Little Joe 6
Template:Short description Template:Infobox spaceflight 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.[1] The Little Joe 6 flew to an apogee of Script error: No such module "convert". and a range of Script error: No such module "convert".. The mission lasted 5 minutes 10 seconds. Maximum speed was Script error: No such module "convert". and acceleration was 5.9 g (58 m/s²). Payload Script error: No such module "convert"..[2]
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References
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