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Investor Presentaiton

Advantages of AM Improving functionality Traditional Manufacturing 1. Time consuming and cost intensive process to produce 2.Increased risk of human error due to requirement of multiple parts for single component. Monolithic Thrust Chamber Core element of a liquid- propellant rocket engine. Measurements: 228X194X310mm 3.Essential cooling structure manufactured separately Material: IN718 (Nickel Superalloy) Machine: SLMⓇ 280 Bedro Co Demo Owigon plan Source: SLM; NASA; G. P. Sutton, History of Liquid Propellant Rocket Engines, AIAA, Reston, VA, 2006. Additive Manufacturing 1. Production time decreased from ~6 months to <5 days 2.Entire component printed, without needing multiple parts - significantly improving reliability. 3.Innovative lattice structure enabling an integrated cooling function which also resulted in increased stability. SLM SOLUTIONS 41
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