Browsing Aerospace Engineering (AE) by Subject "75 mm Fixed-Wing Nano Air Vehicle Design"
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Design and Development of 75 mm Fixed-Wing Nano Air Vehicle
(2018-06-11)This thesis deals with the design and development of a 75 mm fixed-wing nano-air vehicle (NAV). The NAV is designed to fit inside a cube with each side measuring 75 mm. The range and endurance of the NAV are 300 m and 2-3 ...