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The VS-40 (''Foguete Suborbital VS-40'') is a Brazilian sounding rocket using solid fuel, stabilized aerodynamically, distributed between the first stage S40TM (4,200 kg) engine and the second stage S44M (810 kg) engine.〔http://www.iae.cta.br/?action=vs40〕〔http://www.astronautix.com/lvs/vs40.htm〕 This configuration corresponds to the upper stages of the VLS-1 rocket. ==Flights〔http://space.skyrocket.de/doc_lau_fam/s-40.htm〕== * VS-40 PT-01 - "''Operação Santa Maria''" - 1993/04/02 - Qualifying flight for the S44 engine. 760 seconds in micro-gravity. * VS-40 PT-02 - "''Operação Livramento''" - 1998/03/21 - VAP-1 (Fokker) payload. * VS-40M / SHEFEX II - 2012/06/22〔http://www.rocketrange.no/?page_id=751&campaign_id=16〕〔http://www.vnews.com.br/noticia.php?id=123510〕 - ''SHEFEX (Sharp Edge Flight Experiment) II'' payload. * VS-40M / V03 - "''Operação São Lourenço''" - in development - ''SARA - Satélite de Reentrada Atmosférica (Atmospheric Reentry Satellite) Suborbital 1'' 〔http://www.iae.cta.br/?action=sara〕〔http://www.inicepg.univap.br/cd/INIC_2008/anais/arquivosINIC/INIC0101_01_O.pdf〕〔http://www.brasil.gov.br/ciencia-e-tecnologia/2014/05/alcantara-sedia-encontro-que-discute-atividade-espacial-no-pais〕 - 2014 * VS-40 - in development - ''SARA Suborbital 2'' 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「VS-40」の詳細全文を読む スポンサード リンク
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