GERMAN ENGINEERS IN THE USSR

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP82-00457R008000890006-4
Release Decision: 
RIPPUB
Original Classification: 
S
Document Page Count: 
4
Document Creation Date: 
December 14, 2016
Document Release Date: 
December 28, 2000
Sequence Number: 
6
Case Number: 
Publication Date: 
November 2, 1951
Content Type: 
REPORT
File: 
AttachmentSize
PDF icon CIA-RDP82-00457R008000890006-4.pdf544.21 KB
Body: 
CONFIDENTIAL Approved For Release 2001/03/06: CIA-RDP82-OO457ROO8OOO89OOO(- E t; N ',/0a'g1 I US OFF.IOLLi, DULY 25X1A CILASSIF!C EON S.6C r p , ~I f4~ NA~'S A+.JLI.'AkJlJA. L).Idyl ~tA1 CEi~TRAE. I9VeLLIGENCE AGENCY REPORT NO. INFORMATION REPORT CD NO. COUNTRY USSR SUBJECT'' German Engineers in the USSR PLACE 25X1 C ACQUIRED M DATE OF 25X1 X INFO. 1 SOURCE 25X1 C DATE DiSTR.. 2 Nov 195L NO. OF PAGES NO. OF ENCLS. (LISTED BELOW) CULATE SUPPLEMENT TD 25X1A 25X1 X REPORT NO, _ 1. Activitie6 at Test Plant No. 2 in Upravl encheski (53021tH/500l2 VE) included the construction of the BWI-003' turbo jet power plant a This project was completed in early 1947, since the engine was ready at that time for mass production? According to Soviet statement,-., this type of engine was installed. in the first jet fighters employed in Korea. 2 The next project .corked on was the Jumo-012 turbojet engine. During the official acceptance test (state test) this engine produced a static thrust of 3,' or 3,300 kg with an air throughput of 60 kg/sec Q / The 100-hour state test was broken d un into individual tests, each of them including a run of 25 minutes with maximum trust performance, 20 minutes cruising porrier, five minutes take- off thrust, i.e., overload, and 10 minutes acceleration power. During these 10 minutes the engine was accelerated five times for a period of 13 to 18 seconds. Some time after these acceptance tests war held, test orders were received at Test Plant No. 2, which could have come only from a plant engaged in mass production of Jumo Olt power plants v The turboprop engine Jumo--022 with an air throaaghps t of 31 dig/sec was ready for teass production in September 19508 3/' The engine was subjected to a test run of 200 hours. The 14?atage axial-fio compressor of this engine was an enlarged copy of the Jumc-?001 compressor dl 25X1X 2. Between projects, - worked on the construction of a four-stage radial compressor which was to be used in experiments with. combustion chambers and with project P..1300 The P-130 was a combined piston-jet engines The pro- ject was given up as unfeasible. 3,, Kerosene with a calorific pcrixer of 10,400 kg/cal was used as fuel with all. turbojet and turboprop power plants o Transformer oil had to be used as a lubricant in order to overcome difficulties with the fuel. control devices , The .erose e received was very i,,.rapure 0 On 3 ar nh 1949 the-Soviets ordered the construction of the PS starter CL kSS{F ICKNON ShCa- :'T/OONTRt3LUS OFFICIALS MLY 9 tli;RY4'-:..,.._._.-3 NAVY Approved For Release 2001/03/06 : CIA-R P!2~O Approved For Release 2001/03/06: CIA-RDP82-00457R00800089 Si:C:t-t., T/C~-1gTiiOL.U3 0Fr:1C1.'liz 0NLL Ci TR. L 1I T"L,L,1.G -'!X ,'a : ei ii:ai "CY the hrs, but appears rather 1ov:, co;".pared to turboprop engines developed b the estorn rowers. It was reported that the s2Jecific fuel ron:;u, Dtion 1j , of ;400 graanrts/hp/h was to be reduced to 2d0 gr a ss/hp/h, :hich eorro iponds to the fuel consumption of tur ..ow~rop engines of the m,estern nvrers. There are data indicatin ; that the construction of the iumo-022 ..a.s also based on utesigns of the 3.-28 turboprop en:ine. The 1-130, a favorite project of the Novi :ts, had been started in Dessau before the deportation of the The air required for the pistons was to be drain from the third stage of the compressor with a r.a:d.-, si pros sure of 1.5 ati,ios hores, The fi:.a1 pr..,ssi.re to be roduced by the co. Nprecsor was to be 6 at.-.Loseheres. This co:?ined oiston-jet engine was designed for a thrust of 1,700 kr and a Aston engine output of 2000 hP. it is believed that t:..s ,-,roject ,.as cancelled. For diagram of the T turbo starter engine see ,nno.& 1. For cro`^s s_?ction of the starter engine see , nanex 2. For the insta lation of a TS, starter in the Juno 1~aaer i .l nts 012 and 022 see :::. Fey 3, The device offers the advantage of conserving, the battery. 1?'urtc;e'r_:".or~e, the >am. Lype of fuel. can be taken for t.e starter engine and the main cower Plant, The of :.,ateran..i,i and the t::c other ongineers are reported for the first ti : e. The transfer of Soviets from Kazan, Ito,?:ever, vas previ 3u: ].y ment:i >ned, uincc Christian and his group also ~n rkec::. in kazan before troy :rare; tr