Hybrid composites for oxygen propulsion systems
AssigneeLockheed Martin Corporation
InventorsElizabeth P. Kirn, Neil Anthony Graf, Kevin Wilbur Ely
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AssigneeLockheed Martin Corporation
InventorsElizabeth P. Kirn, Neil Anthony Graf, Kevin Wilbur Ely
Estimating the term…
The development of polymer composite liquid oxygen (LOX) tanks is a critical step in creating the next generation of launch vehicles. A composite LOX tank will weigh significantly less than conventional metal tanks. This benefit of reduced weight is critical to enable future launch vehicles to meet required mass ractions. The high strength and low weight of a composite tank allows for a lighter weight craft and/or higher payload capacity which results in lower costs per pound to place an object in orbit. The unique, nontraditional idea described here is to use resin-based composite materials to make such a composite tank or other oxygen carrying component such as a feedline. Polymer composites have traditionally been regarded as being more flammable than metals and therefore deemed not oxygen compatible. However, a hybrid composite material may provide the optimal balance of oxygen compatibility and mechanical performance that would make composite oxygen tanks feasible.
A liquid oxygen tank apparatus comprising:
A method of using a composite tank to hold liquid oxygen, comprising:
Apparatus for holding liquid oxygen comprising:
Apparatus for transporting liquid oxygen comprising:
A launch vehicle comprising:
A liquid oxygen tank apparatus comprising:
A method of using a composite tank to hold liquid oxygen, comprising:
Apparatus for transporting liquid oxygen comprising:
Apparatus for holding liquid oxygen comprising:
A launch vehicle comprising:
Dependencies are inferred from the claim text.