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An 003A-2 subtype turbojet with a BMW 109-718 (RLM powerplant number 109-718) liquid-fuel rocket fixed permanently above the jet exhaust nozzle, running on a hypergolic combination of R-stoff (a.k.a. Tonka or TONKA-250, 50% triethylamine and 50% xylidine) for fuel and SV-Stoff (aka RFNA propellants: 94% HNO 3, 6% N 2 O 4) oxidizer, code-named ...
Using this system, the famous BMW engine used in the Focke-Wulf Fw 190 would be known as the 9-801 (Piston(9)-BMW(8)Number(01)). However, this system was not widely used, even within the RLM, and a common name consisting of the manufacturer's name (often abbreviated) followed by the model number was much more common.
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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.
A single B-series airframe fitted with 2 x BMW 003 engines for engine development testing, and rumored to have been considered for new wing planform tests. Ar 234 V21 to V30 C-series development aircraft. V26 and V30 had experimental thick section wooden and thin section metal laminar flow wings. Ar 234 V16
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