left-click = rotate, middle-button/CTLR-left-click = pan, scroll/right-click/ALT-left-click = zoom
|Manufacuter||ITA - Institute of Aeronautical Technology|
|Description||Flying wing was designed and build by ITA students for SAE Brasil AeroDesign Competition 2016, advanced Class. It has MTOW of 24 kg at 60 meters of takeoff runway, 5 minutes of flight autonomy using electric propulsion from Schubeler DS-51-DIA HST Edf Engine with 15S MaxAmps LiFePo4 batteries. Video: https://www.youtube.com/watch?v=8T3ytnXpro8 We use OpenVSP to predict Structural Inertia, CoG and empty weight for our Optimization algorithm. We Designed internal structures using Conformal elements, this model don't have it.|
1 - The source material used to create this model was Definitive. This means the VSP model is the definition of the vehicle or part (it was built from the model or the model is the best source of infromation available).