American test vehicle. Single stage vehicle consisting of 6 x Algol 1D motors.
Failures: 1. First Fail Date: 1965-05-19. Last Fail Date: 1965-05-19.
Gross mass: 80,300 kg (177,000 lb).
More... - Chronology...
Height: 26.20 m (85.90 ft).
Diameter: 3.96 m (12.99 ft).
Thrust: 3,276.00 kN (736,474 lbf).
Apogee: 35 km (21 mi).
First Launch: 1965.05.19.
Number: 1 .
Little Joe II Little Joe II was an enlarged version of the Little Joe concept used in the Mercury program, used to test the Apollo capsule launch escape system. The vehicle was designed by General Dynamics. Six to nine solid rocket motors were mounted in an aerodynamic finned fairing. More...
Associated Manufacturers and Agencies
Convair American manufacturer of rockets, spacecraft, and rocket engines. Convair, USA. More...
Associated Launch Sites
White Sands White Sands Missile Range occupies an area 160 x 65 km in the Tularosa Basin of southern New Mexico, across the Sacramento Mountain range from Roswell. In the 1930's, Robert Goddard, after surveying weather conditions and population densities, had selected Roswell for his pioneering rocket tests. White Sands, a true desert area, was even more unpopulated than Roswell. German advances in rocketry during World War II impelled the US Army to begin programs to exploit this technology. The White Sands Proving Ground was established for testing German and American long-range rockets on 9 July 1945. Seven days later the first atomic bomb was exploded at Trinity Site, near the north boundary of the range. The first launch of a Tiny Tim rocket was on 26 September 1945. On 11 October a Tiny Tim boosted a WAC Corporal rocket from the tower. This was the first use of Launch Complex 33, later to be used for V-2, Nike, Viking, Corporal, Lance and Multiple Launch Rocket System testing. More...
White Sands LC36 Terrier, Redstone, Nike, Little Joe II, Honest John, Black Brant, Storm, Aries, Apollo LES launch complex. Originally designated Army Launch Area 2, LC36 was later a LC36 was a NASA facility that supported tests of the Apollo Launch Escape System. It was also used to launch NASA sounding rocket missions. The complex included a blockhouse, launch control equipment, and launchers with environmental shelters. These launchers included:
- An 11-m rail with 3600 kg capacity
- A 15-m rail with 11,000 kg capacity
- A 50-m tower with 3600 kg capacity
- A 1.2-m diameter stool with 23,000 kg capacity
- A 9-m rail with 7000 kg capacity.
Algol 1D Solid rocket stage. 440.00 kN (98,916 lbf) thrust. Mass 10,700 kg (23,589 lb). More...
Little Joe II 0-3-3 Chronology
1965 May 19 -
13:01 GMT - .
: White Sands
. Launch Complex
: White Sands LC36
. LV Family
: Little Joe II
. Launch Vehicle
: Little Joe II 0-3-3
. LV Configuration
: Little Joe II-0-3-3 LJII-4 (12-51-2). FAILURE
- Apollo A-003 - .
Nation: USA. Agency: NASA. Apogee: 6.00 km (3.70 mi).
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