Jacqueline Auriol, 1956. (Association Amicale des Essais en Vol/CEV Brétigny)
14 June 1963: Jacqueline Marie-Thérèse Suzanne Douet Auriol flew an Avions Marcel Dassault Mirage III R (nº 307) over a 100 kilometer course near Istres, France, at an average of 2,038.70 kilometers per hour (1,266.79 miles per hour), setting a Fédération Aéronautique Internationale (FAI) world speed record.¹
Mme. Auriol broke the record set six weeks earlier by Jackie Cochran in a Lockheed TF-104G Starfighter. ²
Jacqueline Auriol (1917-2000), aviatrice française. Remise du Record international féminin (14 juin 1963) par Jacques Allez, directeur de l’Aéroclub de France. Paris, janvier 1964.
The Mirage III R is a single seat, single-engine, supersonic all-weather reconnaissance variant of the Mirage IIIE delta-winged fighter. The nose is modified to carry five cameras. Radar and weapons were deleted.
The Avions Marcel Dassault Mirage IIIE was 15,04 meters (49 feet, 4⅛ inches) long with a wingspan of 8,22 meters (26 feet, 11⅔ inches) and height of 4,45 meters (14 feet, 7⅕ inches). The interceptor’s empty weight was 7,050 kilograms (15,543 pounds), and maximum takeoff weight was 13,700 kilograms (30,203 pounds).
Dassault Mirage IIIE three-view illustration with dimensions. (Avions Marcel Dassault)
The aircraft flown by Jacqueline Auriol was powered by a Société nationale d’études et de construction de moteurs d’aviation (SNECMA) Atar 09C single shaft, axial-flow turbo-réacteur (turbojet engine) with afterburner. The engine used a 9-stage compressor section and 2-stage turbine. It was rated at 9,430 pounds of thrust (41.947 kilonewtons), and 13,669 pounds (60.803 kilonewtons) with afterburner. The Atar 09C was 5.900 meters (19 feet, 4.28 inches) long, 1.000 meters (3 feet, 3.37 inches) in diameter and weighed 1,456 kilograms (3,210 pounds).
The Dassault Mirage IIIE had a maximum speed of 2,350 kilometers per hour (1,460 miles per hour). Its service ceiling was 17,000 meters (55,774 feet), and its combat range was range 1,200 kilometers (746 miles).
Jacqueline Auriol flew this Dassault Mirage III R, nº 307, to an FAI world speed record of 2,038.70 km/h, 14 June 1963. (Archives Musée BA 102 – Collection particulière)
Amelia Earhart, Fred Noonan and a group of locals pose for photographs with the Electra at Assab, Eritrea, 14 June 1937. (Purdue University Libraries, Archives and Special Collections)
14 June 1937: Leg 17. From Massawa, Amelia Earhart and Fred Noonan fly their Lockheed Electra 10E, NR16020, 246 nautical miles (283 statute miles/455 kilometers) down the coast of the Red Sea to Assab, Eritrea, to prepare for the next long flight to Karachi, India. They have the aircraft serviced and fueled then await the morning.
On Tuesday, June 14, we moved down the Red Sea from Masawa to Assab to prepare for the long flight along the Arabian coast to India. Assab was nearer our objective than Masawa, offered better take-off facilities, and as well we had a greater supply of 87 Octane gasoline spotted there. Eritrea stretches along the coast of the Red Sea for 670 miles. Our course took us about half that length. Soon we left behind the mountains that bordered the coast-line and bade farewell to everything that was green. Approaching Assab the coast became terribly barren beyond description. . . .
—Amelia Earhart
Amelia Earhart’s Lockheed Electra 10E, NR16020, being serviced inside a hangar at Assab, Eritrea, 14 June 1937 (Purdue University Libraries, Archives and Special Collections)Great Circle route from Massawa to Assab, Eritrea, 246 Nautical miles (283 statute miles/455 kilometers). (Great Circle Mapper)
Adjutant Jean Pie Hyacinthe Paul Jérôme Casale, Aéronautique Militaire, circa 1917
14 June 1919: Sous Lieutenant Jean Pie Hyacinthe Paul Jérôme Casale took off from Issy-les-Moulineaux, France, to set a Fédération Aéronautique Internationale (FAI) World Record for Altitude. Flying a Nieuport-Delage chasseur (an aircraft type we now know as a fighter), he reached an altitude of 9,520 meters (31,234 feet). ¹ At that altitude, he was subjected to air temperatures of -50 °C. (-58 °F.). Casale landed at Villacoublay after a flight of approximately two hours.
