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This concept will be the future of travel! . Now it is up to Google and Apple to "improve" (steal) their designs. Martin Aircraft Company's V4 engine was developed from
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This concept will be the future of travel!.
Now it is up to Google and Apple to "improve" (steal) their designs. ![]() Martin Aircraft Company's V4 engine was developed from the ground up as an aircraft engine to power the Martin Jetpack. After searching the world for a suitable engine, and coming up short, Martin Aircraft assembled a team of experienced engine designers and experts from around the globe. The engine has several key features: High power to weight High reliability Flat torque curve Current Engine Specification : Type : V4 two stroke Displacement : 2.0 litre (122 cu in) Bore : 89 mm (3.50 in) Stroke : 79 mm (3.11 in) Nominal Performance : 200 hp @ 6000 rpm Torque : 180 ftlbs 3500-6000 rpm Features : Sequential fuel injection, Dual CDI ignition Generator : 420W, 12V Weight : 132 lbs (60 kg) Dimensions : (LxWxH) 0.45x0.5x0.3 (metres - without accessories) The Martin Jetpack composite airframe has been developed using the latest composite technologies. The use of composite materials is essential to meet the unique demands of the Martin Jetpack. Each component or assembly has been engineered to be lightweight, strong and rigid. The composite structures, designed and developed in conjunction with Dynamic Composites, account for less than 30% of dry machine weight. Key manufacturing processes : Prepreg Resin infusion (V.I.P) Vacuum bagging Rapid manufacture tooling Current Composite Airframe Specifications : Ducts : Carbon fibre, aramid fibre, honeycomb core, epoxy resin Fans : Epoxy prepreg carbon fibre, aramid fibre, foam core Main Beam : High modulus carbon fibre, foam core Spine : Epoxy prepreg carbon fibre Fuel tank : Carbon fibre, Kevlar, fuel resistant epoxy resin Undercarriage : Carbon fibre, epoxy resin, aluminium alloy Engine heads : Carbon fibre, high temp flame resistant vinylester resin Airboxes : Carbon fibre, epoxy resin Last edited by USAFControl; 02-17-2015 at 07:51 PM. |
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