{"product_id":"veb-baade-152-aircraft-manuals-collection","title":"VEB Baade 152 Aircraft Manuals Collection - Digital Download","description":"\u003ch3\u003eVEB Baade 152 Aircraft Manuals Collection\u003c\/h3\u003e\n\u003cp\u003eThis is a curated archival collection of technical manuals, specification documents, and manufacturer brochures covering the VEB Baade 152 — East Germany's first and only indigenous jet-powered airliner, developed by VEB Flugzeugwerke Dresden in the late 1950s. The collection spans both the 152\/I and 152\/II standards, providing researchers, aviation historians, and enthusiasts with a rare window into one of the Cold War era's most ambitious — and ultimately tragic — aviation programmes.\u003c\/p\u003e\n\u003cp\u003e\u003cstrong\u003eDefinitive Collection with Free Lifetime Updates:\u003c\/strong\u003e This is a living collection that we continuously expand and refine. As we acquire additional VEB Baade 152 documentation, technical bulletins, or variant-specific materials, we update this collection and provide free lifetime updates to all purchasers. Your one-time purchase guarantees access to all future additions and improvements to this collection.\u003c\/p\u003e\n\u003ch2\u003eHistorical Note\u003c\/h2\u003e\n\u003cp\u003eThe Baade 152 emerged from the post-war reorganisation of German aviation expertise under Soviet oversight. Its lineage traces directly to the Junkers OKB-1 150 bomber project, developed by German engineers working in the USSR after 1945. When those engineers returned to East Germany in the early 1950s, they brought with them swept-wing jet design experience that would form the foundation of the 152 programme.\u003c\/p\u003e\n\u003cp\u003eLed by Brunolf Baade — a former Junkers engineer — the project aimed to produce a modern short-to-medium range jet airliner capable of serving Interflug, the East German state airline. The aircraft featured high-mounted swept wings using aerodynamic profiles TsAGI S-10s-9 at the root and SR-3-12 at the tip, and was powered by four Pirna 014 A-0 turbojets.\u003c\/p\u003e\n\u003cp\u003eThe first prototype, the 152\/I-V1, flew on 4 December 1958 — a historic milestone for East German aviation. However, the maiden flight revealed serious handling deficiencies, including severe right-hand drift attributed to non-uniform thrust from the engines, requiring significant corrective input from test pilot Willi Lehmann. The 152\/I used a tandem centreline (bicycle) undercarriage with wingtip outriggers — a configuration deemed unsuitable for commercial operations and subsequently redesigned for the 152\/II, which adopted a conventional tricycle undercarriage with main legs retracting into the engine nacelles.\u003c\/p\u003e\n\u003cp\u003eOn 4 March 1959, prototype DM-ZYA crashed fatally during a test flight. Investigations — not made public until 1990 — revealed that the Pirna 014 engines experienced fuel starvation when the aircraft was flown at a nose-down angle of 16 degrees or greater, a critical design flaw compounded by probable pilot error. The crash effectively ended the programme's momentum. Further development continued briefly with the 152\/II standard, but the project was cancelled in 1961 under Soviet pressure to purchase Tupolev Tu-104 airliners instead.\u003c\/p\u003e\n\u003cp\u003eThe sole surviving airframe — Baade 152\/II-011 — was rescued from a barn and is now preserved at the Verkehrsmuseum Dresden \/ Dresden Airport. Much of the original engineering documentation was lost or destroyed following cancellation, making the surviving manuals and brochures in this collection particularly significant.\u003c\/p\u003e\n\u003ch2\u003eManuals Included in This Collection\u003c\/h2\u003e\n\u003cp\u003e\u003cstrong\u003eVariant I — 4 Documents\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eBaade 152 I Aircraft Handbook\u003c\/strong\u003e\n\u003cul\u003e\n\u003cli\u003eVEB Baade 152 I Aircraft Specification Manual Volume 1 — Kurz_Bedienanlietung-1958-V1 (German Language)\u003c\/li\u003e\n\u003cli\u003eVEB Baade 152 I Aircraft Specification Manual Volume 2 — Kurz_Bedienanlietung-1958-V2 (German Language)\u003c\/li\u003e\n\u003cli\u003eVEB Baade 152 I Aircraft Specification Manual Volume 3 — Kurz_Bedienanlietung-1958-V3 (German Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBaade 152 I Slides, Photos and Brochures\u003c\/strong\u003e\n\u003cul\u003e\n\u003cli\u003eVEB Baade 152 I Aircraft Brochure 1956 — 152-1956-brochure (German Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003e\u003cstrong\u003eVariant II — 2 Documents\u003c\/strong\u003e\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eBaade 152 II Aircraft Handbook\u003c\/strong\u003e\n\u003cul\u003e\n\u003cli\u003eVEB Baade 152 II Aircraft Specification Manual 1960 — Kurz_Bedienanlietung-1960 (German Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eBaade 152 II Slides, Photos and Brochures\u003c\/strong\u003e\n\u003cul\u003e\n\u003cli\u003eVEB Baade 152 II Aircraft Brochure 1958 — 152-1958-brochure (German Language)\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003cp\u003eThis collection covers both the 152\/I and 152\/II standards, spanning documentation from 1956 through 1960 — the full active development arc of the programme. The Kurz-Bedienungsanleitung (abbreviated operating instructions) volumes provide the most detailed surviving technical record of the aircraft's systems and operational procedures.