A Review on Vertical Take-Off and Landing (VTOL) Tilt-Rotor and Tilt Wing Unmanned Aerial Vehicles (UAVs)

<table class="table-group" id="tab7"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Length</td><td class="align_center">15.2 m</td><td class="align_center">Width</td><td class="align_center">13.4 m</td></tr><tr><td class="align_left">Max weight</td><td class="align_center">5450 kg</td><td class="align_center">Time in service</td><td class="align_center">—</td></tr><tr><td class="align_left">Engine</td><td class="align_center">4000 HP</td><td class="align_center">Max. speed</td><td class="align_center">741 km/h</td></tr><tr><td class="align_left">Manufacturer</td><td class="align_center">DRPA</td><td class="align_center">Development nation</td><td class="align_center">USA</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div><i>X</i>-PLANE performance and data [<a href="/journals/je/2022/1803638/#B35" target="_blank">35</a>].</div>

Journal of Engineering

tab7

Table 7

Table 7: A Review on Vertical Take-Off and Landing (VTOL) Tilt-Rotor and Tilt Wing Unmanned Aerial Vehicles (UAVs) 