Open Daily 9:00am to 9:00pm by Appointment
website security
Breast Cancer

Customer Breast Cancer Contributions $117
Donated to Dana-Farber Cancer Institute


You have 0 items in your cart

Sub Total: $0.00

Click here to view your cart

Home Page Current Specials My Account Cart Contents Checkout
Categories
Adhesives & Foam (5)
Components (196)
Electronics (12)
Model Rocket Kits (62)
Recovery (136)
Rocket Motor Hardware (244)
Rocket Motors (645)
Igniters & E-Matches (11)
Gift Certificates (5)

Jump to Category:
Search Website
 
Use keywords to find products.
Advanced Search
Manufacturers
Information
About Us
Ordering Procedures
Current Specials
Certification Support
98mm and Larger Motors
Launch Schedule
Launch Site Weather Forecast
Resources
Links
Privacy Notice
Contact Us
Resources

Basics:

Model Rocket Basics

Calculators:

 

Documents:

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
Continue
Copyright © 2017, Off We Go Rocketry, LLC. All Rights Reserved.         Web site hosting and maintenance provided by iPage.