Nieuport-Delâge Ni-D 29 C.1, s/n 12002, right front quarter view.
Casale’s chasseur was a Nieuport-Delâge Ni-D 29 C.1, a single-place, single-engine, two-bay biplane. The airplane was 6,50 meters (21.3255 feet) long with a wing span of 9,70 meters (31.8241 feet). The total wing area was 26,85 square meters (289.01099 square feet). The fighter had an empty weight of 740 kilograms (1,631.4 pounds) and gross weight of 1,100 kilograms (2425.085 pounds).
The airplane was powered by a water-cooled, turbosupercharged, 18.473 liter (1,127.29-cubic-inch displacement) right-hand tractor Hispano-Suiza 8Fb single overhead cam (SOHC) 90° V-8 engine. The engine was modified with the installation of a Rateau turbosupercharger to increase its output to more than 300 chaval vapeur. This was a direct-drive engine, and turned a two-bladed-fixed pitch propeller. The engine was 1.32 meters (4 feet, 4 inches) long, 0.89 meters (2 feet, 11 inches) wide, and 0.88 meters (2 feet, 10½ inches) high. It weighed 256 kilograms (564 pounds).
Engine cooling was provided by Lamblin cylindrical radiators mounted under the lower wing.
Nieuport-Delâge Ni-D 29 C.1, s/n 12002, right profile.
The standard airplane had a top speed of 230 kilometers per hour ( miles per hour), a range of 580 kilometers (360 miles) and a service ceiling of 8,500 meters (27,887 feet).
Nieuport-Delâge Ni-D 29 C.1, s/n 12002, right rear three-quarter view.
FLIGHT reported:
Pushing up World’s Height Record
Not satisfied with his height record of last week Lieut. Casole [sic] on June 14 took his Nieuport up to 10,100 metres (33,330 feet) during a flight from Villacoublay which lasted 1 hr. 55 mins. As in his previous flights, he used a Nieuport, fitted with a 300 h.p. Hispano-Suiza motor. His previous highest was 9,500 metres (31,350 ft.) and not 51,350 ft., as a printer’s error made it appear in our last issue.
—FLIGHT & The AIRCRAFT ENGINEER, No. 547, Vol. XI, No. 25, 12 June 1919, Page 799, Column 1
Jean Pie Hyacinthe Paul Jérôme Casale was born 24 September 1893 at Olmeta-di-Tuta, Corsica. His mother died when he was 9 years old, and his father, also, when he was 15.
Casale attended Bastia high school. On 1 Oct 1913, he enlisted in French Army, assigned to 8th Regiment of Chasseurs à Cheval. He was wounded in combat, 19 Aug 1914. After recuperating, he volunteered for aviation, December 1914. On completion of flight training, on 20 April 1915, he was awarded military pilot certificate # 837.
Casale was then assigned to the 1st Aviation Group, 20 May, and was promoted to corporal 5 June 1915. He was again promoted to Sergeant, 21 August 1915. On 19 May 1916, Sergeant Casale was awarded the Médaille Militaire and promoted to Adjutant. He scored his fifth shootdown of an enemy aircraft on 10 December 1916. He was next promoted to Sous Lieutenant, 24 June 1917
During World War I, Sous Lieutenant Casale was credited with 13 victories in air combat. For his service, Casale was awarded the Croix de Guerre with 9 palms, and was appointed Chevalier de la légion d’honneur.
Sous Lieutenant Casale was killed 23 June 1923 when he crashed in the forest of Daméraucourt dans l’Oise.
Captain Richard H. Coan, USAF, at Mono Lake, California, 13 June 1962. (FAI)
13 June 1962: At Mono Lake, California, Captain Richard H. Coan, United States Air Force, set a Fédération Aéronautique Internationale (FAI) World Record for Distance Over a Closed Circuit Without Landing with a specially prepared Kaman HH-43B Huskie, serial number 60-0263. With cowlings, doors and unneeded internal equipment removed—including brake lines to the rear wheels—the helicopter had an empty weight of just 5,300 pounds (2,404 kilograms).
