The SNECMA ATAR 101 is a French axial-flow turbojet engine built by SNECMA. It was derived from engines and design work carried out at BMW in Germany during World War II, and extensively developed though a progression of more powerful models. The name is derived from its original design group, Atelier Technique Aéronautique de Rickenbach employing Hermann Östrich and many of the wartime BMW gas turbine design group as well as other German engine design teams.[1] The ATAR 101 powered many of the French post-war jet aircraft, including the Vautour II, Étendard IV, Super Mystère B2, and the Mirage III-001, prototype of the Mirage III series.[2]
^ abcKay, Anthony L. (2007). Turbojet: History and Development 1930–1960: Volume 2: USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy, Czechoslovakia and Hungary. Marlborough, Wiltshire: Crowood Press. ISBN 978-1-86126-939-3.
The SnecmaAtar is a French axial-flow turbojet engine built by Snecma. It was derived from the German World War II BMW 018 design, and developed by ex-BMW...
The SNECMAATAR101 is a French axial-flow turbojet engine built by SNECMA. It was derived from engines and design work carried out at BMW in Germany during...
fuselage. It was tested with two SnecmaAtar101 turbojets each engine having a different system of afterburner. The Snecma Vulcain was also tested in a similar...
35° swept wing and a "flying" tail. Power was provided by a pair of SNECMAAtar101 turbojet engines, which were carried in pods located underneath the...
favour of a further-developed design, powered by the newly developed SnecmaAtar afterburning turbojet engine, designated as the Mirage III. In October...
turbojet, two completed. VG 91 Production version of the VG 90 with a SNECMAAtar101 turbojet, one built, but not completed. VG 92 Land-based version of...
where he worked for Snecma subsidiary Aeroplanes Voisin. Oestrich and his team worked on the further development of the Atar101. In 1948 he acquired...
(7,700 lbf) Thrust-to-weight ratio: 1.52 Related development BMW 003 SNECMAAtar Comparable engines Westinghouse J40 Related lists List of aircraft engines...
089 ft) / 900 km/h (559 mph; 486 kn) Related development BMW 018 BMW GT 101SnecmaAtar Comparable engines Junkers Jumo 004 Ishikawajima Ne-20 Heinkel HeS...
fuel to generate thrust for a second than did the Concorde's Rolls-Royce/Snecma Olympus 593 turbojet. However, since energy is force times distance and...
minimize the development risk by keeping the 24-kilonewton (5,400 lbf) SNECMAAtar 101C turbojet installation as simple as possible. He opted for a straight-through...
average maximum takeoff thrust of 9.83 kN (2,210 lbf). The Mirage III's SnecmaAtar G.2 propulsion engine was replaced with an un-reheated (non-afterburning)...
aircraft, and M.D.450-10, which was used as a flying testbed for the SNECMAAtar engine. According to Munson, around the time of the pre-production aircraft...
Wright J65 Comparable engines General Electric J73 Rolls-Royce Avon SNECMAAtar Tumansky R-13 Tumansky R-25 Related lists List of aircraft engines "armstrong...
Havilland Australia Rolls-Royce Avon built for the Sabre and GAF Canberra SnecmaAtar built for the Mirage Bristol Siddeley Viper built for the Macchi MB-326H...
powered by both turbojet and turboprop engines; among these was one for a SnecmaAtar-powered tri-jet to be developed in association with the SNCA du Nord...
Global Information