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SCE-200 : ウィキペディア英語版
SCE-200

The SCE-200 is a liquid-fuel rocket engine being developed by the Liquid Propulsion Systems Centre, a subsidiary of India's space agency ISRO. It is being developed to power the future heavy-lift Unified Launch Vehicle (ULV) and the Reusable Launch Vehicle (RLV) being planned by ISRO〔 but before that it will be tested with GSLV Mk III by replacing L110(powered by old Vikas engine) stage to SC160.
The primary goal of ISRO will be making new SLV family called ULV (Unified Launch Vehicle) by replacing currently operational PSLV, GSLV and GSLV Mk III. The ULV (Unified Launch Vehicle) marks the renunciation of India for N2O4/UDMH as propellant for space launch vehicle systems.
==History==
On June 2, 2005, India and Ukraine signed the ''Framework Agreement between the Government of Ukraine and the Government of the Republic of India on Cooperation in the Peaceful Uses of Outer Space'', which would enter in force on February 15, 2006.〔 As per unconfirmed information obtained by Wikileaks this contract involved the transfer of technology and blueprints for a rocket engine by the Yuzhnoye Design Office.〔〔〔 The engine designs involved in the transfer are identified as the RD-810.〔〔
During May and June of 2015, ISRO and Roscosmos signed a wide-ranging Memorandum of Understanding for cooperation in space.〔 A. S. Kiran Kumar, Chairman of the Indian Space Research Programme, stated that one of the first benefits would be the availability of Russian test stand for initial testing of the SCE-200, while the Mahendragiri semi-cryogenic test stand is finally commissioned. He also stated that the engine was part of the Rs. 1,800-crore semi-cryogenic launch vehicle programme, which would be capable of placing to in the GTO.〔〔 This cooperation would only be for facilities use and would have no technology transfers, thus, eliminating the international political risk.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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