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Little Joe 6 : ウィキペディア英語版 | Little Joe 6
The Little Joe 6 was a Launch Escape System test of the Mercury spacecraft, conducted as part of the U.S. Mercury program. The mission used a boilerplate Mercury spacecraft. The mission was launched October 4, 1959, from Wallops Island, Virginia. The Little Joe 6 flew to an apogee of and a range of . The mission lasted 5 minutes 10 seconds. Maximum speed was and acceleration was 5.9 g (58 m/s²). Payload . ==See also==
* Little Joe * Boilerplate (spaceflight)
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「Little Joe 6」の詳細全文を読む
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