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- Q1811537 subject Q7142277.
- Q1811537 subject Q8807208.
- Q1811537 abstract "Little Joe 1 (LJ-1) was a failed launch of a Little Joe solid fuel rocket that was designed to test the Mercury spacecraft Launch Escape and Recovery systems. The vehicle was 48 ft (15 m) in height, weighed approximately 43,000 lb (20,000 kg), and was 80 in (2.0 m) in diameter with a fin span of 21.3 ft (6.5 m). The Little Joe booster consisted of four Pollux and four Recruit clustered, solid-fuel rockets, could develop a thrust of 250,000 lbf (1,100 kN), and could lift a maximum payload of 3,942 lb (1,788 kg). The escape system, using a Grand Central 1KS52000 rocket motor, weighed 1,015 lb (460 kg).On August 21, 1959, LJ-1 was being prepared for launch from the Wallops Flight Facility, Wallops Island, Virginia. 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 2,000 ft (610 m) and landed about 2000 feet away. The flight time was 20 seconds.According to the Sept. 18, 1959 accident report, the unexpected triggering of the launch escape system was caused by a transient or electrical leak; analysis showed it to be due to the rapid-abort system being wired directly into the destruct arming busbar. The batteries were shipped from England to the U.S. uncharged and shorted; on charging at the pad, the batteries, when enough charge was reached, actuated the sequencer for the abort system, and sensing insufficient altitude, fired the squibs in the abort motor. Insufficient power in the batteries then failed to initiate the tower jettison motor and capsule parachute recovery charge, and both crashed into the sea.".
- Q1811537 thumbnail Little_Joe_on_launcher_at_Wallops_Island_-_GPN-2000-001883.jpg?width=300.
- Q1811537 wikiPageExternalLink sc-query.html.
- Q1811537 wikiPageExternalLink cover.htm.
- Q1811537 wikiPageWikiLink Q1030817.
- Q1811537 wikiPageWikiLink Q1322791.
- Q1811537 wikiPageWikiLink Q1370.
- Q1811537 wikiPageWikiLink Q182348.
- Q1811537 wikiPageWikiLink Q2110026.
- Q1811537 wikiPageWikiLink Q23548.
- Q1811537 wikiPageWikiLink Q2417557.
- Q1811537 wikiPageWikiLink Q41291.
- Q1811537 wikiPageWikiLink Q52162.
- Q1811537 wikiPageWikiLink Q533668.
- Q1811537 wikiPageWikiLink Q675129.
- Q1811537 wikiPageWikiLink Q7142277.
- Q1811537 wikiPageWikiLink Q750141.
- Q1811537 wikiPageWikiLink Q7641034.
- Q1811537 wikiPageWikiLink Q83481.
- Q1811537 wikiPageWikiLink Q8807208.
- Q1811537 wikiPageWikiLink Q907773.
- Q1811537 type Place.
- Q1811537 type ArtificialSatellite.
- Q1811537 type CelestialBody.
- Q1811537 type Location.
- Q1811537 type Place.
- Q1811537 type Satellite.
- Q1811537 type Thing.
- Q1811537 comment "Little Joe 1 (LJ-1) was a failed launch of a Little Joe solid fuel rocket that was designed to test the Mercury spacecraft Launch Escape and Recovery systems. The vehicle was 48 ft (15 m) in height, weighed approximately 43,000 lb (20,000 kg), and was 80 in (2.0 m) in diameter with a fin span of 21.3 ft (6.5 m).".
- Q1811537 label "Little Joe 1".
- Q1811537 depiction Little_Joe_on_launcher_at_Wallops_Island_-_GPN-2000-001883.jpg.