Nike-Cajun

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25. Nike-Cajun ready for launch.

26. Nike-Cajun launch.

The Nike-Cajun was used extensively during International Geophysical Year (1957-58) to perform a variety of research tasks. These included weather photography, studies of water-vapor distribution in the upper atmosphere, and magnetic soundings in the ionosphere.

For photographic studies, the instrument package separated from the nose cone at about 80 kilometers (50 miles) and then coasted to a peak altitude of about 120 kilometers (75 miles), during which time data was collected. Then parachutes opened, lowering the cameras for recovery. Other data was radioed to Earth.

The Cajun rocket was developed by the Pilotless Aircraft Division of the National Advisory Committee for Aeronautics and the University of Michigan. The solid-fuel engine was designed and manufactured by Thiokol Chemical Company. The Nike booster was also solid fuel.


The rocket on exhibit is from the National Aeronautics and Space Administration.

Length 7.9 m. (26 ft.); Cajun, 4.1 m. (13.5 ft.)
Diameter 41.9 cm. (16.5 in.) max; Cajun, 17.1 cm. (6.75 in.)
Propellant Solid
Thrust Sustainer, 4364 kg. (9620 lb.)
Velocity 6760 km/ hr. (4200 mi/hr.)
Altitude 161 km. (100 mi.) with a 23 kg. (50 lb.) instrument package; higher with a lighter payload
                                                                                                                                                                                                                                                                                                           

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