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Capricornio (rocket) : ウィキペディア英語版 | Capricornio (rocket)
Capricornio was a Spanish satellite launch vehicle developed by the ''Instituto Nacional de Técnica Aeroespacial'' (''INTA'') in the 1990s. It was expected to be a low cost solution to place up to 70 kg payloads into 600 km polar orbits or 60 to 140 kg payloads into low Earth orbit. Part of the technology was related to Argentina's Condor missile program. ==Development==
* First phase: development of solid motors using the INTA-100 and INTA-300 sounding rockets, launched from the El Arenosillo test range in southern Spain. * Second phase: use Capricornio second and third stages as the Argos sounding rocket (originally planned for winter 1998-99). * Third phase: first launch of the full Capricornio rocket, carrying a micro-satellite.
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「Capricornio (rocket)」の詳細全文を読む
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