Saturn AL-41
This article needs additional citations for verification. (May 2014) |
AL-41F | |
---|---|
AL-41F1S engine | |
Type | Turbofan |
National origin | Russia |
Manufacturer | NPO Saturn , UMPO , NPC Saljut |
The AL-41F is a designation for two different Russian military turbofan engine variants. The NPO Saturn AL-41F is a Russian variable-bypass ratio turbofan engine, designed for supercruise flight for the MFI (Mnogofunktsionalni Frontovoy Istrebitel, "Multifunctional Frontline Fighter") program, which resulted in the Mikoyan Project 1.44. It is considered by Jane's as the Russian counterpart to the General Electric YF120 engine which lost to the more conventional fixed-bypass YF-119 in the Advanced Tactical Fighter engine program. Since the cancellation of the MFI program, the AL-41F1S and AL-41F1 designation was assigned to heavily upgraded AL-31F variants that powers the Su-35S and initial production Sukhoi Su-57 stealth aircraft.
Design and development
The AL-41F program was launched in 1982, and the first prototype engine flew in a MiG-25 Foxbat testbed. Originally developed for the Mikoyan Project 1.44,[1] 28 engines were built, however the engine did not advance beyond prototype stage when the MiG 1.44 was cancelled.
The AL-41 designation was reused for heavily upgraded variants of the Saturn AL-31 used to power the Sukhoi Su-35 (Izdeliye 117S/AL-41F1S) and initial production Sukhoi Su-57 (Izdeliye 117/AL-41F1) stealth aircraft. Some of the technologies of the original AL-41F were applied in the Izdeliye 117S, 117 engines[2][3]. It is important to note that the AL-41F1S is not considered a part of the same AL-41 line as was planned for the Mikoyan Project 1.44 because it uses the core of the AL-31F, whereas the AL-41F utilizes an entirely different approach.
Operators
Specifications
General characteristics
- Type: Turbofan
- Length: 4990 mm
- Diameter: 1280 mm
- Dry weight: 1,420 kilogram (3,131 pound)
Components
- Compressor: axial
Performance
- Maximum thrust: 18,000 kgf (180,000 N; 40,000 lbf)
- Thrust-to-weight ratio: 11:1
See also
References
- ^ "Archived copy". Archived from the original on 2010-06-16. Retrieved 2012-09-21.
{{cite web}}
: Unknown parameter|deadurl=
ignored (|url-status=
suggested) (help)CS1 maint: archived copy as title (link) - ^ Пятое отклонение kommersant 10.12.2007
- ^ Пятое отклонение kommersant 10.12.2007
Sources
- Butowski, Piotr. "Raptorski's Maiden Flight". Air International, Vol. 78, No 3, March 2010, pp. 30–37. Stamford, UK: Key Publishing.
- Butowski, Piotr. "T-50 Turning and Burning over Moscow". Air International, Vol. 85, No 4, October 2013, pp. 79–82. Stamford, UK: Key Publishing.