| 词条 | Draft:Geosynchronous Satellite Launch Vehicle Mk II |
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This page has been declined or rejected as an abandoned draft by an inactive editor. If it is not edited further within six months after it has been declined or rejected, it will be deleted as a disused draft. Since the originator of this draft is inactive, any comments may be addressed to the last reviewer. Robert McClenon (talk) 07:48, 23 February 2019 (UTC)}} Geosynchronous Satellite Launch Vehicle Mk II is the second in the GSLV Mark series of launch vehicles developed by Indian Space Research Organisation. GSLV Mk-II is capable of launching satellites which can weigh up to 2,500 kg in geosynchronous transfer orbit. It differs from GSLV Mk I in the sense that it uses Indian made cryogenic engine for CUG while former one used russian made engine.[1] References1. ^http://space.skyrocket.de/doc_lau_det/gslv_mk2.htm |
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