Search results
Results From The WOW.Com Content Network
The BMW 003 began development as a project of the Brandenburgische Motorenwerke (Brandenburg Motor Works, known as "Bramo"), under the direction of Hermann Östrich and assigned the RLM designation 109-003 (using the RLM's "109-" prefix, common to all jet and rocket engine projects). Bramo was also developing another turbojet, the 109-002.
Download as PDF; Printable version; In other projects Appearance. move to sidebar hide. From Wikipedia, the free encyclopedia. Redirect page. Redirect to: BMW 003;
The HeS 30 (HeS - Heinkel Strahltriebwerke) was an early jet engine, originally designed by Adolf Müller at Junkers, but eventually built and tested at Heinkel.It was possibly the best of the "Class I" engines, a class that included the more famous BMW 003 and Junkers Jumo 004.
The BMW GT 101 was a turboshaft-type gas turbine engine developed from the BMW 003 aviation engine, that was considered for installation in Nazi Germany's Panther tank.The German Army's development division, the Heereswaffenamt (Army Ordnance Board), studied a number of gas turbine engines for use in tanks starting in mid-1944.
The 109-718 (109 prefix number for the Reichsluftfahrtministerium, or RLM, designation used for all reaction-propulsion [rocket and gas turbine] aviation engine projects) was designed as an assist rocket for aircraft, for rapid takeoffs or to enable them to achieve high-speed sprints, akin to what Americans called "mixed power" postwar.
Download QR code; Print/export Download as PDF; Printable version; In other projects Wikidata item; Appearance. ... BMW 003; BMW 018; Bristol Phoebus; D. Daimler-Benz ...
He was given the development plans of the BMW 003, Jumo 004 and Heinkel HeS 011 engines. Late in 1942 the Project Office, led by Ludwig Mittelhuber, began to work on a series of fighter projects, to be powered by one of these new turbojet units. The first proposed design featured a BMW P.330 2 or Jumo 004 engine, positioned on the fuselage back ...
Data from Masters (1982). General characteristics Length: 11.7 m (38 ft 5 in) Wingspan: 15.0 m (49 ft 3 in) Gross weight: 9,000 kg (19,842 lb) Powerplant: 2 × BMW 003 turbojet, 7.8 kN (1,800 lbf) thrust (800 kg) each References Notes ^ Cowin (1963) ^ Masters (1982) Bibliography Hugh Cowin; "Blohm und Voss Projects of World War II", Air Pictorial, October 1963, pp. 312–316. David Masters ...