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A pad abort test is a test of a launch escape system to determine how well the system could get the crew of a spacecraft to safety in an emergency on the launch pad. == Project Mercury == ''Section sources.''〔(Mercury Pad Abort Tests )〕〔(NASA History Archives )〕 The Mercury program included several pad abort tests for the launch escape system with a boilerplate crew module. * 1959 July 22 - First successful pad abort flight test with a functional escape tower attached to a Mercury Boilerplate. * 1959 July 28 - A Mercury Boilerplate with instruments to measure sound pressure levels and vibrations from the Little Joe test rocket and Grand Central abort rocket/escape tower. 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「Pad abort test」の詳細全文を読む スポンサード リンク
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