TECHNICAL SPECIFICATIONS OF THE EF-132 TYPE HEAVY BOMBER

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP82-00457R010800090009-8
Release Decision: 
RIPPUB
Original Classification: 
S
Document Page Count: 
4
Document Creation Date: 
December 14, 2016
Document Release Date: 
January 18, 2002
Sequence Number: 
9
Case Number: 
Publication Date: 
February 28, 1952
Content Type: 
REPORT
File: 
AttachmentSize
PDF icon CIA-RDP82-00457R010800090009-8.pdf235.88 KB
Body: 
0 Approved Fg1~08t: CIA-RDP82-004578010800090009-8 i , ,6'klAAix) - U CLASSIFIG 1 a ' L,.? CENTRAL INTELLIGENCE AGENCY REPORT NO. INFORMATION REPOR' .,OU NTRY SUBJECT 25X1A PLACE :ACQUIRED 25X1 C DATE OF INFO. 25X1 X l,, USSR/Germany (Soviet Zone) Technical Specifications of the 9-132 Type Heavy Bomber OF ENCLS.. DO NOT CIRCULATE. ` REPORT NO .T TO In 1946 a heavy bomber having the type designation EF-132 and a mo 1f _;;ation of t his type which was to be used as a reconna:Lsance plans were de z .grad by the Special Constructions Bureau (SKTB) No,, 1 in Dessau? A mock-up r...el of the aircraft was made.* 2. Descriptive data: sw The aircraft was designed as a semi-high-wing monoplane with se;:;; back wings and tail assembly. In order to meet the range specificat.,-r?: demanded, the plane was fitted with six JUr110-012 engines mounted ... the wings. The wing thickness required in the jet engine area was :t. fl.ned by increasing the profile thickness from 16 to 20 percent. For ,,e-.eons of better stability and servicing, the jet engines were ultimratr>1y placed on rails, which made it possible to ovll them out of the b. The aircraft was designed with a tricycle landing 'ear$ the nose k.r3ei retracting into a recess under the pressurized cabin. The main 1i.ev'f:tin g gear, in tandem, was fitted inboard of the inside jet engine, " -.Al. arrangement of the landing gear was known from various large airer?:tt types designed at the Junkers Aircraft Plant. The ::ecquired tiro s res of 1.80 meters in diameter were, however, not available at that A second solution was therefore provided. This verzion was char.,-.c?.9ri.zed by the utilization of smaller wheels and an auxilliary landing mounted between the two main wheels which was jettisoned after t_1.=: off. The Junkers Plant acquired experience with multiple-wheel landing ears by the construction. of the Ju-390 type aircraft, c. The four-man crew** was housed in a spacious pressurized cabin nose. The shape of this cabin was similar to that of the Ju-2E" 3x;: Ju-86 aircraft. d. The plane was to be provided with three remote-controlled gun st L5-:}ns to be delivered by the Dorsig firm. Tv.o gun syations each with tr~x: 3C yam cannon: were located just behind the pressurized cabin. These ?,tuna. stations had a complete free area for firing except for dead spaces of the #::Al CLASSIFICART RJR .._ FBI ONTt~JL - US L DISTRIBUTION Approved For Release 2002/08/08: CIA-RD 25X1A 25X1A _.,......_._....,,25X1 A No ' ~ __ o ngb Class,] Class. Changcd To; TS S Mitta HR 70.2 W&QQ45714oWbWk009-8 CD NO. "DATE DISTR. 2' Feb' 1952 NO.. OF PAGES 28 Approved For Release 2002/08/08 : CIA-RDP82-00457RO10800090009-8 CE''TfAL I1Ia1IGErCE AGE'CY 25X1A assembly and the pressurized cabin, A remote-controlled. 20wmn four- barreled machine gun was mounted aft of the tail assembly, Weapons having effective range directly to the front were not provided* eo The mounting of the jot engines in the wings and the arrangement of the landing gear made it impossible to carry sizable amounts of fuel in the wings. The bulk of the fuel was therefore stored in special rubber containers* f4 Specifications: Payload: four tons of bombs and one ton armament. Wing span: apprbximately 40 meters, Length: approximately 30 meters king area: approximately 230 square maeterso Tail assembly areas approximately 38 percent of the wing area* s um take-off load: 90,000 kgo Tactical range: 8,000 to 10,,000 km. ;~aocixm speed: at sea level, approximately 800 km per hours at 4,000 meters, approximately 900 km per houro at 11,000 meters, approximately 750 1cm ner 1ouro Service co ling: anproximately 13,000 lad, Rated take-off ground run: 2,700 metom V&N- t C'OP:TRtOL-UG S o nd2o The report supplies information on design project --- 25X1 C 25X1A No, 132, which was being worked on at the Junkers Aircraft Plant shortly before the and of the warp : Previously reported to be a five.man crew, Attar s: 'Lo ke a es of the EF-132 type bomber 2a Graphic representation of the ma:iimum 'speeds of the EF-132 at various altitudes? /coYTRoL..U.5 25X1A Approved For Release 2002/08/08 : CIA-RDP82-00457RO10800090009-8 jr._ 25X1 A l Coz~~~cT,~.uvs4 25X1A Awed For Release 2002/08/ - - 09-8 C&TRAL INTELLIG&CE AGENCY 77F::, T, r, ~~. `~ IdO1,1m 0L u, 25X1A Approved For Release 2002/08/08 : CIA-RDP82-00457RO10800090009-8 rrNF1DENT AL CE!TTRAI II'Tz I.1G '-CE AC,::,MCYP Approved For Release 2002/08/08 : CIA-RDP82-00457R01080063bbb~ ~ hic re; enta. 1,R Y of xzmam of the :P-r-1 3,,' - tit Various A1.titu den CONFIDENTIAL SECR-T/CONTROL-U.So 2 X1A 25X1A Approved For Release 2002/08/08 : CIA-RDP82-00457R010800090009-8