The main purpose of this project is to minimize the loss of life in times of catastrophic failure of the hydraulic system or case of failure of engines. A new design concept that has the potential to save the lives of a thousand passengers in the event of an air crash. The notion involves the redesigning of a plane with the detachable wings that would eject during the emergency to touch down on land or water safety. It is the method of detaching the wings from an aircraft which is in the state of an unrecoverable stall, which could add up to damage in time of catastrophe.
In this project, we are going to fabricate an aircraft with detachable wings and the Orion parachute system (3 parachutes). Later creating a 3D model of an aircraft and run analysis over the model and obtain the results. At last a field test is conducted based on flight data requirements.
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Step 1: Conceptual design is considered.
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Step 2: The Prototype is fabricated based on the requirements.
Step 3: 3D modeling is done using design software.
Step 4: Field Test is carried out.
Step 5: Plot the flight characteristics.
The design process detailed by this report began with an examination of the project objective. This project is to build a scaled-down prototype of Boeing 737-200 capable of wing detachability at the time of catastrophic failure.
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