Little Joe 6

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search

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]

See also

References

<templatestyles src="Reflist/styles.css" />

  1. Script error: No such module "citation/CS1".
  2. Script error: No such module "citation/CS1".

Script error: No such module "Check for unknown parameters".

Template:Include-NASA

Script error: No such module "Navbox".

Template:Asbox