Utility Cargo Aircraft (Conceptual Design)
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The senior level design project for Aircraft Design was an intriguing challenge. For a complete breakdown of the design and performance analysis, please feel free to reach out. Key specifications of this aircraft include seating for two crew members (pilot and copilot), a total cabin volume excluding cockpit of 10 cubic meters, a cabin height of 1.46 meters, a cabin floor width of 1.52 meters, and a cargo door opening of 135x135 cm. The aircraft has a payload capacity of 1580 kg and requires a take-off distance of 690 meters on an unpaved runway under maximum weight and at 30°C standard level (+30°C). Upon landing, it needs 548 meters on the same type of runway. The aircraft's range with maximum payload and IFR reserve is 2700 km. It can cruise at a best range speed of 550 km/h at a standard altitude of 6 km. Its service ceiling is 9,000 meters, and it has a rate-of-climb of 1,700 feet per minute under maximum weight and at 30°C standard level (+30°C).
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