In 1957, the Tupolev Design Bureau was in very good standing. Their Tu-95 was being actively introduced to the Air Force, their Tu-16 was being produced in three plants. Tupolev, however, was worried about Nikita Khrushchev's growing interest in rocket weapons. The USSR had made significant progress in rocket science and was preparing to launch their first rocket – the R-7. Rockets seemed invincible for existing and future anti-aircraft systems. Soviet bombers were not so lucky, being extremely vulnerable. The NORAD system, which was being developed and deployed by the United States at the time was practically impermeable for the strategic bombers of that era.[1]
Various attempts to arm Tu-95s with missiles had a serious drawback – the bomber itself remained vulnerable to interceptors and ground-to-air missiles.
Tu-121 was conceived as an aircraft able to reach speeds of over 2,000 km/h and a flight altitude of 50 km which would allow it to easily penetrate both American air- and missile defence systems.
However, even at the early stages, Tupolev himself realized that his bureau was unable to develop such an aircraft. The biggest problem was immense heat. The materials necessary to build the heat-shield were developed only in the 1980s for the Buran programme.
The aircraft was built and several test launches were performed. However, it did not go beyond the prototype phase. The R-12 rocket, developed by Mikhail Yangel had better range and accuracy. On 5 February 1960, the project was officially cancelled.
The aircraft was a full-metal monoplane made almost entirely of traditional materials. The wing had no high-lift devices. The aircraft was piloted using vertical and horizontal stabilizers. Most of the fuselage consisted of fuel tanks.
tupolev, unmanned, aircraft, intended, cruise, missile, designed, tupolev, soviet, union, during, cold, 121role, unmanned, aerial, vehiclenational, origin, ussrmanufacturer, tupolevdesigner, alexey, tupolevfirst, flight, 1959status, prototypenumber, built, pro. The Tupolev Tu 121 was an unmanned aircraft intended for use as a cruise missile designed by Tupolev in the Soviet Union during the Cold War Tu 121Role Unmanned aerial vehicleNational origin USSRManufacturer TupolevDesigner Alexey TupolevFirst flight 1959Status PrototypeNumber built 1 prototype Contents 1 Development 2 Specifications 3 See also 4 ReferencesDevelopment editIn 1957 the Tupolev Design Bureau was in very good standing Their Tu 95 was being actively introduced to the Air Force their Tu 16 was being produced in three plants Tupolev however was worried about Nikita Khrushchev s growing interest in rocket weapons The USSR had made significant progress in rocket science and was preparing to launch their first rocket the R 7 Rockets seemed invincible for existing and future anti aircraft systems Soviet bombers were not so lucky being extremely vulnerable The NORAD system which was being developed and deployed by the United States at the time was practically impermeable for the strategic bombers of that era 1 Various attempts to arm Tu 95s with missiles had a serious drawback the bomber itself remained vulnerable to interceptors and ground to air missiles Tu 121 was conceived as an aircraft able to reach speeds of over 2 000 km h and a flight altitude of 50 km which would allow it to easily penetrate both American air and missile defence systems However even at the early stages Tupolev himself realized that his bureau was unable to develop such an aircraft The biggest problem was immense heat The materials necessary to build the heat shield were developed only in the 1980s for the Buran programme The aircraft was built and several test launches were performed However it did not go beyond the prototype phase The R 12 rocket developed by Mikhail Yangel had better range and accuracy On 5 February 1960 the project was officially cancelled The aircraft was a full metal monoplane made almost entirely of traditional materials The wing had no high lift devices The aircraft was piloted using vertical and horizontal stabilizers Most of the fuselage consisted of fuel tanks Specifications editData from http www airwar ru enc bpla tu121 htmlGeneral characteristicsCrew unmanned Length 24 77 m 81 ft 3 in Wingspan 8 40 m 27 ft 7 in Empty weight 11 450 kg 25 243 lb Max takeoff weight 35 000 kg 77 162 lb Fuel capacity 16 600 kgPerformance Maximum speed 2 775 km h 1 724 mph 1 498 kn See also editAircraft of comparable role configuration and era AGM 28 Hound DogReferences edit Tu 121 Airwar RU Retrieved 4 January 2019 Retrieved from https en wikipedia org w index php title Tupolev Tu 121 amp oldid 993823039, wikipedia, wiki, book, books, library,
