch on the right side, over the wing. A Pratt & Whitney Twin Wasp SB-G was fitted. This engine was very slight smaller and weighed lest than the R-1830-13, and had a normal rating of 900 horsepower at 2,450 r.p.m. to 6,500 feet (1,981 meters), and 1,000 horsepower at 2,600 r.p.m. for takeoff.
In this new configuration the SEV-1XP was called the “SEV-S1 Executive.” The experimental registration was changed to restricted: R18Y.
On 4 September 1937, R18Y was flown by Seversky’s chief test pilot, Frank Sinclair, in the cross-country Bendix Trophy Race. It carried the race number 63 on the vertical fin. Sinclair finished in fourth place, 33 minutes behind Jackie Cochran in her green Beechcraft D17W Staggerwing. He then flew R18Y in the Thompson Trophy pylon race, again finishing fourth with an average of 252.360 miles per hour (406.134 kilometers per hour).
On 27 October the SEV-1XP reverted to its experimental license number, X18Y.
Ms. Cochran continued to fly the Seversky in speed record attempts. On 3 December she flew it from Floyd Bennett Field in New York to Miami, Florida, in an elapsed time of 4:12:27.2, averaging 278.13 miles per hour (447.61 kilometers per hour).
On 9 December Jackie flew X18Y to a new U.S. national record speed of 252.875 miles per hour (406.963 kilometers per hour) over a 100-kilometer course. She was attempting to increase the her speed on 13 December, reaching an average 255.973 miles per hour (411.949 kilometers per hour).
When she landed at Miami after the record runs, the Seversky’s tail wheel began rapidly swinging from side to side. This was something that the P-35s were experiencing and a number of the fighters had been wrecked. Jackie said, “One wing was pulled off altogether and the landing gear was torn off,” she said. “The tail [wheel] had jumped its lock throwing the plane to one side.”
The SEV-1XP was damaged beyond economical repair. In less than three years it had served its purpose. Seversky would build a new airplane. X18Y’s registration was suspended 4 January 1938 and the airplane was scrapped.
19 September 1969: After four days of testing in a tethered hover, OKB Mil Design Bureau test pilot Herman V. Alferov made the first free flight of the prototype Mil Mi-24 attack helicopter, V-24.
Designed by a team led by Chief Project Engineer V. A. Kuznetsov, the Mi-24 used the drive train of the Mil Mi-8 Hip-B/C transport and Mi-14 Haze-A anti-submarine helicopters. It had a five-blade main rotor. a three-blade tail rotor and was equipped with retractable tricycle landing gear.
The Mi-24 (named “Hind” by NATO forces) was operated by a pilot and a weapons system operator seated in tandem configuration, with the pilot slightly offset to the left. The gunner is in the forward position. It differed from the American Bell AH-1G Cobra attack helicopter in that it could carry 8 troops or 1,500 pounds (680 kilograms) of cargo in a center fuselage compartment.
The Mi-24 is 17.5 meters (57 feet, 5 inches) long, 6.5 meters (21 feet 4 inches) high, with a main rotor diameter of 17.3 meters (56 feet, 9 inches). As is standard practice with Soviet helicopters, the five-blade main rotor turns clockwise as seen from above. (The advancing blade is on the left.) The tail rotor diameter is 3.9 meters (12 feet, 9½ inches).
The entire fuselage is tilted 2° 30′ (and thus, the transmission, mast and main rotor) to the right to counteract the rotor system’s translating tendency, and helps with high-speed stability.
In early versions, the tail rotor was mounted on the right side in pusher configuration and rotated counter-clockwise as seen from the left. (The advancing blade is above the axis of rotation.) Because of poor handling conditions, the tail rotor was changed to the left side in tractor configuration, with the advancing blade below the hub.
The helicopter’s empty weight is 8,500 kilograms (18,739 pounds) and loaded weight is 12,000 kilograms (26,455 pounds).
Power is supplied by two Isotov TV3-117 turboshaft engines rated at 1,700 shaft horsepower, or 2,200 horsepower for takeoff or one engine inoperative emergency operation.
The Mi-24 has a maximum speed of 335 kilometers per hour (208 miles per hour) and range of 450 kilometers (280 miles). The service ceiling is 4,500 meters (14,764 feet).
Armament consists of a turret-mounted Gryazev-Shipunov GSh-23 23mm cannon with 450 rounds of ammunition. Air-to-air and air-to-ground missiles are carried on pylons mounted under the helicopter’s stub wings.
More than 5,200 Mi-24 attack helicopters have been built, many of them exported. It is estimated that the cost of an individual helicopter is $32,500,000.
