The Heinkel HeS 30, also known by its official designation 109-006 or HeS 006, was an early axial-flow turbojet originally designed by Adolf Müller at Junkers and finally built and tested at Heinkel after Müller and part of his team moved to Rostock in 1939. It had a five-stage axial compressor, ten can-annular combustion chambers and a single-stage turbine with adjustable guide vanes. The first engine ran in May 1942, and by October it was running at full speed with about 860 kilograms-force of thrust at a dry weight of only 390 kilograms, a better thrust-to-weight ratio than either the BMW 003 or the Junkers Jumo 004. The air ministry still refused it a production contract and told Heinkel to turn to the larger HeS 011.
Facts
Displacement or Thrust Classification
Fuel or Cycle Connections
Exemplifies
Source Heinkel HeS 30 (Wikipedia)
Of Make
Source Heinkel HeS 30 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Heinkel HeS 30 (Wikipedia)Lead, makerQuote, Lead, maker
but eventually built and tested at Heinkel
Sources
1. Heinkel HeS 30 (Wikipedia)
Argument and resignation, first run
it was not until May 1942 the first engine actually ran
Specifications, fuel type
Fuel type: Petrol
Specifications, thrust
Maximum thrust: 8.4 kN (1,900 lbf) at 9100 rpm
Lead, maker
but eventually built and tested at Heinkel
Of Make: Heinkel, Lead
but eventually built and tested at Heinkel
In Group: Turbojet and Turbofan Engines, Lead, engine type
was an early jet engine, originally designed by Adolf
Exemplifies: Aviation, Lead, aircraft engine
was an early jet engine, originally designed by Adolf
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