Little Joe 1
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| Mission Insignia | |
|---|---|
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| Mission Statistics | |
| Mission Name: | Little Joe 1 |
| Call Sign: | LJ-1 |
| Number of Crew Members: | 0 |
| Launch: | August 21, 1959 Wallops Island |
| Landing: | August 21, 1959 |
| Duration: | 0 min 20 s |
| Number of Orbits: | suborbital |
| Apogee: | 0.4 mi - 0.6 km |
| Distance Traveled: | 0.5 mi - 0.8 km |
| Maximum velocity: | ~975 mph 1.569 km/h |
| Peak acceleration: | ? g |
| Mass: | 1,007 kg |
| LJ-1 | |
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The Little Joe 1 was a solid fuel rocket that was designed to test the Mercury spacecraft Launch Escape and Recovery systems. It was 48 feet (14.6 m) in height, weighed (at maximum) 41,330 pounds (18,747 kg), was 6.66 feet (2 m) in diameter, consisted of four Pollux and four Recruit clustered, solid-fuel rockets, could develop a thrust of 250,000 lbf (1,112 kN), and could lift a maximum payload of 3,942 pounds (1,788 kg).
The Little Joe 1 was being prepared for launch from the Wallops Flight Facility, Wallops Island, Virginia, on August 21, 1959. Suddenly, about a half hour before the scheduled launch, the escape rocket fired and pulled the Mercury spacecraft away from the launch pad.The spacecraft reached an apogee of 2000 feet (600 m) and landed about 2000 feet (600 m) away. The unexpected triggering of the Launch Escape System was caused by a transient or stray electrical current. Flight time 20 seconds. Payload 1,007 kg.
External links
- This New Ocean: A History of Project Mercury - NASA SP-4201 (http://www.hq.nasa.gov/office/pao/History/SP-4201/cover.htm)
- NASA NSSDC Master Catalog (http://nssdc.gsfc.nasa.gov/nmc/sc-query.html)
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