Buran cruise missile
From Wikipedia, the free encyclopedia
The Buran cruise missile, designation RSS-40, was a Soviet intercontinental cruise missile capable of carrying a 3500 kg nuclear warhead. The project was canceled before flight tests began.[1]
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[edit] Development
The project was authorized on 20 May 1954, parallel to the development of the Burya missile. The development however, began in April 1953 as a rocket-aircraft system by Myasishchev OKB with internal designation M-40[2]. The project was canceled in November 1957, when two prototypes were just ready for flight testing, in favor of the R-7 Semyorka since ICBMs were unstoppable. Like the Burya, the Buran consisted of two stages, the booster rockets designated M-41, and the cruise missile stage designated M-42.
[edit] Specifications
[edit] General characteristics
- Function: Nuclear cruise missile
- Launch mass: 125000 kg
- Total length: 24.0 m
- Launch platform: Launch pad
- Status: Canceled before first flight tests
[edit] Launch vehicle (M-41)
- Engine: 4× RD-213
- Thrust: 4× 55 t
- Length: 19.1 m
- Diameter: 1.20 m
- Oxidizer: Liquid oxygen
- Combustible: Kerosene
[edit] Cruise missile (M-42)
- Engine: 1× RD-020 ramjet
- Speed : Mach 3.1-3.2
- Range: 8,500 km
- Flight altitude: 18-20 km
- Warhead: thermonuclear, 3500 kg
- Length: 23.3 m
- Diameter: 2.40 m
- Wing span: 11.6 m
- Wing area: 98 m²
[edit] Related content
[edit] Comparable missiles
SM-62 Snark - SM-64 Navaho - Burya
[edit] Referencess
- ^ FAS.org - "Burya / Buran- Russian / Soviet Nuclear Forces". Retrieved on 2006-06-17.
- ^ "Astronautix.org - "Buran". Retrieved on 2006-06-17.
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| Other: | TR-1 | RT-2 | RT-2PM | RT-2UTTH | RT-15 | RT-20 | RT-21 | RT-23 | RT-25 | RSM-56 | RKV-500A, RK-55 | KSR-5 | RSS-40 | UR-100 | UR-100 | UR-100N |
