A favorite experience for us has been a science project inspired by Meisha.
My son entered a regional science competition, selecting engineering. The specific category was rocketry. The objective was to reengineer an Estes Alpha rocket.
I advised I would assist him, however that he would have to take ownership of the project, make the decisions and do the work.
Project Name: Too Fast
Recognitions:
Event Award: First Place in Class
Event Award: Overall Event Recognition
Special Recognition: Parrot exposure to the local junior science community; management and members.
Special Recognition (unconfirmed): Fastest cockatoo feather flight.
Special Recognition (unconfirmed): First rocket constructed using keratin based biomass.
Flock Designation Identification: Insignia located on the vertical tail fin and as nose art.
Credits:
Concept / Design / Engineering: Junior Engineer
Design Consultant: Meisha
Product Development / Manufacturing / Troubleshooting: Junior Engineer
OEM / Original Equipment Manufacturers: Estes / Meisha
Project Quartermaster (supplies, tools, transportation, progress historical record): WhiteFlight
Engineering Achievements: Skippable Technobabble
Wing Design: Swept Elliptical Tapered Hybrid
Resembling a static version of the variable cockatoo wing design.
Wing Structure, Each: Tapered leading edge frame with twenty-four flight feathers, each unique. Open areas at the feather calamus (quill) to leading edge joints have been closed off using modified flight feathers sectioned to fit, stabilizing airflow over the wing.
Two Descent Recovery Systems:
Low Wind / Parachute Assist Descent: Requires engine selection, parachute deployment charge.
High Wind / Tumble Return Descent: Requires engine selection, parachute deployment charge DELETE.
Wing to Fuselage Construction / Wing-Box: Special engineering considerations were applied to achieve structural integrity combined with design function for the parachute assist descent system. A closed wing-box would have prevented parachute deployment. An open framed style wing-box was custom fabricated from an Estes engine block. The design secured the wing assembly to the fuselage with allowance for the parachute deployment charge to pass from the engine through the wing-box to the upper fuselage section housing the parachute assembly and nosecone.
Stability Test Results: PASSED
Wing positioning with overall weight considerations achieved by the project engineer.
Entry Classification: Official