Design Specifications

Details coming soon...

SolidWorks Model of Daedalus III

Internal Component Assembly of Daedalus III

Daedalus II

The second in the series of Daedalus rockets was successfully launched in January 2006 in Argonia, Kansas.  Reaching an altitude of nearly 30,000 feet, this solid-fueled rocket served to verify our mathematical and modeling methods and test various electronics and communication systems. Originally designed as a booster for the Daedalus III, the rocket acted mainly as launch training for future rockets.

Click here to view more information on the Daedalus II rocket