Expendable Multistage Pressure-Fed Ablative-Cooling Nontoxic Non-Heavy Launch Vehicle

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20240409240A1
SERIAL NO

18390538

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Abstract

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An expendable launch vehicle is provided using pressure-fed liquid propellant fixed steering ablatively-cooled rocket engines. The vehicle is manufactured minimizing toxic or exotic metals and maximizing the use of conventional, inexpensive composites and 3D printed parts. Fuselage, fairing, stage shells, adapters, propellant tanks, and even engine combustion chambers are unified for all stages, are ablatively cooled, and, like the fairing, integral propellant tanks and adapters, are made of composites or 3D printed parts. Using non-toxic materials with non-toxic by-products, and non-toxic fabrication methods, using mostly non-metallic components allows for an environmentally neutral design.

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Patent Owner(s)

Patent OwnerAddress
TARDIGRADE SPACE SYSTEMS LLC11 EDMOND ROAD NEWTOWN CT 06470

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
CARPENTER, Michael L Cleveland Heights, US 3 73
FAKAS, Sergii Kharkiv, UA 1 0
GRECHUKHIN, Mykhailo Kyiv, UA 1 0
PARNOWSKI, Aleksei Kyiv, UA 1 0

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