Project Description
This project will entail the design and construction of a rocket capable of atmospheric flight and carrying experimental
system payloads. It will be used to test the flight controller, telelmetry computer, onboard video system, and any
future projects.
Project Goals
Design Vehicle for an active recovery system.
Design Vehicle with a significant payload bay.
Project Specs
6 in diameter
Length will be determined from payload requirements and stability criteria
Project Status 3/3/07
Waiting to secure funding for purchase of vehicle parts.
