KB SAT SR-10
| SR-10 | |
|---|---|
 | |
| First prototype of SR-10 during the flight. | |
| Role | Training aircraft |
| National origin | Russia |
| Manufacturer | KB SAT , Aviaaggregat , Smolensk SmAZ , KTRV |
| Designer | KB SAT |
| First flight | 25 December 2015 |
| Number built | 1 |
The KB SAT SR-10 is a prototype Russian single-engine jet trainer aircraft, fitted with forward-swept wings. It first flew in 2015, and is being offered to the Russian Air Force and for export.
Design and development
The Russian design bureau KB SAT (Sovremyenne Aviatsyonne Tekhnologii - Modern Aircraft Technologies) began work on a single-engine jet trainer and sport aircraft, the SR-10, in 2007, displaying a mockup at the MAKS airshow at Zhukovsky in August 2009. The SR-10 is a mid-wing monoplane of all-composite construction, with a wing swept forward at an angle of 10 degrees. The crew of two sit in a tandem cockpit. It is powered by a single turbofan, with a Ivchenko AI-25V fitted in the prototype, but more modern Russian engines, such as the NPO Saturn AL-55 are proposed for production aircraft.[1]
The SR-10 was offered to meet a 2014 requirement for a basic trainer for the Russian Air force, but was rejected in favour of the Yakovlev Yak-152, a proposed turboprop trainer. Despite this setback, KB SAT continued to develop the SR-10, proposing it as an intermediate trainer between the Yak-152 and the Yakovlev Yak-130 advanced trainer and for export. The first prototype SR-10 made its maiden flight on 25 December 2015.[1]
In July 2017, KB SAT announced it had developed an unmanned variant of the aircraft named the AR-10 Argument[2][3]
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Specifications (SR-10)
Data from Russia's New Jet Trainer[1]
General characteristics
- Crew: 2
- Length: 9.59 m (31 ft 6 in)
- Wingspan: 8.40 m (27 ft 7 in)
- Height: 3.55 m (11 ft 8 in)
- Gross weight: 2,400 kg (5,291 lb)
- Max takeoff weight: 2,700 kg (5,952 lb)
- Powerplant: 1 × Ivchenko AI-25V turbofan, 16.87 kN (3,790 lbf) thrust
Performance
- Maximum speed: 900 km/h (559 mph; 486 kn)
- Cruise speed: 520 km/h (323 mph; 281 kn)
- Range: 1,500 km (932 mi; 810 nmi)
- Service ceiling: 6,000 m (20,000 ft)
- g limits: +10/-8
- Rate of climb: 60 m/s (12,000 ft/min)
References
- 1 2 3 Butowski 2016, p. 15.
- ↑ "Russia Develops UAV Based on SR-10 Trainer". UAS Vision. 1 August 2017. Archived from the original on 1 August 2017. Retrieved 1 August 2017.
- ↑ Novinchkov, Nikolai (26 July 2017). "SAT develops SR-10-based UAV concept". IHS Jane's 360. Archived from the original on 1 August 2017. Retrieved 1 August 2017.
- Butowski, Piotr (February 2016). "Russia's New Jet Trainer". Air International. Vol. 90 no. 2. p. 15. ISSN 0306-5634.
External links
 |
Wikimedia Commons has media related to SAT SR-10. |
- "New Russian forward-swept wing jet trainer has made its first flight. And here’s the video". The Aviationist. 2 January 2016.
- "Russia’s 1st forward-swept wing training aircraft performs maiden flight (VIDEO)". Russia Today. 1 January 2016.
- KB-SAT official site (in Russian)