Shroud driven deployable flight surfaces and method
AssigneeRaytheon Company
InventorsPaul A. Merems, Shane Olsen
Life of this patent
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AssigneeRaytheon Company
InventorsPaul A. Merems, Shane Olsen
Estimating the term…
A nose or tail assembly for a flight vehicle is provided in which the deployment of the canards or fins is driven by energy imparted by the shroud when it is released. A tip section is rotatably coupled to a base, and both are stowed in a volume between the shroud and nose/tail assembly. As the shroud is released, a drive feature engages the tip section to rotate and join the base to form a complete canard or fin. This eliminates the need for storing the canards or fins in or wrapped around the body and eliminates the need for a complex deployment mechanism occupying an internal volume of the body. Although viable for all sizes of flight vehicles, the shroud-driven deployment system scales to very small diameter vehicles in which internal volume is not available to store either flight surfaces or deployment mechanisms.
A flight vehicle, comprising:
A nose assembly for a flight vehicle, comprising:
A method of deploying a flight surface on a flight vehicle, said flight vehicle including a body, a tapered section positioned fore or aft of the body, and a shroud including a plurality of detachable segments that define an external volume between the tapered section and the shroud, the method comprising:
Dependencies are inferred from the claim text.