TUPOLEV TU-95

Aircraft
Name: 
TU-95
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Mid wing
Tail: 
Regular tail, mid set
WTC
H
APC
C
Type Code: 
L4T
Engine: 
Turboprop
Engine Count: 
Multi
Position: 
(Front) Wing leading mounted
Landing gear: 
Tricycle retractable
Manufacturered as
TUPOLEV Tu-142
TUPOLEV Tu-20
TUPOLEV Tu-95

TU95

The Tupolev Tu-95 is a large, four-engine turboprop-powered strategic bomber and missile platform. First flown in 1952, the Tu-95 entered service with the Soviet Union in 1956 and is expected to serve the Russian Air Force until at least 2040. A naval development of the bomber is designated Tu-142.

Technical Data
Wing span: 
51.10 m
Length: 
49.20 m
Height: 
12.12 m
Powerplant: 

4 x Kuznetsov NK-12M turboprops, 11,000 kW each.

Engine Model: 
Kuznetsov NK-12
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
188000 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
435 kts
MACH: 
n/a
Ceiling: 
410
Range: 
6775 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
n/a

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