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・ Little Lights Free Education High School
・ Little Lili
・ Little Lillooet Lake
・ Little Lima
・ Little Limestone Lake
・ Little Linford
・ Little Linga
・ Little Lion Man
・ Little Lit
・ Little Lithodendron Wash
・ Little Little
・ Little Livermere
・ Little Liverpool Range
・ Little Llangothlin Nature Reserve
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Little Joe 1A
・ Little Joe 1B
・ Little Joe 2
・ Little Joe 5
・ Little Joe 5A
・ Little Joe 5B
・ Little Joe 6
・ Little Joe Blue
・ Little Joe Cook
・ Little Joe II
・ Little Joe II Qualification Test Vehicle
・ Little Joe River
・ Little Joe the Wrangler
・ Little Joe's
・ Little John


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Little Joe 1A : ウィキペディア英語版
Little Joe 1A

Little Joe 1A (LJ-1A) was an unmanned rocket launched as part of NASA's Mercury program on November 4, 1959. This flight, a repeat of the Little Joe 1 (LJ-1) launch, was to test a launch abort under high aerodynamic load conditions. After lift-off, the pressure sensing system was to indicate when the correct abort dynamic pressure was reached. This should have happened about thirty seconds after launch. A signal was sent to the explosive bolts to separate the spacecraft from the launch vehicle. Up to this point, everything was going as planned. The impulse was also intended to ignite the escape motor. The motor was ignited, but it took a number of seconds to build up thrust, and thus the abort maneuver was not accomplished at the desired dynamic pressure. Because of this, a repeat of the test was planned. Other events from launch through recovery occurred without incident. An altitude of 9 statute miles (14.5 km) and a range of 11.5 statute miles (18.5 km) were obtained, and a speed of 2,021.6 miles per hour (3,254 km/h) was reached. Flight time 8 minutes 11 seconds. Payload 1,007 kg.
==See also==

* Little Joe


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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