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.

SNECMA Atar 101 The Snecma Atar 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 engineers through a progression of more powerful models.

Les Snecma Atar sont une famille de turboréacteurs militaires produits par la firme française Snecma. L' Atar volant est le prototype qui permit de valider le système de stabilisation par déviation de jet du futur C450.

"Atar-101 with afterburner" -The range is completed with Atar-8 and Atar-9. From the 1950's, the production is fully done by Snecma, wherefore these engines are known under the name "Snecma-Atar9K" for example.

Sep 24, 2024 · 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.

Jul 23, 2024 · -The Atar 101 served as the basis for starting two new families of engines that have been very important: the Atar 08 and the Atar 09. Both group together refinements obtained from the experience of the 101 series.

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.

Development continued until production of the ATAR 101 engine commenced at SNECMA in May 1946, and the engine first ran on March 26, 1948. In 1954 SNECMA designed an engine to upgrade power output and this was designated ATAR 08 and the thrust was rated at 9,400lbs.

L’Atar 101 G fut l e premier réacteur français supersonique. Produit à 462 exemplaires pour équiper les 180 monoréacteurs Dassault Super Mystère B2, l’Atar 101 G s’est décliné en deux variantes de série : le modèle G-2 à démarrage électrique (monté sur les avions israéliens) et le modèle G-3 à démarrage pneumatique. 406 ...

The powerplant was a SNECMA ATAR 101D-1 turbojet which produced 6,610 pounds of thrust (29.403 kilonewtons). The maximum speed of the Mystère IIC was 660 miles per hour (1,062 kilometers per hour). Its range was 550 miles (885 kilometers) and the service ceiling was 50,000 feet (15,240 meters).