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Design
Key structural details:
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Carbon Fiber exterior shell - 16 layers printed through carbon 3D printer.
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Liquid rocket fuel in a lighter enclosure - reduces weight up to 2500 pounds.
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Oxidation assembly is reduced because of the overall weight of the rocket by ~ 3.5x.
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Payload increases by up to ~ 4x the initial payload with existing fuel chambers or upto ~2x with reduced fuel needs.
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Carbon + Silicon exterior shell for the payload top to protect from the heat descent (~reduces the overall temperature by 3000 degrees).
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Engines - Light weight engines for increased thrust.
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Reduced water gallon usage by ~15 times for minimal launchpad cooling.
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