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 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 |
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 |
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. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
Drawing 5800 A - Turbo-pump Assembly 1 March 1944. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
Drawing Number: 5741 D3 showing B (fuel) pump centrifugal impeller mpe drawing dated April 1944. mpe original drawing (Digipeer.de image)
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Category | Turbo-pump |
Drawing 5742 B - Steam Tubine Assembly showing part/drawing numbers. (Digipeer.de image)
Album | V2 rocket turbo-pump |
Category | Turbo-pump |
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.
In this diagram the V2 Turbo-pump is shown in a cutaway presentation and rotated 90 degrees counter clockwise. The B stoff (fuel) pump is nearest the viewer - the over-speed device can be seen on the B stoff pump's case end-plate. The low pressure inlet ports our shown to the left, and high-pressure outlet ports are on the right. The steam distribution manifold can be seen at the furthest point from the viewer - the steam inlet pipe flange can also be seen. The feed pipe from the steam generator attaches to thus flange.
A Stoff (liquid oxygen) pump casing diagram showing stress points that require X ray quality control photography before use. The diagram shows the specific locations where photographic film is to be placed for X-ray analysis.
This mpe* drawing from 1945 shows the individual steam buckets or blades (labeled A and C) mounted to the rim of the rotor disk. As well as the fixed (i.e. stationary) stater blade B, positioned such that blades A & C can pass either side of it. The steam expansion is well shown by the increasing surface area of the blades from A to C, and growing larger, from left where the high pressure super heated steam enters the turbine, to right where it exits the blade pathway and passes in to the exhaust outlet. The lower graphic shows the way the super-heated high pressure steam is passed from the initial A blade and deflected by the reversed B stator blade for its energy to to be harvested for a second time by the C rotor blade. * mpe is the secret three letter armament code for Karlshagen, Werk Nord (North Works).
This HVP technical drawing from October 1940, shows a proposal from the Oddesse company - the full title of this company is KLEIN SCHANZLIN ODDESSE GmbH. Klein, Schanzlin & Becker A.G. (waffenamt code: ebb) took over Oddessa in 1929 and the company became formally known as KLEIN SCHANZLIN-ODDESSE GmbH (code ebc) in 1939. (NB: The company name has nothing to do with a similar sounding place name Odessa. The Oddesse trading name was formed from the partnership of English engineer Oddie, and German businessman Hesse.). The dual centrifugal turbo-pump shown in the drawing is a variant of a high pressure fire-fighting pump manufactured by Oddesse. Note the off-center outflow ports - not also that the outlet flanges are still level at this stage. Note also the incorrect spelling of the company name in the details panel lower right. (Digipeer.de image)
Signatur FA 014/21241 (Digipeer.de image)
Another HVP technical drawing from later in October 1940, shows further data from the KLEIN SCHANZLIN ODDESSE (ebc) company A4-V2 turbo-pump project. See previous image for company details. The dual centrifugal turbo-pump shown in the drawing is a variant of a high pressure fire-fighting pump manufactured by Oddesse. Note the off-center outlet ports. Note also the corrected spelling of the company name in the details panel lower right (see previous Oddesse image) and the small note below the top table that indicates that the pumps are from Oddesse (ODD) and the turbine from a company indicated as SSW. (Digipeer.de image)
V2 rocket turbo-pump preliminary dimension sheet for O series, drawing. Many of the final elements of the turbo-pump design can be seen in this 'preliminary' drawing and table form 1941. The word lieferfirma in the data box btm right mean supply company - and this is indicated to be KSB or Klein Schanzlin & Becker AG, Frankenthal. Signatur FA 014/14769
(Digipeer.de image)
Centrifugal impeller for A or liquid oxygen (LOX) pump. The drawing originated in Aug 1943 and was superseded in December 1944. A key to the image hatching can be seen with the label 'Hochbeansprucht' which in English means Highly Stressed. Next to the drawing numbers two secret three letter armament codes can be seen indicating the 'origination' of the document. The top one mpe = Heimat Artillerie Park 11 (HAP or Army Artillery Range). The lower code ebb = Klein Schanzlin & Becker AG, Frankenthal.
Signatur FA 014/02542 (Digipeer.de image)
Signatur FA 014/02537
Abmessungen: 42,9x59,8