Mercury LJ-1

Launch & landing data:

Mission:

Mission details:

• 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.
  
  

  The Little Joe rocket left behind after the accidental activation of the launch escape system during the countdown for LJ-1. (NASA/LRC)

  
  
• At 35 minutes before launch, evacuation of the area had been proceeding on schedule and the batteries for the programmer and destruct system in the test booster were being charged. Suddenly, half an hour before launchtime, an explosive flash occured. When the smoke cleared it was evident that only the capsule-and-tower combination had been launched, on a trajectory similar to an off-the-pad abort. The booster and adapter-clamp ring remained intact on the launcher. Near apogee, at about 2000 ft, the clamping ring that held tower to capsule released and the little pyro-rocket for jettisoning the tower fired. The spacecraft 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 The fault was found in a coil designed to protect biological specimens from too rapid an abort. (Reference SP-4201 p. 208)

Mission Highlights: