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Little Joe 1 (LJ-1) was a failed launch of a Little Joe by NASA, a solid fuel rocket that was designed for a Max Q abort and launch escape system test for the Mercury capsule. The objective was to determine how well the escape rocket would function under the most severe dynamic loading conditions anticipated during a Mercury-Atlas launching. [1]
Little Joe was a solid-fueled booster rocket used by NASA for eight launches from 1959 to 1961 from Wallops Island, Virginia to test the launch escape system and heat shield for Project Mercury capsules, as well as the name given to the test program using the booster. The first rocket designed solely for crewed spacecraft qualifications, Little ...
The Little Joe 1B was a launch escape system test of the Mercury spacecraft, conducted as part of the U.S. Mercury program. The mission also carried a female rhesus monkey (Macaca mulatta) named Miss Sam in the Mercury spacecraft. The mission was launched January 21, 1960, from Wallops Island, Virginia.
Little Joe 1A (LJ-1A) was an uncrewed rocket launched as part of NASA's Mercury program on November 4, 1959. [1] 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 ...
Launch Duration Purpose Result Little Joe 1: Boilerplate August 21, 1959 20 s Test of launch escape system during flight. Failure Big Joe 1: Big Joe Boilerplate September 9, 1959 13 m 00 s Test of heat shield and Atlas/spacecraft interface. Partial success Little Joe 6: Boilerplate October 4, 1959 5 m 10 s Test of spacecraft aerodynamics and ...
November 4, 1959: Launch of Little Joe 1A. Little Joe 1A was launched in a test for a planned abort under high aerodynamic load conditions. This flight was a repeat of the failed Little Joe 1 launch that had been planned for August 21, 1959. After lift-off, the pressure sensing system was to supply a signal when the intended abort dynamic ...
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The launch vehicle was the second in the series of Little Joe II vehicles, which had been developed to accomplish early and economical testing of the launch escape system. The Little Joe II was propelled by seven solid-propellant rocket motors - one Algol sustainer motor, which provided thrust for about 42 seconds, and six Recruit motors, which ...