Student Work
Design and fabrication of a micro-aerial vehicle
PublicThe goal of the MAV project was to design, fabricate and flight test a fixed-wing aircraft of minimum size which meets the design requirements of the 8th international MAV competition. The MAV's design included a fiberglass cambered plate wing, a foam fuselage and a propulsion system consisting of an electric motor and Lithium Polymer battery. The final weight and size of the MAV was 106 g with a wingspan of 18 cm and a chord length of 19.5 cm.
- This report represents the work of one or more WPI undergraduate students submitted to the faculty as evidence of completion of a degree requirement. WPI routinely publishes these reports on its website without editorial or peer review.
- Creator
- Publisher
- Identifier
- 05D517M
- Advisor
- Year
- 2005
- Date created
- 2005-01-01
- Resource type
- Major
- Rights statement
Relations
- Dans Collection:
Contenu
Permanent link to this page: https://digital.wpi.edu/show/jw827f990