Herman V. Alferov (Алфёров Герман Витальевич)—also known as G.V. Alferov or German V. Alferov—was born at Moscow, Russia, U.S.S.R., 11 April 1934. He graduated from the 3rd Moscow Flying Club in 1950, and from 1952 to 1954 was a flight instructor at the Central Aeroclub Chkalov. In 1954, He graduated from the Voluntary Society of Assistance to the Air Force (DOSAAF) central flight technical school at Saransk in the Mordovian Autonomous Oblast.
Alferov was employed as a test pilot at OKB Mil in Moscow from 1954 until 1982, and remained with the flight test center until 1992. He participated in setting 11 Fédération Aéronautique Internationale (FAI) world helicopter records, and was named an Honored Test Pilot of the Soviet Union, 16 November 1973. In 1977, he was awarded the Order of the October Revolution, twice received the Order of the Red Banner of Labor, and twice the Order of the Red Star.
14–18 September 1984: Colonel Joseph W. Kittinger II, United States Air Force (Retired), lifted of from Caribou, Maine, at the extreme northeast corner of the United States, aboard Rosie O’Grady’s Balloon of Peace, a 3,000-cubic-meter Yost GB55 helium-filled balloon, registered N53NY. 86 hours later, he came rest at Montenotte, Italy, having completed the very first solo transatlantic balloon flight.
Kittinger established four Fédération Aéronautique Internationale (FAI) World Records for Distance, having travelled 5,703.03 kilometers (3,543.70 miles).¹ These records still stand.
This was not the first time Joe Kittinger had ascended in a balloon. The previous year he had set two FAI distance records, covering 3,221.23 kilometers (2,001.58 miles) from Las Vegas, Nevada to Farmersville, New York.² But he is best known for his historic high-altitude balloon flights. On 2 June 1957, Joe Kittinger rode the Project MAN-HIGH I balloon to an altitude of 97,760 feet (29,490 meters). One 16 August 1960, aboard Excelsior III, Kittinger reached 102,800 feet (31,333 meters). He then stepped out of the gondola and began the longest free-fall parachute descent attempted.
During the Vietnam War, Joe Kittinger flew 483 combat missions during three tours. He shot down one enemy MiG-21 fighter, and was later himself shot down. He was captured and held at the infamous Hanoi Hilton for 11 months.
¹ FAI Record File Numbers 1045, 1046, 1047 and 1048
18 September 1961: Jackie Cochran, acting as a test pilot and consultant for Northrop Corporation, set a Fédération Aéronautique Internationale (FAI) World Record for Distance when she flew the Northrop T-38A-30-NO Talon, 60-0551, from Palmdale, California, to Minneapolis, Minnesota, a distance of 2,401.780 kilometers (1,492.397 miles).¹
Jackie’s friend, famed Air Force test pilot Colonel Chuck Yeager, kept notes during the series of record attempts:
September 18: Jackie took off from Palmdale at 10:00 am for attempt to set records from points to points. I took off from Edwards with 275-gallon [1,041 liter] drop tanks. During climb Jackie reported rough engine and poor performance. Also the fuel flow was inoperative. Jackie returned to the field where I finally found her takeoff flaps were still down. Also her navigation lights and beacon were on. I was rather disappointed. She’s a little cocky in the airplane. She landed back there at Palmdale with 1500 pounds [680 kilograms] of fuel in each side and made a good heavy-weight landing. The aircraft refueled and another takeoff was made at 12:30 pm. Everything went smooth this flight. We ran into clouds at the edge of Utah which lasted until Cheyenne, Wyo. Clear the rest of the way. Jackie landed with 250 pounds of fuel in each side. Made a beautiful landing and turned off after a 4000 foot [1,220 meters] ground roll. Bob White returned the F-100 to Edwards.
— Brigadier General Charles Elwood (“Chuck”) Yeager, U.S. Air Force, quoted inJackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York, 1987, Pages 306.
The Northrop T-38A Talon is a two-place, twin-engine jet trainer capable of supersonic speed. It is 46 feet, 4 inches (14.122 meters) long with a wingspan of 25 feet, 3 inches (7.696 meters) and overall height of 12 feet, 10 inches (3.912 meters). The trainer’s empty weight is 7,200 pounds (3,266 kilograms) and the maximum takeoff weight is 12,093 pounds (5,485 kilograms).
The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. It is 108.1 inches (2.746 meters) long, 22.0 inches (0.559 meters) in diameter and weighs 584 pounds (265 kilograms).
It has a maximum speed of Mach 1.08 (822 miles per hour, 1,323 kilometers per hour) at Sea Level. The Talon’s service ceiling of 55,000 feet (16,764 meters) and it has a maximum range of 1,093 miles (1,759 kilometers).
In production from 1961 to 1972, Northrop has produced nearly 1,200 T-38s. As of January 2014, the U.S. Air Force had 546 T-38A Talons in the active inventory. It also remains in service with the U.S. Navy, and the National Aeronautics and Space Administration.
Jackie Cochran’s record-setting T-38 is in the collection of the Smithsonian Institution, National Air and Space Museum.