HAP11 drawing of standard 3304D fuel injector screw insert. showing details of primary swirl cavity and orrifice and all additional apertures including the four small cooling pores. HAP11 (Heimat-Artillerie-Park 11, AKA armament code: mpe), drawing number 4554D, Deutsches Museum München
Album: V2 rocket fuel injector inserts
Categories: Combustion Propellant flow
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HVP drawing no 1203D showing burner cup ‘diffuser system’ disposition for 19-pot head (at this stage the 25 ton thrust injector head had nineteen so called ‘pre-chambers’ or pots as no central fuel valve was present). HVP drawing dated 1939.
Album: V2 rocket fuel injector inserts
Categories: Combustion Propellant flow
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Drawing from the Army Experimental Station Peenemünde dated 1939. The specification describes an insert template that could be used for a range of outlet and inlet orifice sizes. The German text beginning (eingedrehte …) translates as ‘Center-line of screw used for holes to be drilled later’, and the hole dimensions are not specified on this document. HVP drawing number 1113 E, Deutsches Museum München
Album: V2 rocket fuel injector inserts
Categories: Combustion Propellant flow
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Photo shows a small section of the burner cup with row A (2131E) fuel injector inserts with three row B drilled holes below. The two undamaged inserts carry the armament code ‘csl’. The relic was found near a workshop in the Development works Pennemünde. Slag from the cutting flame and damage to the inserts at both ends of the relic would indicate that the section was cut from a steel burner cup using a gas cutter (fuel and oxygen) for purposes unknown. V2RH collection image
Album: V2 rocket fuel injector inserts
Categories: Combustion Electrical connection V2 Missile relics
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Diagram showing cut-away presentations of the settled configuration of standard four ‘swirl’ inserts used in the V2 rocket engine’s 18-pot head from 1943 until the end of the war. The inserts are shown with their drawing code identification. All of the insert types used in the injector head are shown, however there were additional screw-in type fuel supply inserts, used to provide a fuel cooling balance function, located radially in the lower part of the combustion cavity.
Album: V2 rocket fuel injector inserts
Categories: Combustion Propellant flow
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Copyright: V2 Rocket History
