Tag Archives: Jacqueline Marie-Thérèse Suzanne Douet

22 June 1962

Jacqueline Auriol climbs out of the cockpit of a Dassault Mirage IIIC. (Joyeux Magazine)

22 June 1962: At Istres, France, Société des Avions Marcel Dassault test pilot Jacqueline Marie-Thérèse Suzanne Douet Auriol flew a delta-winged Dassault Mirage III C interceptor to set a new Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 100 Kilometers. Her average speed over the course was 1,850.2 kilometers per hour (1,149.7 miles per hour).¹ Mme. Auriol broke the record set 6 October 1961 by Jacqueline Cochran with a Northrop T-38A Talon.²

Dassault Mirage III C. (Dassault Aviation)

The Dassault Mirage III C was the first production variant of the Mirage series. It was a single-place, single-engine tailless-delta-wing interceptor designed for Armée de l’air (the French air force), with variants for export. It was designed as a light-weight fighter capable of Mach 2 speeds.

The Mirage III C was 45 feet, 5 inches (13,843 meters) long with a wingspan of 27 feet, 0 inches (8.230 meters) and height of 14 feet, 9 inches (4.496 meters.) The fuselage had a horizontal ellipse cross section and incorporated the Area Rule, similar to the delta wing Convair F-102A. The Mirage IIIC had an empty weight of 12,350 pounds (5,602 kilograms) and maximum takeoff weight of  max gross 22,860 pounds (10,369 kilograms).

The interceptor’s low-mounted delta wings used trailing edge flight controls, with ailerons outboard, elevators at the center and small trim tabs inboard. The leading edges were swept aft to 60° 34′ and there was 2° 30′ anhedral. The total wing area was 366 square feet (34.00 square meters).

The Mirage III C 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).

When configured as a high-altitude interceptor, the Mirage could be equipped with a hypergolic liquid fueled Société d’Études pour la Propulsion par Réaction SEPR 841 rocket engine mounted under the rear fuselage. When the booster pack not used, a small additional fuel tank would be mounted in the same position.

The Dassault Mirage III C could climb to 30,000 feet (9,144 meters) in 3 minutes, 60,000 feet (18,288 meters) in 6 minutes, 10 seconds, and reach 72,000 feet (21,946 meters) in 9 minutes. It had an economical cruise speed of 0.9 Mach at 40,000 feet (12,192 meters), and maximum speed of Mach 2.3 at 36,000 feet (10,973 meters). The maximum range with external fuel tanks was 1,850 miles (2977 kilometers).

The interceptor was equipped with search radar and a missile targeting computer. Armament consisted of a modular gun pack with two Direction des Études et Fabrications d’Armement (DEFA) 5-52 autocannon with 125 rounds of ammunition per gun (the targeting computer had to be removed for this installation). A Nord AA.20 guided air-to-air missile could be carried under the fuselage on a centerline hardpoint, or a AS.30 air-to-ground missile. Both of these were controlled by the pilot through a cockpit joystick. Alternatively, two Sidewinder infrared-homing air to air missiles were carried on underwing pylons.

95 Mirage III Cs were built. The served with the Armée de l’air from 1961 to 1988.

Dassault Mirage III C No. 92. (Dassault Aviation)

¹ FAI Record File Number 12391.

² FAI Record File Number 13036: 1,262.19 km/h (784.29 miles per hour)

© 2018, Bryan R. Swopes

14 June 1963

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)

¹ FAI Record File Number 12392

² FAI Record File Number 12390

© 2019, Bryan R. Swopes

31 May 1955

Jacqueline Auriol devant le Mystère IV, en juillet 1955. L'avion a servi de modèle au collier vendu aux enchères mardi 13 mai 2014 à Genève. [AP Photo/Str - Keystone]
Jacqueline Auriol devant le Mystère IV, en juillet 1955. L’avion a servi de modèle au collier vendu aux enchères mardi 13 mai 2014 à Genève. [AP Photo/Str – Keystone]
31 May 1955: Test Pilot Jacqueline Marie-Thérèse Suzanne Douet Auriol flew the Dassault MD.454 Mystère IV N to a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15/25 Kilometer Straight Course at Brétigny-sur-Orge, France.¹ Her average speed of 1,151 kilometers per hour (715 miles per hour)—0.94 Mach—broke the previous record which had been set two years earlier by her friend, Jacqueline Cochran.

Jacqueline Auriol was awarded the Harmon International Trophy for 1955, the third of four that she would receive.

Dassault Mystere IV N 01
Dassault MD.454 Mystère IV N 01. (Weygand Collection via FrenchWings.net) 

The Société des Avions Marcel Dassault MD.454 Mystère IV N 01 was the first of two prototype two-place, single-engine, swept-wing interceptors. 01 was first flown 19 July 1954 by test pilot Gérrard Muselli. It had a large air-search radar mounted over the intake and was armed with 52 rockets carried in a retractable tray in the belly, very similar to the North American Aviation F-86D Sabre. The fuselage had been lengthened over the single-seat Mystère IV to provide space for the second cockpit.

The Mystère IV N was 49 feet, 11 inches (15.215 meters) long with a wingspan of 37 feet, 6 inches (11.430 meters) and overall height of 15 feet, 1 inch (4.597 meters). Its empty weight was 15,741 pounds (7,140 kilograms) and maximum takeoff weight was 22,572 pounds (10,238 kilograms).

Dassault Mystère IV N 01 F-ZXRM, right side profile. (© Collection Pyperpote)
Dassault Mystère IV N 01 F-ZXRM, right side profile. (© Collection Pyperpote)

The Mystère IV N was powered by a Rolls-Royce Avon RA.7R axial flow, afterburning turbojet engine. It used a 12-stage compressor, 8 combustion chambers and 2-stage turbine. It produced 9,500 pounds of thrust (42.258 kilonewtons) at 7,800 r.p.m., with afterburner. The engine was 42.2 inches (1.072 meters) in diameter, 276 inches (7.010 meters) long and weighed 2,960 pounds (1,343 kilograms).

Jacqueline Auriol’s record-setting Dassault Mystère IV N 01 F-ZXRM is on display at the Conservatoire l’Air et l’Espace d’Acquitane, Bordeaux Merignac Airport, France.

Mystère IV N aux cent ans de l'aviation de Mérignac (PA/Wikipedia)
Dassault Mystère IV N 01 on display at the Conservatoire l’Air et l’Espace d’Acquitane, Bordeaux Merignac Airport, France. (PA/Wikipedia)

¹ FAI Record File Number 9074

© 2019, Bryan R. Swopes