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Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance

Aerodynamic Heating and Boundary-Layer Transition on a 1/10-Power Nose Shape in Free Flight at Mach Numbers Up to 6.7 and Free-Stream Reynolds Numbers Up To 16 x 10(Exp 6)

Measurements of Heat Transfer and Boundary-Layer Transition on an 8-Inch-Diameter Hemisphere-Cylinder in Free Flight for a Mach Number Range of 2.00 to 3.88

Published Year

• 1950-1959 (3)

Subject

• Charts, diagrams, etc (1)
• Rockets (Aeronautics)--Performance (1)
• Rockets (Aeronautics)--Testing (1)
• Solid propellant rockets (1)
• Sounding rockets (1)

Author

• Garland, Benjamine J. (3) *
• Royall, John F. (1)
• Swanson, Andrew G. (1)

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