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C o n t r i b u t e
● H e l p ● L e a r n t o e d i t ● C o m m u n i t y p o r t a l ● R e c e n t c h a n g e s ● U p l o a d f i l e
S e a r c h
Search
A p p e a r a n c e
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P e r s o n a l t o o l s
● C r e a t e a c c o u n t ● L o g i n
P a g e s f o r l o g g e d o u t e d i t o r s l e a r n m o r e ● C o n t r i b u t i o n s ● T a l k
( T o p )
1 S p e c i f i c a t i o n s ( T u - 1 2 5 T u m a n s k y e n g i n e s – e s t i m a t e d )
2 S e e a l s o
3 N o t e s
4 R e f e r e n c e s
T o g g l e t h e t a b l e o f c o n t e n t s
T u p o l e v T u - 1 2 5
4 l a n g u a g e s
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E d i t l i n k s
● A r t i c l e ● T a l k
E n g l i s h
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T o o l s
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A c t i o n s
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G e n e r a l
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P r i n t / e x p o r t
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A p p e a r a n c e
F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
Tu-125
Role
Supersonic medium bomber
Type of aircraft
National origin
USSR
Manufacturer
Tupolev
The Tupolev Tu-125 was an unrealized project to develop a new long-range supersonic bomber for the Soviet Air Force .[1] [better source needed Development commenced in 1958 to replace the newest Tu-22 . The "Tu-125" designation was an internal one used by the Tupolev design bureau. Since the aircraft was never built, it never received a military designation.[2]
A canard design was chosen for the aircraft, featuring a delta planform for the wing and stabilizer. Two turbojets (Kuznetsov NK-6 or NK-10 (230–240 kN )) were to be installed in nacelles under the wings. A four-turbojet version, powered by Tumansky R-15 B-300s in two nacelles also was considered. The fuselage and wings made from titanium and aluminium alloys.[2]
In September 1962 , the Soviet Air Force rejected the project and it was stopped. No aircraft were built.[2]
Specifications (Tu-125 Tumansky engines – estimated) [ edit ]
General characteristics
Length: 41.40 m (135 ft 10 in )
Wingspan: 22.20 m (72 ft 10 in )
Height: 9.55 m (31 ft 4 in )
Wing area: 226.0 m 2 ft )
Gross weight: 110,000 kg (242,508 lb )
Powerplant: 4 × Tumansky R-15B-300 , 110 kN (25,000 lbf) thrust each
Performance
Maximum speed: 3,500 km/h (2,200 mph, 1,900 kn )
Range: 7,000 km (4,300 mi, 3,800 nmi)
Service ceiling: 25,000 m (82,000 ft )
Wing loading: 487 kg/m2 ft )
Thrust/weight :
Armament
See also [ edit ]
Aircraft of comparable role, configuration, and era
^ a b c Buttler, Tony; Yefim Gordon (2004). Soviet Secret Projects – Bombers Since 1945 . Hinkley: Midland publishing. pp. 132–134. ISBN 1-85780-194-6
References [ edit ]
Buttler, Tony; Yefim Gordon (2004). Soviet Secret Projects – Bombers Since 1945 . Hinkley: Midland publishing. pp. 132–134. ISBN 1-85780-194-6
t
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Civilian
Military
Unmanned
Experimental
Proposed,
Early period
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● T h i s p a g e w a s l a s t e d i t e d o n 2 8 M a y 2 0 2 3 , a t 1 6 : 3 9 ( U T C ) . ● T e x t i s a v a i l a b l e u n d e r t h e C r e a t i v e C o m m o n s A t t r i b u t i o n - S h a r e A l i k e L i c e n s e 4 . 0 ;
a d d i t i o n a l t e r m s m a y a p p l y . B y u s i n g t h i s s i t e , y o u a g r e e t o t h e T e r m s o f U s e a n d P r i v a c y P o l i c y . W i k i p e d i a ® i s a r e g i s t e r e d t r a d e m a r k o f t h e W i k i m e d i a F o u n d a t i o n , I n c . , a n o n - p r o f i t o r g a n i z a t i o n . ● P r i v a c y p o l i c y ● A b o u t W i k i p e d i a ● D i s c l a i m e r s ● C o n t a c t W i k i p e d i a ● C o d e o f C o n d u c t ● D e v e l o p e r s ● S t a t i s t i c s ● C o o k i e s t a t e m e n t ● M o b i l e v i e w
