About: Tupolev Tu-125

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An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Tupolev Tu-125 was an unrealized project to develop a new long-range supersonic bomber for the Soviet Air Force. 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. In September 1962, the Soviet Air Force rejected the project and it was stopped. No aircraft were built.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Tupolev Tu-125
rdfs:comment	The Tupolev Tu-125 was an unrealized project to develop a new long-range supersonic bomber for the Soviet Air Force. 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. In September 1962, the Soviet Air Force rejected the project and it was stopped. No aircraft were built.
sameAs	dbr:Tupolev_Tu-125
dcterms:subject	dbkwik:resource/8BfhgATC5_fqWJWBD4FMIA== dbkwik:resource/9rh1gF7JXSY5VfZAdOI4gA== dbkwik:resource/qtDLJtdsFaCfUNYHP4qMfw==
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range km	7000(xsd:integer)
gross weight kg	110000(xsd:integer)
Type	Supersonic bomber
height m	9(xsd:double)
span m	22(xsd:double)
missiles	1(xsd:integer)
wing loading kg/m	487(xsd:integer)
Manufacturer	Tupolev OKB
max speed kmh	3500(xsd:integer)
eng1 kn	110(xsd:integer)
ceiling m	25000(xsd:integer)
thrust/weight	0(xsd:double)
length m	41(xsd:double)
National Origin	USSR
wing area sqm	226(xsd:integer)
prime units?	met
eng1 name	dbkwik:resource/5l9wD7bda-urCsX0X0ufuA==
eng1 number	4(xsd:integer)
abstract	The Tupolev Tu-125 was an unrealized project to develop a new long-range supersonic bomber for the Soviet Air Force. 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. 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-15B-300s in two nacelles also was considered. The fuselage and wings made from titanium and aluminium alloys. In September 1962, the Soviet Air Force rejected the project and it was stopped. No aircraft were built.

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