A RISK FREE APPROACHING FOR PAYLOAD LAYOUT

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A RISK-FREE DESIGN APPROACH solution for Payload layout • To minimize ( or nearly eliminate ) Catastrophic fire risk with removing mechanism With that design there will not be any mechanisms and movable and/or frictioning parts for that reason we can eliminate the risk of spark and breaking a fire which is extremely important for station crew safety. • To eliminate any stuck problem and elimination any supply risk • -Easy accessibility due to highly easy accessibility • -Reduce ( or nearly eliminate ) void risk which could be caused by thermal strength cracks • -Reduce or elimination thermal stresses ( or cracks which could be emerged from thermal stress) OTHER BENEFITS ENGINEERING POINT OF VIEW - High effectives for having lightweight-ratio - Highly simple manufacturing process - Highly controllable manufacturing process - Note: If it would be any other thermal manufacturing process such as welding structures to the cylinder then we would need to have Ultrasonic crack tests to be sure there is no any crack or void which could be a real issue in space environment ( it would still too difficult to see some cracks underneath of surface) - Minimum material usedIndirectly less -fuel consumption during launch due to less -weight in comparison with other designs