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V2 fuel injector Insert test rig

V2 fuel injector Insert test rig

Single nozzle insert test rig used by V2 Rocket History to test spray shape and volume at supply pressures consistent with fuel pressures specified for the injector head of summer 1944. The test system features an adjustable pressure regulator and fluid pressure gauge. For test purposes the device was simply connected to a relatively high pressure mains water supply. And although water does not have the same viscosity of the 75% Ethenol to 25% water mix of the V2’s fuel it was considered close enough by the German technicians, who regularly used plain water as a substitute when testing issues related to furl flow rather than combustion. A 2131E fuel injector insert is shown installed in the holder at the front of the rig, but as the thread was the same on all inserts the nozzle can be changed for other models easily with aid of a pin spanner. See video for a demonstration of this simple test system.

Album: V2 rocket fuel injector inserts

Categories: Combustion Propellant flow

Tags: #Combustion and injection #Propellent injector system

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Part of the ‘Standard’ series A aluminium head from 1941/42

Part of the 'Standard' series A aluminium head from 1941/42

Part of the ‘Standard’ series A aluminium head from 1941 to early 1942. Showing the position of standard type LOX injector. The brass fuel injector inserts type and position pattern on the relic seem to be of the standard type with the row of 3 inlet aperture type inserts positioned furthest from the LOX injector. Photo courtesy Horst Beck Collection

Album: A4-V2 Injection head, combustion chamber, and nozzle

Categories: Combustion Propellant flow V2 Missile relics

Tags: #Combustion and injection #Propellent injector system #V2 Missile relics