Little Joe 5B
Little Joe 5B prepared for launch, Wallops Island | |
Mission type | Abort test |
---|---|
Operator | NASA |
Mission duration | 5 minutes, 25 seconds |
Distance travelled | 14 kilometres (9 mi) |
Apogee | 4.5 kilometres (2.8 mi) |
Spacecraft properties | |
Spacecraft | Mercury No.14 |
Manufacturer | McDonnell Aircraft |
Launch mass | 1,141 kilograms (2,515 lb) |
Start of mission | |
Launch date | April 28, 1961, 14:03 UTC |
Rocket | Little Joe |
Launch site | Wallops LA-4 |
End of mission | |
Landing date | April 28, 1961, 14:08 UTC |
Project Mercury Abort Tests |
Little Joe 5B was an unmanned Launch Escape System test of the Mercury spacecraft, conducted as part of the US Mercury program. The mission used production Mercury spacecraft # 14A. The mission was launched April 28, 1961, from Wallops Island, Virginia. The Little Joe 5B flew to an apogee of 2.8 miles (4.5 km) and a range of 9 miles (14 km). The mission lasted 5 minutes 25 seconds. Maximum speed was 1,780 mph (2865 km/h) and acceleration was 10 g (98 m/s²). The mission was a success and Mercury spacecraft # 14A was recovered.[1]
Mercury spacecraft #14A used in the Little Joe 5B mission, is currently displayed at the Virginia Air and Space Center in Hampton.
See also
References
- ↑ Loyd S. Swenson Jr., James M. Grimwood, Charles C. Alexander (1966). "This New Ocean: A History of Project Mercury - NASA SP-4201". NASA Special Publication-4201 in the NASA History Series. p. 9. Archived from the original on 2009-04-07. Retrieved 26 June 2013.
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