{"product_id":"tupolev-tu-16-badger-soviet-strategic-bomber-technical-document-collection","title":"Tupolev Tu-16 Badger — Soviet Strategic Bomber | Technical Document Collection","description":"\u003ch2\u003eTupolev Tu-16 Badger — Soviet Strategic Bomber\u003c\/h2\u003e\u003cp\u003eThe Tupolev Tu-16 (NATO reporting name: \u003cem\u003eBadger\u003c\/em\u003e) is one of the most significant Soviet aircraft of the Cold War era — a twin-engine, swept-wing strategic and naval bomber that first flew in April 1952 and entered service in 1954. Designed by the Tupolev OKB under Project 88, the Tu-16 served as the backbone of Soviet Long-Range and Naval Aviation for decades, was produced under license in China as the Xian H-6, and laid the aerodynamic foundation for the Tu-104 jet transport. Variants of the design remained in active service into the mid-2020s.\u003c\/p\u003e\u003ch2\u003eWhat This Collection Contains\u003c\/h2\u003e\u003cp\u003eThis living collection brings together primary-source English-language technical documentation on the Tu-16, sourced from declassified U.S. intelligence translations and original Soviet service manuals. Documents cover the full spectrum of aircraft systems — airframe, powerplant, avionics, armament, and flight operations.\u003c\/p\u003e\u003ch3\u003eDocument Manifest\u003c\/h3\u003e\u003cul\u003e\n\u003cli\u003e\n\u003cstrong\u003eAircraft Ty-16 — Description of Design, Book I:\u003c\/strong\u003e Aircraft Performance Characteristics\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTu-16 Badger — Flight Manual:\u003c\/strong\u003e Operating Limitations, Pre-Flight Inspection, Engine Starting, Taxiing, Pattern Flying, Landing, Advanced Manoeuvres\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eTu-16 Badger — Aircraft Service Manual, Book II:\u003c\/strong\u003e Navigation Equipment, Autopilot, Oxygen, Electrical, Photo and Radio Equipment\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAircraft Tu-16 — Technical Description, Book IV, Part 1:\u003c\/strong\u003e Electrical, Radio and Camera Equipment\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eAircraft TU-16 — Maintenance Instructions, Book III:\u003c\/strong\u003e Bombing Equipment (English Language)\u003c\/li\u003e\n\u003cli\u003e\n\u003cstrong\u003eCIA Intelligence Report — Soviet Manual on Maintenance of Bombing Equipment on the TU-16 Aircraft\u003c\/strong\u003e (February 1964, Declassified)\u003c\/li\u003e\n\u003c\/ul\u003e\u003ch2\u003eTechnical Highlights\u003c\/h2\u003e\u003ch3\u003eAerodynamics \u0026amp; Airflow\u003c\/h3\u003e\u003cp\u003eThe Tu-16 employs a 35° leading-edge wing sweep to mitigate shockwave drag in the high-subsonic flight regime. Wing fences and a semi-monocoque aluminum fuselage define its aerodynamic profile. Primary flight controls are manually operated with hydraulic boost augmentation and trim tabs.\u003c\/p\u003e\u003ch3\u003ePowerplant\u003c\/h3\u003e\u003cp\u003eTwo Mikulin AM-3 turbojets (approx. 85.3 kN \/ 19,180 lbf each) in early production; upgraded to RD-3M-500 turbojets (approx. 93.2 kN \/ 21,000 lbf each) in later missile-carrying variants. Engines are buried in the wing roots with optimized circular intakes at the fuselage-wing junction.\u003c\/p\u003e\u003ch3\u003eHandling \u0026amp; Stability\u003c\/h3\u003e\u003cp\u003eFlight test studies documented Dutch roll tendencies addressed by an integrated yaw damper in the autopilot. A rearward aerodynamic center shift occurs near Mach 0.85, requiring nose-up trim adjustment. Aeroelastic bending and torsional flexibility studies were integral to the aircraft's certification.\u003c\/p\u003e\u003ch3\u003ePerformance Data\u003c\/h3\u003e\u003ctable\u003e\n\u003cthead\u003e\u003ctr\u003e\n\u003cth\u003eSpecification\u003c\/th\u003e\n\u003cth\u003eValue\u003c\/th\u003e\n\u003c\/tr\u003e\u003c\/thead\u003e\n\u003ctbody\u003e\n\u003ctr\u003e\n\u003ctd\u003eCrew\u003c\/td\u003e\n\u003ctd\u003e6–7 (Pilot, Co-pilot, Navigator, Bombardier, Gunners, EW Operator)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Takeoff Weight\u003c\/td\u003e\n\u003ctd\u003e79,000 kg (174,165 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Speed\u003c\/td\u003e\n\u003ctd\u003e1,050 km\/h (Mach 0.85)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eService Ceiling\u003c\/td\u003e\n\u003ctd\u003e12,800–13,716 m (42,000–45,000 ft)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eRange (max payload)\u003c\/td\u003e\n\u003ctd\u003eapprox. 3,900 nmi (7,200 km)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eMax Bomb Load\u003c\/td\u003e\n\u003ctd\u003e9,000 kg (19,800 lb)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003ctr\u003e\n\u003ctd\u003eDefensive Armament\u003c\/td\u003e\n\u003ctd\u003e6–7 × 23mm AM-23 cannons (dorsal, ventral, tail turrets)\u003c\/td\u003e\n\u003c\/tr\u003e\n\u003c\/tbody\u003e\n\u003c\/table\u003e\u003ch3\u003eEngineering Bulletins\u003c\/h3\u003e\u003cp\u003eService documentation covers structural fatigue and life-cycle directives, missile conversion modifications (Badger-A to Badger-B\/C\/G variants), and pitot-static system integrity requirements for defensive turret and radar system operation.\u003c\/p\u003e\u003chr\u003e\u003cp\u003e\u003cem\u003eLiving Collections with Free Lifetime Updates — Please review our Disclaimer and Export Notice before purchasing.\u003c\/em\u003e\u003c\/p\u003e","brand":"Online Aviation Library","offers":[{"title":"Default Title","offer_id":53411676553563,"sku":null,"price":35.0,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0955\/4788\/3867\/files\/tu-16-promotional-banner.png?v=1781944543","url":"https:\/\/onlineaviationlibrary.com\/products\/tupolev-tu-16-badger-soviet-strategic-bomber-technical-document-collection","provider":"Online Aviation Library","version":"1.0","type":"link"}