Near Mono Lake, California, Captain Richard H. Coan prepares to lift off aboard HH-43B-KA Huskie 60-0263, at dawn, 13 June 1962. (U.S. Air Force)
Flying along a 12-mile (19.3 kilometer) section of California Highway 167 (Pole Line Road) on the north shore of the lake, Captain Coan flew 27 laps in just over seven hours, until the Huskie ran out of fuel and settled to the pavement in a low-altitude autorotation. Without brakes and with the rear wheels locked, the helicopter rolled off the side of the roadway, but came to a stop before ending up in a ditch. The total distance flown was 1,055.16 kilometers (655.65 miles), a new Fédération Aéronautique Internationale (FAI) World Record for Distance Over a Closed Circuit Without Landing.¹
Kaman HH-43B Huskie 60-0263 parked at the edge of Pole Line Road after its record-setting flight near Mono Lake, California, 13 June 1962. (FAI)
This same helicopter, flown by Captain Walter C. McMeen, set an FAI World Record for Altitude with a 1000 kilogram Payload to an altitude of 8,037 meters (26,368 feet) over Luke Air Force Base, Arizona, 25 May 1961.² On 18 October 1961, again at Bloomfield, Lieutenant Colonel Francis M. Carney set a World Record for Altitude Without Payload when he flew 60-0263 to 10,010 meters (32,841 feet).³ The following week, on 24 October 1961, Colonel Carney set six more world records, flying the HH-43B to 3,000 meters (9,853 feet) in 2 minutes, 41.5 seconds;⁴ 6,000 meters (19,685 feet) in 6 minutes 49.3 seconds;⁵ and to 9,000 meters (29,528 feet) in 14 minutes, 31 seconds.⁶ The following summer, Captain Chester R. Radcliffe, Jr., set an FAI World Record for Distance Without Landing when he flew it from Hill Air Force Base, Utah, to Springfield, Minnesota, a distance of 1,429.80 kilometers (888.44 miles), 5 July 1962.⁷
The Kaman Aircraft Corporation Huskie was used by the U.S. Air Force, U.S. Navy and Marine Corps, primarily for short range rescue operations. It was operated by two pilots and two rescue crewmen.
A turboshaft engine drove a unique system of counter-rotating and intermeshing rotors to provide lift, thrust and directional control. The counter-rotation cancelled the torque effect so no anti-torque, or tail, rotor was necessary. This allowed all of the engine’s power to drive the main rotor system.
The fuselage of the H-43B was 25 feet, 2 inches (7.671 meters) long. Each rotor had a diameter of 47 feet, 0 inches (14.326 meters). It’s height was 15 feet, 6½ inches (4.737 meters). The helicopter’s empty weight was 4,470 pounds (2,028 kilograms) and its maximum gross weight was 8,800 pounds (3,992 kilograms).****
The H-43B was powered by one Lycoming T53-L-1B turboshaft engine, rated at 860 shaft horsepower at 21,510 r.p.m. The engine uses a 5-stage axial-flow, 1 stage centrifugal-flow, compressor with a single stage gas producer turbine and single-stage power turbine. A reverse-flow combustion section allows significant reduction in the the engine’s total length. The power turbine drives the output shaft through a 3.22:1 gear reduction. The T53-L-1 is 3 feet, 11.8 inches (1.214 meters) long and 1 foot, 11.0 inches (0.584 meters) in diameter. It weighs 460 pounds (209 kilograms).
The Huskie’s economical cruise speed was 98 miles per hour (158 kilometers per hour), and the maximum speed was 120 miles per hour (193 kilometers per hour). Its hover ceiling out of ground effect (HOGE) was 18,000 feet (5,486 meters), and in ground effect (HIGE) was 20,000 feet (6,096 meters) and it had a range of 235 miles (378 kilometers). Normal rotor speed in flight was 255–260 r.p.m., with a minimum 238 r.p.m. in autorotation.
Captain Coan was awarded the Distinguished Flying Cross for the record flight. Later as a major, he commanded Detachment 8, 38th Aerospace Rescue and Recovery Squadron, at Cam Ranh Bay Air Base during the Vietnam War. He retired from the Air Force at the rank of lieutenant colonel.
With the call sign Pedro, the HH-43 was a rescue helicopter that served in combat during the Vietnam War.
The record-setting Kaman HH-43B Huskie 60-0263 was last assigned to Detachment 3, 42nd Aerospace Rescue and Recovery Squadron, Kirtland Air Force Base, New Mexico. It is in the collection of the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. Its distance record still stands.
