Search U.S. government technical reports digitized or harvested by TRAIL.

Keyword Search

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)

• About TRAIL
• FAQ
• Join TRAIL
• Contact Us

Search developed and maintained by the University of Washington Libraries
Copyright 2010