\u003c\/p\u003e\n\u003ch2\u003eEngineering Norms and Standards\u003c\/h2\u003e\n\u003cp\u003eThe Baade 152 was designed to East German and Soviet-influenced engineering norms of the late 1950s, drawing on both German Junkers-era practices and TsAGI aerodynamic research.\u003c\/p\u003e\n\u003ch3\u003ePirna 014 Turbojet — Technical Data\u003c\/h3\u003e\n\u003cp\u003eThe aircraft was powered by four Pirna 014 turbojets, developed by the former Junkers-OKB engineering team — the only jet engine designed and produced in East Germany:\u003c\/p\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eType:\u003c\/strong\u003e Single-shaft axial-flow turbojet\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCompressor:\u003c\/strong\u003e 12-stage axial\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTurbine:\u003c\/strong\u003e 2-stage\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eThrust:\u003c\/strong\u003e 3,150 kp (6,900 lbf \/ 30.9 kN) at 8,000 rpm\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003ePressure ratio:\u003c\/strong\u003e 7:1\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCritical flaw:\u003c\/strong\u003e Fuel supply interrupted during steep nose-down descent angles (≥16°), a factor in the fatal 1959 crash of prototype DM-ZYA\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eInstallation:\u003c\/strong\u003e Mounted in pairs on 152\/I; redesigned individual pods on 152\/II\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003eAerodynamics and Handling\u003c\/h3\u003e\n\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eWing:\u003c\/strong\u003e High-mounted swept wing; TsAGI S-10s-9 profile at root, SR-3-12 at tip\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eStability issues:\u003c\/strong\u003e Nosewheel shimmy and tail surface vibration recorded during flight tests\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eHandling:\u003c\/strong\u003e Right-hand drift tendency on maiden flight due to non-uniform engine thrust\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eUndercarriage evolution:\u003c\/strong\u003e 152\/I — bicycle centreline gear with wingtip outriggers (unsuitable for commercial ops); 152\/II — conventional tricycle, main legs retracting into engine nacelles\u003c\/li\u003e\n\u003c\/ul\u003e\n\u003ch3\u003ePerformance Data (152\/II V4)\u003c\/h3\u003e\n\u003ctable\u003e\n\u003cthead\u003e\n\u003ctr\u003e\n\u003cth\u003eMetric\u003c\/th\u003e\n\u003cth\u003eSpecification\u003c\/th\u003e\n\u003c\/tr\u003e\n\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eMaximum Speed\u003c\/td\u003e\n\u003ctd\u003e920 km\/h (572 mph)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Speed\u003c\/td\u003e\n\u003ctd\u003e800 km\/h (497 mph)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eCruising Altitude\u003c\/td\u003e\n\u003ctd\u003e11,600 m (38,058 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange\u003c\/td\u003e\n\u003ctd\u003e2,000–2,500 km (1,243–1,553 miles)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e46,500 kg (102,515 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e~12,500 m (41,000 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\n\u003ch2\u003eFormat and Delivery\u003c\/h2\u003e\n\u003cp\u003eAll documents are delivered as high-resolution PDF files, optimised for both screen reading and printing. Files are organised by variant and document type. Instant download upon purchase. Compatible with all standard PDF readers on desktop, tablet, and mobile devices.\u003c\/p\u003e\n\u003ch2\u003eDisclaimer\u003c\/h2\u003e\n\u003cp\u003eAll documents in this collection are provided for historical research and archival reference only. The VEB Baade 152 programme was cancelled in 1961 and no airworthy examples exist. These materials are not intended for operational use. Trade names, designations, and document numbers are used for identification purposes only. Copyright © Sicuro Publishing.\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":52834606580059,"sku":null,"price":29.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/veb-baade-152-promotional-banner.png?v=1776484751","url":"https:\/\/onlineaviationlibrary.com\/products\/veb-baade-152-aircraft-manuals-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}