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US 2014/0109551 A1Published application
Solid chemical rocket propulsion system
AssigneeLos Alamos National Security, LLC
InventorsBryce C. Tappan, Grant A. Risha
Life of this patent
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Abstract
A solid chemical rocket propulsion system includes a solid fuel and a solid oxidizer that is physically separated from the solid fuel and is not mixed with solid fuel while the rocket is initially at rest.
Claims8
A rocket propulsion system comprising:
- a solid energetic fuel, and
- a solid oxidizer,
- wherein said solid energetic fuel is physically separated from the solid oxidizer and is not mixed with the solid oxidizer while the rocket is initially at rest.
Dependencies are inferred from the claim text.