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Model Rocket Basics




Nose Cone & Fin Optimization
Recovery Systems
Rocket Design
Staging & Air Starting

Technical Papers:

Fin Research:

ATL-TR-846 - Roll Damping for Finned Projectiles Including: Wraparound, Offset, and Arbitrary Number of Fins
NACA RM A6G24 - The Subsonic Aerodynamic Characteristics of Two Double-Wedge Airfoil Sections Suitable for Supersonic Flight
NACA RM L7A08 - Effect of Number of Fins on the Drag of a Pointed Body of Revolution at Low Supersonic Velocities
NACA RM L8F08 - Transonic Drag Characteristics of a Wing-Body Combination Showing the Effect of a Large Wing Fillet
NACA RM L53K12 - A Summary of Information on Support Interference at Transonic and Supersonic Speeds
NACA TN 4197 - Summary of Flutter Experiences as a Guide to the Preliminary Design of Lifting Surfaces on Missiles
NACA TR 460 - The Characteristics of 78 Related Airfoil Sections from Tests in the Variable-Density Wind Tunnel
NASA TN D-3182 - Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges
NASA TP 2433 - Experimental and Theoretical Study of the Longitudinal Aerodynamic Characteristics of Delta and Double-Delta Wings at Mach Numbers of 1.60, 1.90, and 2.16
NASA TR R-202 - Theoretical Aerodynamic Characteristics of Sharp and Circularly Blunt-Wedge Airfoils
NAVORD Report 6025 - Effect of Fin Cant and Nose Shapes on Free Spin of Basic Finner
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