Unreliable Jumo jet engines would have been a problem if most destroyed Me262s actually survived that long. Apparently, they were kaput in combat by about 7 sorties. Figure 1 hr/sortie and the engines good for 20 hrs or 20 sorties.
View: https://youtu.be/prSwmH3Rjas?si=sS3XdZCmaAo68kyT
In summer 1943, Lyulka started the design of the S-18/VRD-3 eight-stage axial-flow turbojet, with 2.10 m length and 0.75 m of diameter.
The new engine was bench tested in August 1945 giving 1,268 kg static thrust, but their mass production was dismissed because steel turbine blades were not heat-resisting enough for use in operational airplanes, due to technological backwardness of Soviet metallurgy alloys.
In April-May 1945, twelve BMW 003 A turbojets were taken by Soviet troops at Breslau-Lower Silesian, one in Vienna-Hinterbruehl, blueprints and several engines at Basdorf-Zühlsdorf and eleven semi-destroyed turbojets at Heidfield.
Two Heinkel He 162 A-2 jet fighters, powered by BMW 003 A-1 engines, six HeS 8a and nine Jumo 004 B turbojets were captured at Heinkel-Vienna facilities.
Two BMW 003 E engines, along with a complete set of drawings, at Heinkel-Rostock factory.
One Arado Ar 234 C-3 bomber, powered by four BMW 003 A-1 engines, was seized in Damgarten, and their blueprints were found buried in the ground at the Arado-Brandenburg firm.
Several Jumo 004 B turbojets were captured at Brandis-Leipzig and ten at CKD-Prague works.
At Muldenstein Werke AG, Ascherleben FZA, Junkers-Ebersbach, Koethen MZK-Merseburg and Lindenthal-Leipzig underground facilities the Soviets captured enormous stocks of Jumo 004 B components and the technology for manufacturing and testing turbojets.
When some samples of Jumo 004, BMW 003 and HeS 8a engines were bench tested, in August 1945, by the TsIAM scientists, it was discovered that the construction of German turbojets required enormous technical and manufacturing resources that were not available in the USSR.
The high temperatures and high rotation speeds reached by the turbine blades required the use of austenitic steel alloys to withstand stresses caused by centrifugal forces.
The precision machining of these heat-resisting parts could only made possible by sophisticated machine tooling and highly skilled labor force.
Jumo 004 B-1 turbine blades were made of the 580ºC heat-resisting steel alloy Krupp-Essen
Tinidur (C, Si, Mn, Ti, Ni, Cr, Fe).
The air compressor casing was made of
Electron Magnesium alloy and the turbine discs were built in forged Molibdenum steel.
Other parts of the engine were made of aluminized anti-corrosion mild steel. To obtain this material the Germans had developed the manufacturing process called
Aluminitieren.
It was also necessary to develop a new procedure for welding the solid turbine blades, the WMF atomic hydrogen welding process.
To increase the life of the turbine Junkers, they tried making air-cooled hollow blades, but the
Tinidur sheet proved unsuitable for welding.
A new manufacturing process was developed by William Prym-Stolberg using
Degussa Flussmetal (85% Ag, 15% Mn),
Silma solder and Lithium fluoride at 1,000 ºC.
In August 1944 production of hollow blades started at Prym-Zweiffall factory and the whole project was classified secret.
The main Junkers plant at Dessau was heavily bombed in late 1943 and the Jumo 004 B-2 production was taken over by Köthen and Muldenstein satellite factories in August 1944.
When the Nickel became extremely scarce in the Reich, after their supply lines of Finnish ore were cut off, Krupp-Essen developed the heat-resisting alloy known as
Cromadur (Mn, Cr, V, Si, C, Fe). It was easy to weld, and it was used for the manufacture of the Jumo 004 B-4 air-cooled hollow blades.
Jumo 004 was developed from the beginning to run on diesel oil, but the BMW 003 availability suffered delays when converted to diesel and the BMW-Bramo’s Spandau plant was bombed in 1943.
By August 1944 it was finally ready for mass production, under SS control, in underground dispersed sites of SS-Kraftfahrttechnischen Versuchsanstalt-Oranienburg, Eisenach, Zühlsdorf, Nordhausen, Wittringen and Stassfurt.
The BMW 003 air compressor forged blades were of Normen Nº 3510 Magnesium alloy and the compressor discs of Normen Nº 3115 Duralumin.
The turbine blades were made of
Sicromal 10 heat-resisting steel (Cr, Al, Si, C, Fe), FBD Chrome-Nickel steel (Cr, Ni, Mo, Ta-Nb, Si, C, Fe) and FCMD steel (Cr, Mn, Mo, Nb, Si, V, C, Fe).
The turbine discs were made of steel alloy (Mn, Cr, Mo, Si, C, Fe) and the cooling insert of the blades of WMF
Remanit 1880S Chrome-Nickel steel.
Other parts of the engine had undergone an anti-corrosion treatment, based on Aluminum lacquer paint, developed by Zarges-Weilheim.