![V2 turbo propellant pump B](https://v2rockethistory.com/wp-content/grand-media/image/Drawing_5741_B1_-_fuel_B_pump_Spiralhousing.jpg)
Drawing 5741 B1 mpe - Fuel (B) Pump Spiral-housing with dimensions. Drawing origin 18 July 1944, revised to new drawing (AM41780) 11 Jan 1945. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![Drawing 5741 B - Fuel (B) Pump Assembly - Part Numbers](https://v2rockethistory.com/wp-content/grand-media/image/Drawing_5741_B_-_fuel_B_pump_assembly_-_part_numbers.jpg)
Drawing 5741 B mpe - Fuel (B) pump assembly showing part/drawing numbers. Drawing originates 20 July 1944 and revised with new number (AM41780) 16 Jan 1945. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![V2-Turbine: steam-distributor-revision](https://v2rockethistory.com/wp-content/grand-media/image/V2-Turbine-steam-distributor-revision.gif)
Animation highlighting just one of many revisions to the turbo-pump that occurred at an accelerating rate between August 1943 and late 1944 as the missile moved from development to full production, and finally use in combat. (Digipeer.de images: animation RJD)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![Turbopump (cut-away) - Figure 12](https://v2rockethistory.com/wp-content/grand-media/image/Turbopump_cut-away_-_Figure_12.jpg)
Drawing 8526 E mpe 1944: Turbo-pump training presentation image showing cutaway. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![Drawing 6380 A - Turbo-pump Assembly 08 Aug 1944](https://v2rockethistory.com/wp-content/grand-media/image/Drawing_6380_A_-_Turbopump_assembly_08_Aug_1944.jpg)
Drawing 6380 A - Turbo-pump Assembly 08 Aug 1944. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![Drawing 5800 A - Turbo-pump Assembly 1 March 1944](https://v2rockethistory.com/wp-content/grand-media/image/Drawing_5800_A_-_Turbopump_assembly_1_March_1944.jpg)
Drawing 5800 A - Turbo-pump Assembly 1 March 1944. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![Drawing 5742 B - Steam Tubine Assembly Part Numbers](https://v2rockethistory.com/wp-content/grand-media/image/Drawing_5742_B_-_Steam_tubine_assembly_part_numbers.jpg)
Drawing 5742 B - Steam Tubine Assembly showing part/drawing numbers. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![Turbo-pump drawing: 5741 D3](https://v2rockethistory.com/wp-content/grand-media/image/Drawing_5741_D3.jpg)
Drawing Number: 5741 D3 showing B (fuel) pump centrifugal impeller mpe drawing dated April 1944. mpe original drawing (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
![V2 rakete drawing number 3207C fuel valve](https://v2rockethistory.com/wp-content/grand-media/image/Drawing_of_main_fuel_valve_3207C.jpg)
Original mpe 1944 drawing number 3207 C of main fuel valave. (mpe = Heimat-Artillerie-Park Karlshagen, Werk Nord Peenemünde).
Album | Valves |
Category | Propellant flow |
![Ofen (R-Behälter) mit 1000 kg Schubleistung](https://v2rockethistory.com/wp-content/grand-media/image/1000kg_4B_ofen_reversed_larger.jpg)
The injector head section of the 4B 1000kg thrust rocket engine is a precursor to the injector pot or 'pre-chamber' design used later for each of the 18-pots of the 25-ton V2 rocket engine. Most of the essential ingredients are shown in this drawing from 1940. Drawing no 1848E Deutsches Museum München online archive ref FA 014/12829
![A4/V2 rocket Düse or nozzle drawing from 1944](https://v2rockethistory.com/wp-content/grand-media/image/V2_rocket_fuel_injector_insert_3304D_1944.jpg)
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
![HVP Drawing of diffuser system 1939](https://v2rockethistory.com/wp-content/grand-media/image/HVP_drawing_of_diffuser_system_1939.jpg)
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.
![A4/V2 rocket Düse or nozzle drawing from 1939](https://v2rockethistory.com/wp-content/grand-media/image/Fuel_nozzle_insert_113E_1939.jpg)
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
![V2 rocket steam turbine driven fuel and LOX pumps](https://v2rockethistory.com/wp-content/grand-media/image/section_Turbo_Pump_1942.jpg)
Sectioned general assembly view of the V2 turbo-pump (TP) dated September 1942. This image has been edited to show TP and document data closer together than the original.
![Fuel injector specifications](https://v2rockethistory.com/wp-content/grand-media/image/4554_18pot_combustion_sys_10-1943_blue.jpg)
Specification for fuel injector inserts showing orifice size, type, and A to E echelon position. Peenemünde document dated 30th October 1943. Of note on this document is the combination of high and low volume injector inserts (3304D and 3305D) in the echelon E position of the 12 cups comprising outer ring I. It shows that each cup or pot on this outer ring had 16 inserts at the lowermost position E with 12 of the inserts with three inlet apertures (3305D) and 6 with only two inlet apertures (3304D being lower flow volume) positioned in the segment covering 165 degrees and closest to the outside edge of the head. HAP11 (Heimat-Artillerie-Park 11, AKA armament code: mpe), drawing number 4554D, Deutsches Museum München