Kaman HH-43B-KA Huskie 60-0263 at the National Museum of the United States Air Force. (U.S. Air Force)
¹ FAI Record File Number 1258
² FAI Record File Number 13154
³ FAI Record File Number 1870
⁴ FAI Record File Numbers 13057 and 13135
⁵ FAI Record File Numbers 13056 and 13136
⁶ FAI Record File Number 13137
⁷ FAI Record File Number 13208
**** Maximum overload gross weight is 9,150 pounds (4,150 kilograms) at a load factor of 2.0
LNER’s Grove Road railway bridge after the V-1 attack, 13 June 1944. (The National Archives)LNER Class B-12/3 standard gauge 4-6-0 locomotive, 7488, pulls a passenger train across the rebuilt Grove Street railway bridge, 9:27 p.m., 14 June 1944. (Great Eastern Railway Society)
13 June 1944: At approximately 4:30 a.m., the first V-1 flying bomb struck London. The “buzz bomb” detonated on a London and North Eastern Railway bridge crossing over Grove Street, between Devonshire Street and Osborne Road in Bethnal Green. Six persons were killed by the explosion, and twenty-six others were injured.
Twelve homes were demolished and at least fifty others badly damaged.
The bridge was along an important railway route. It was heavily damaged and the LNER decided to replace it rather than undertake any repairs. The new bridge was in service by 7:45 p.m., that evening.
“Detail from a Bomb Census map. The Grove Road V1 bomb is the lower of the two shown here. Catalogue reference: HO 193/50, map sheet 56/20 SE (A).” (The National Archives)
A Mr. Dowe witnessed the attack from the Bethnal Green Town Hall. He said, “When warning went I saw my wife and family into the shelter and then stood at the entrance to watch events. I heard a plane in the distance, then gunfire and then the sound of the plane as if diving. There was an orange flash, followed by a terrific explosion. There were no sounds of bombs falling as in the blitz, only only that of the plane zooming.”
Three other “P.A.C.s” (Pilotless Aircraft) ¹ fell in Kent and Sussex with little effect.
A V-1 flying bomb is brought out of a protective bunker for launching. Foto: PK-Lysiak/Transocean-Europapress
The Fieseler Fi 103 (better known as the Vergeltungswaffe 1 (“retaliation weapon”), or simply, the V-1, was what would today be considered a cruise missile. It was designed and built by the Gerhard Fieseler Werke GmbH. Construction of the missiles was very simple and it was mass produced at a rate of about 8,000 per month.
The V-1 is an unmanned mid-wing monoplane, constructed of a welded steel fuselage with straight wings which were covered by sheet steel. A pulse jet engine was mounted above the fuselage. The “flying bomb” was 8.325 meters (27 feet, 3¾ inches) long with a wingspan of 5.370 meters (17 feet, 7½ inches). The wing used a symmetrical airfoil with no sweep, dihedral or twist. There are no ailerons. Steel barrage balloon cable cutters were installed in the wings’ leading edges. The aircraft had a total weight of 2,160 kilograms (4,762 pounds).
Powered by an Argus Motoren Werke GmbH As 014 pulse jet engine which produced a maximum thrust of 3,530 newtons (794 pounds of thrust) at 750 kilometers per hour (460 miles per hour) at Sea Level. The pulse jet engine had no moving parts and fired 45–50 times per second. It burned low-octane gasoline with compressed air.
The V-1 was controlled in flight through pneumatic servos connected to a gyroscopic automatic pilot built by Askania Werke AG. A magnetic compass in the nose could be set to direct the V-1 in a particular direction. Air driven vanes at the nose drove an air log, which kept track of the distance flown by means of a turn counter. At a preselected count, the device shut down the pulse jet engine and the flying bomb entered a steep dive and crashed into the ground and the warhead detonated. The V-1 was only accurate enough to land in a general geographic area.
The aircraft had a maximum speed of 600 kilometers per hour (373 miles per hour) at 2,500 meters (8,200 feet). The maximum range was 235 kilometers (146 miles).
The warhead contained 830 kilograms (1,830 pounds) of Amatol 3 gm (a mixture of the high explosive TNT with ammonium nitrate). The warhead could be detonated by any one of three fuses: an electrical impact fuse, a mechanical impact fuse, or a mechanical delayed action fuse.
The V-1 was usually launched from an inclined ramp by catapult, though it could also be air launched from a carrier airplane.
Between 13 June 1944 and 29 March 1945, approximately 10,500 V-1s were launched against England. In the area around London, 6,184 people were killed and 17,981 others seriously injured. The V-1 was also targeted against cities on the European continent, especially Antwerp. 8,696 V-1s were launched against that city, and 3,141 fired at Liège. These attacks killed 4,683 persons and wounded 10,075.
¹ “Flying bomb” replaced Pilotless Aircraft as the preferred term in a Cabinet meeting, 19 June 1944.
