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The Su-30MKI was designed by Russia's Sukhoi Corporation beginning in 1995 and built under licence by India's Hindustan Aeronautics Limited (HAL). [11] [12] The Su-30MKI is derived from the Sukhoi Su-27 and has a fusion of technology from the Su-37 demonstrator and Su-30 program, [13] being more advanced than the baseline Su-30. [13]
The Su-30MKM was developed by the Sukhoi Design Bureau and is based on the Su-30MKI of the Indian Air Force. Both aircraft have common airframe , thrust vectoring engines and a digital fly-by-wire system, however the MKM version differs from the MKI mainly in the composition of the onboard avionics . [ 1 ]
There are already many maps of nuclear power stations out there on the internet. For example, the INSCDB Map s (example: Image:Ukraine nuclear power plants.png) [dead link ] have already been used on a number of other language Wikipedias because they are somehow released into the public domain or gave permission for the usage.
A version of the Su-30MKI sold to Algeria. All of the Israeli equipment, like the head-up display and the digital map generator, is replaced by Indian equivalents. [141] Su-30MKM (Flanker-H) A derivative of the Russian-Indian Su-30MKI, [142] the MKM is a highly specialised version for Royal Malaysian Air Force. It includes thrust vectoring ...
Power station No. of units Net capacity under construction (Construction start Planned connection Country Location; Akkuyu: 4: 4,456: 2015: 2025 Turkey Bushehr: 2 2100 2017
The Sukhoi Su-30MKK (NATO reporting name: Flanker-G) [2] is a modification of the Sukhoi Su-30, incorporating advanced technology from the Sukhoi Su-35 variant. The Su-30MKK was developed by Sukhoi in 1997, as a result of a direct Request for tender between the Russian Federation and China. [3]
Renewable energy power stations in Asia by country (41 C) A. Power stations in Afghanistan (1 C, 2 P) Power stations in Armenia (4 C, 1 P)
The design of the AL-31 turbofan began in the 1970s under the designation izdeliye 99 [N 1] by the Lyulka design bureau, also known as Lyulka-Saturn. With an emphasis on greater fuel efficiency over turbojets for longer range, the 12.5 tonnes-force (122.6 kN; 27,560 lbf) class turbofan engine was intended to power the heavy PFI (Russian: ПФИ, short for: перспективного ...