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IARE | SAE INTERNATIONAL AERO DESIGN

SAE International Aero Design Challenge - 2025

The Society of Automotive Engineers hosts aero design competitions at both national and international levels. The competition consists of three distinct classes: Advanced, Regular, and Micro. This year, IARE Lakshya Micro participated in the SAE Aero Design West 2025 Micro Class, which took place from April 4 to April 8, 2025, in Van Nuys, California, headed by Dr. BDY Sunil, under the guidance of Dr. Rathan Babu Athota as the technical advisor. The goal of the SAE Aero Design West 2025 competition is to provide undergraduate and graduate engineering students with a realistic design challenge. Industry professionals have developed these regulations with a focus on educational value and practical experience. The rules are structured to simulate a typical aircraft development program over the course of a year, mirroring the initial stages of system engineering and requirements development. This competition will provide participants with insight into conceptual design, manufacturing, system integration and testing, and verification through practical demonstrations.

Design Requirements:

S.No Design Feature Requirement
1 Wing configuration Fixed wing
2 Gross take-off weight <55 lbs
3 Propulsion system Electric propulsion
4 Propulsion system battery Li-Po 4 cell
5 Power limiter (SAE V4 limiter) ≤450 Watts

Mission Requirements:

S.No Mission Feature Requirement
1 Take-off Distance 100 ft
2 Distance from initial start before turn 400ft
3 Landing Distance Limits 200ft
4 Number of take-off attempts Single

About The UAV:

The UAV designed for the SAE Aero Design West 2025 competition is a micro-class model tailored to operate within specified constraints. The design mandates a fixed-wing configuration with a maximum take-off weight under 55 lbs, using an electric propulsion system powered by a 4-cell Li-Po battery and capped at 450 watts through an SAE V4 power limiter. The mission profile is set to 1 minute, requiring the UAV to take off, achieve flight, and land with its payload within this timeframe. The aircraft’s take-off and landing distance requirements are limited to 100 ft and 200 ft, respectively, while the payload discharge must be completed within 60 seconds after take-off. These requirements emphasize the need for a lightweight, highly efficient, and stable design to ensure compliance with power, weight, and distance restrictions.

One of the key challenges for this UAV lies in achieving optimal take-off performance despite its small wingspan, which can impact lift and increase the difficulty of maintaining take-off distances between 0 and 50 ft. This is compounded by the single-motor setup and the strict 450-watt power limit, which restricts the UAV’s power output. To address these challenges, the team has focused on optimizing the UAV’s aerodynamic efficiency and carefully selecting components, including a high-efficiency motor and propeller configuration that maximizes thrust within the power constraints. The resulting design balances compactness and power, aiming to meet the mission objectives and ensure smooth, controlled flight and landing under competitive constraints.

Team IARE LAKSHYA Micro:

S.No Roll No Name
1 22951a2150 CH Steven Raj (Captain)
2 22951a2131 Puneetha Sutram (Vice-Captain)
3 21951a2185 Lingampally Sai Nithin (Pilot)
4 22951a2119 Kirthi Reddy Mule (Design Lead)
5 22951a2114 Ameripalli Gunadeep (Fabrication Lead)
6 22951a2158 Ansh Jaiswal (Technical Lead)
7 22951a2101 Aayuman Amit Kumar (Avionics Lead)
8 22951a2152 Umama Mahroz (Team Manager)
9 23951a2162 Vivek Mahevar
10 23951a2139 Phanindra Pathuri
11 23951a2119 Hisham Mohammed Asim Khan
12 23951a2111 Desaboina Archana
13 23951a2160 Vedanth Akula
14 23951a2102 Abdul Samee

The Team IARE LAKSHYA Micro achieved an overall ranking of 8th at the SAE Aero Design West event, held in Van Nuys, California, USA, 2025.