Search results
Results from the WOW.Com Content Network
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]
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 ...
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 ]
Tharkaytha GT + Max Power Co, Ltd Tharkaytha, Yangon Division 92 + 50 1990-1997/2013 EPGE/Max Power Co, Ltd Shwe Taung Gas Engine Based Power Plant Shwe Taung, Bago Division 28 + 42 2020/2022 EPGE [22]
Language links are at the top of the page. Search. Search
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]
Location Owner/operator Co-ordinates Capacity Baikonur solar power plant Kyzylorda Region: Baikonur Solar LLP 50 M-KAT Jambyl Region: Access Power Limited: 75 Nomad Kyzylorda Region: Access Power Limited: 28 Nurgisa: Almaty Region: 100 Burnoye Solar-1 Zhualy: Kazakh Samruk Kazyna Invest LLP 50 Burnoye Solar-2 Zhualy: Kazakh Samruk Kazyna Invest ...
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 ...