Tupolev Tu-95LAL

· Tupolev
Length
46.2 m
Flat Wing Span
50.1 m
Height
12.12 m
Flat Wing Area
310 m²
Cruise Speed
750 km/h
Number of Engines
4
First Flight
1961-01-01
Number Built
1
Maximum Range
4700 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Tupolev Tu-95LAL 4700

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m)
Tupolev Tu-95 Kuznetsov NK-12 46.2 50.1 Compare
Beriev A-100 46.59 50.5 Compare
Ilyushin Il-78 46.59 50.5 Compare
Ilyushin Il-76 Aviadvigatel PS-90 46.6 50.5 Compare
Beriev A-50 46.6 50.6 Compare
Xi'an Y-20 Shenyang WS-20 47 50 Compare
All data (16 fields)
Name
Tupolev Tu-95LAL
Manufacturer
Tupolev
Description
The Tupolev Tu-95LAL experimental aircraft () which flew from 1961 to 1965 was a modified Tupolev Tu-95 Soviet bomber aircraft, analogous to the United States' earlier Convair NB-36H.
First Flight
1961-01-01
Designer
Tupolev
Type
Experimental nuclear aircraft
Length (m)
46.2
Height (m)
12.12
Cruise Speed (km/h)
750
Endurance (h)
6.4
Number Built
1
Powerplant Description
4 × Kuznetsov NK-12M turboprop engines
Wikipedia Article (URL)
en.wikipedia.org/wiki/Tupolev_Tu-95LAL
Flat Wing Span (m)
50.1
Flat Wing Area (m²)
310
Number of Engines
4