Tupolev Tu-95

· Tupolev · 4 × Kuznetsov NK-12

Airplanes

Length

46.2 m

Flat Wing Span

50.1 m

Height

12.12 m

Flat Wing Area

310 m²

Cruise Speed

710 km/h

Max Speed

925 km/h

Max Ceiling

13716 m

Number of Engines

Aircraft Engine

First Flight

1952-11-12

Entry Into service

1956-01-01

Number Built

500

Maximum Take-Off Weight

188 t (paragliders: kg)

Maximum Range

15000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Tupolev Tu-95	188	15000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Myasishchev M-4		47.2	50.5		Compare
Tupolev Tu-116		46.17	54.1	24	Compare
Beriev A-50		46.6	50.6		Compare
Ilyushin Il-78		46.59	50.5		Compare
Ilyushin Il-76	Aviadvigatel PS-90	46.6	50.5		Compare
Tupolev Tu-95LAL		46.2	50.1		Compare

All data (28 fields)

Name: Tupolev Tu-95
Manufacturer: Tupolev
Description: The Tupolev Tu-95 (; NATO reporting name: "Bear") is a large Soviet nuclear-capable, four-engine turboprop strategic bomber and missile launch platform.
ICAO Code: TU95
First Flight: 1952-11-12
Entry Into service: 1956-01-01
Production End: 1993-01-01
Designer: Tupolev
Type: Strategic heavy nuclear bomber
Length (m): 46.2
Height (m): 12.12
Cockpit Crew: 6
Max Speed (km/h): 925
Cruise Speed (km/h): 710
Max Ceiling (m): 13716
Rate of Climb (m/s): 10
Armament: 2 × 23 mm Gryazev-Shipunov GSh-23 autocannon in tail turret; Up to 15000 kg, including the Kh-20, Kh-22, and Kh-55/101/102, or 8 Kh-101/102 cruise missiles mounted on underwing pylons.
National Origin: Soviet Union
Number Built: 500
Powerplant Description: 4 × Kuznetsov NK-12 turboprop engines
Primary Users: Russian Aerospace Forces, Soviet Air Forces (historical) , Soviet Navy (historical) , Ukrainian Air Force (historical)
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Tupolev_Tu-95
Flat Wing Span (m): 50.1
Flat Wing Area (m²): 310
Wake Category: H
Aircraft Engine: Kuznetsov NK-12
Number of Engines: 4