Tsybin RSR
From Wikipedia, the free encyclopedia
| RSR | |
|---|---|
| Type | Reconnaissance Aircraft |
| Manufacturer | Tsybin |
| Status | Prototype/Project |
The Tsybin RSR (Reactivnyi Strategicheskii Razvedchik) was a Russian design for an advanced, long-range, Mach 3 strategic reconnaissance aircraft.
Contents |
[edit] Development and design
In 1954, the design bureau headed by Pavel Tsybin started development of a ramjet powered strategic supersonic bomber, the RS. This design proved impracticable, and a smaller derivative, the 2RS was proposed, which would achieve intercontinental range by being air launched from a modified Tupolev Tu-95 bomber.[1]
This too was unsuccessful, with the aircraft unable to return to base if used on an intercontinental mission,[1] while being incapable of carrying a thermonuclear bomb.[2] The design was therefore revised again to to a reconnaissance aircraft capable of operating from conventional runways, the RSR. As ramjets could not be used for take-off, they were replaced by turbofans.[1]
The RSR was primarily of aluminium construction, with a long circular section fuselage, which housed a pressure cabin for the pilot together with cameras and fuel, with thin, low aspect ratio trapezoidal wings. The engines, two Soloviev D-21 turbofans, were mounted at the tips of the wings. The aircraft had a bicycle underarriage, with outriggers under the engine nacelles. It was planned to cruise at greater than Mach 2 at a height of 20,000 m (65,600 ft) giving a range of 3,760 km (2,340 miles).[3]
A simplified, full sized aerodynamic prototype for the novel layout, the NM-1 was built in 1957. This aircraft, powered by two Mikulin AM-5 turbojets first flew on 7 April 1959.[3] Based on the results of these trials, the RSR was redesigned (as the R-020) to make it more manouverable at high altitude (it was proposed to carry out barrel rolls to avoid Surface-to-air missiles, reaching a maximum altitude of 42,000 m (138,000 ft) during the manouver.[4] More conventional Tumansky R-11 turbojets (the engine used in the MiG-21 replaced the unavailable Soloviev turbofans. Five R-020 airframes were vitually complete, only awaiting engines by April 1961, with another 10 planned when Soviet Premier Nikita Kruschev cancelled the program.
[edit] Specifications (NM-1)
Data from The Osprey Encyclopedia of Russian Aircraft 1875 - 1995 [5]
General characteristics
- Crew: One
- Length: 26.57 m (87 ft 3¼ in)
- Wingspan: 10.48 m (34 ft 4⅝ in)
- Height: ()
- Wing area: 64 m² [6] (689 ft²)
- Empty weight: 6,355 kg (14,010 lb)
- Loaded weight: 9,000 kg (19,800 lb)
- Powerplant: 2× Mikulin AM-5 turbojet, 49kN (4,410 lbf)2,000 kgf each
Performance
- Maximum speed: 500 km/h (324 knots, 373 mph)
- Service ceiling 4,000 m [6] (13,000 ft)
- Wing loading: kg/m² (lb/ft²)
[edit] References
[edit] Notes
- ^ a b c Butowski 1998. p.39-40
- ^ Gunston 1995, p.376
- ^ a b Gunston 1995, p.377
- ^ Tsybin R-020 www.testpilot.ru. Retrieved 28 February 2008.
- ^ Gunston 1995, p.378
- ^ a b Tsybin NM-1www.testpilot.ru. Retrieved 28 February 2008.
[edit] Bibliography
- Butowski, Piotr. "Steps Towards 'Blackjack': Soviet supersonic intercontinental bombers before the Tu-144". Air Enthusiast. No. 73, January - February 1998. Stamford, Linconshire: Key Publishing. Page 36-49. ISSN 0143 5430.
- Gunston, Bill. The Osprey Encyclopedia of Russian Aircraft 1875 - 1995. London: Osprey, 1995. ISBN 1 85532 405 9.
