Yak-35 Bomber
In autumn 1961 the Ministry of Aviation Industry of the USSR issued OKB-156 Tupolev, DB-51 Sukhoi and OKB-115 Sukhoi Design Bureau the task to develop on a competitive basis a supersonic bomber-missile. Tupolev presented the project "135" and Sukhoi the T-4. Yakovlev proposed aircraft Yak-35 project represent a "tailless" configuration with a delta wing and motors located under the wings. The main construction material was supposed to heat-resistant steel. At the same time, two engine-building design bureau offered their engines: S.Tumansky - P-15 (developed at that time for the MiG-25 ) and P.Kolesov - R-36-41 (the engine and got preference).
The guided anti-ship missile Kh-45 was created A.Bereznyaka team. The works of three aircraft-building Design Bureau carefully studied the institutions and, in July and September 1962 were discussed at the scientific-technical council of the Ministry. The Yakovlev Design Bureau project was rejected in favor of the T-4.
| developer | Yakovlev Design Bureau |
| designation | Yak-35 |
| type | The supersonic missile crrier |
| Crew | 2 (?) |
| Dimensions & Weight | |
| Aircraft Length m | |
| Takeoff weight, kg | 90000 |
| number of engine | s 4 |
| Engine | TRD RD36-41 |
| Engine Thrust, kgf | 16150 |
| Flight data (calculated) | |
| Flight distance, km | 7200 (7000-8000) |
| Flight speed at height, km / h | 3000-3200 |
| weaponry | SD "air-land" 2 X-45 |
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