System for multiple burns from a rocket motor
A system for multiple burns from a solid fuel rocket motor may extinguish rocket fuel after the rocket has been ignited. The motor may be extinguished via rapid decompression of the combustion chamber. The fuel may then be reignited by a suitable igniter, and the process of extinguishing and reigniting may be repeated, enabling multi-burn maneuvers. A decompressive extinguishing plug nozzle may extinguish solid rocket fuel after the rocket has been ignited and/or keep a rocket in a disarmed (zero thrust) state until the rocket is to be armed. The nozzle may include a plug that mostly impedes the opening of the nozzle and an outer cowl that is movable to rapidly decompress the combustion chamber. This rapid decompression extinguishes the solid rocket fuel. In some aspects, the fuel can be reignited and extinguished multiple times.
1. A decompressive extinguishing plug nozzle, comprising:
an outer cowl, wherein shelves formed in the outer cowl define a track along which a wheel bearing is configured to traverse;
a plug;
a plug housing that houses the plug;
a plug seal, wherein the plug housing is connected to the plug via the plug seal, and wherein the plug seal is configured to seal against an inside of a rocket body downstream from a combustion chamber; and
a mechanically variable throat at least partially defined by the outer cowl and the plug, wherein traversal of the wheel bearing along the track is configured to cause movement of the outer cowl relative to the plug thereby transitioning the decompressive extinguishing plug nozzle from a sealed configuration to an active configuration, wherein the mechanically variable throat defines a choked sonic flowpath in the active configuration.
2. The decompressive extinguishing plug nozzle of claim 1 , wherein the decompressive extinguishing plug nozzle is configured to transition from the sealed configuration to the active configuration to a decompressive configuration, and then back to the sealed configuration.
3. The decompressive extinguishing plug nozzle of claim 1 , wherein the plug seal comprises passages that allow exhaust to flow around the plug through the plug housing and a plug ring, and then out of a nozzle defined by the plug ring.
4. The decompressive extinguishing plug nozzle of claim 1 , wherein
the plug housing comprises a first lip,
the outer cowl or a cowl housing comprises a second lip, and
the first lip and the second lip are configured to limit a range of motion of the outer cowl as the decompressive extinguishing plug nozzle transitions from the active configuration to a decompressive configuration.
5. The decompressive extinguishing plug nozzle of claim 1 , further comprising:
a rod operably coupled to the plug seal.
6. The decompressive extinguishing plug nozzle of claim 1 , further comprising:
a plug ring defining a nozzle and located within the outer cowl, wherein the plug ring is at least partially within the outer cowl.
7. The decompressive extinguishing plug nozzle of claim 1 , further comprising:
one or more springs configured to bias the decompressive extinguishing plug nozzle into the sealed configuration in response to insufficient gas pressure in the combustion chamber of a rocket to move the decompressive extinguishing plug nozzle into the active configuration.
8. The decompressive extinguishing plug nozzle of claim 1 , further comprising:
one or more vents, wherein when closed, the one or more vents bias the decompressive extinguishing plug nozzle into the sealed configuration, and when open, the one or more vents bias the decompressive extinguishing plug nozzle into the active configuration.
9. The decompressive extinguishing plug nozzle of claim 1 , further comprising:
one or more movement mechanisms configured to facilitate movement between the active configuration and a decompressive configuration by moving the outer cowl to increase an area of the mechanically variable throat.
10. The decompressive extinguishing plug nozzle of claim 1 , further comprising:
a cowl housing configured to receive the outer cowl.
11. A decompressive extinguishing plug nozzle, comprising:
an outer cowl, wherein shelves formed in the outer cowl define a track along which a wheel bearing is configured to traverse;
a plug;
a plug housing that houses the plug;
a plug seal; and
a mechanically variable throat at least partially defined by the outer cowl and the plug, wherein traversal of the wheel bearing along the track is configured to cause movement of the outer cowl relative to the plug thereby transitioning the decompressive extinguishing plug nozzle from a sealed configuration to an active configuration, wherein the mechanically variable throat defines a choked sonic flowpath in the active configuration, and wherein the plug seal is configured to seal against an inside of a rocket body downstream from a combustion chamber.
12. The decompressive extinguishing plug nozzle of claim 11 , wherein
the plug housing is connected to the plug via the plug seal,
the plug housing comprises a first lip,
the outer cowl or a cowl housing comprises a second lip, and
the first lip and the second lip are configured to limit a range of motion of the outer cowl as the decompressive extinguishing plug nozzle transitions from the active configuration to a decompressive configuration.
13. The decompressive extinguishing plug nozzle of claim 11 , wherein the decompressive extinguishing plug nozzle is configured to transition from the sealed configuration to the active configuration to a decompressive configuration, and then back to the sealed configuration.
14. The decompressive extinguishing plug nozzle of claim 11 , wherein the plug seal comprises passages that allow exhaust to flow around the plug through the plug housing and a plug ring, and then out of a nozzle defined by the plug ring.
15. The decompressive extinguishing plug nozzle of claim 11 , further comprising:
a rod operably coupled to the plug seal.
16. The decompressive extinguishing plug nozzle of claim 11 , further comprising:
one or more springs configured to bias the decompressive extinguishing plug nozzle into the sealed configuration in response to insufficient gas pressure in the combustion chamber of a rocket to move the decompressive extinguishing plug nozzle into the active configuration;
one or more vents, wherein when closed, the one or more vents bias the decompressive extinguishing plug nozzle into the sealed configuration, and when open, the one or more vents bias the decompressive extinguishing plug nozzle into the active configuration; or
one or more movement mechanisms configured to facilitate movement between the active configuration and a decompressive configuration by moving the outer cowl to increase an area of the mechanically variable throat.
17. A decompressive extinguishing plug nozzle, comprising:
an outer cowl, wherein shelves formed in the outer cowl define a track along which a wheel bearing is configured to traverse;
a plug;
a plug housing that houses the plug;
a plug seal, wherein the plug housing is connected to the plug via the plug seal, and wherein the plug seal is configured to seal against an inside of a rocket body downstream from a combustion chamber, and
a mechanically variable throat at least partially defined by the outer cowl and the plug, wherein traversal of the wheel bearing along the track is configured to cause movement of the outer cowl relative to the plug thereby transitioning the decompressive extinguishing plug nozzle from an active configuration to a decompressive configuration, wherein the mechanically variable throat defines a choked sonic flowpath in the active configuration, and wherein the mechanically variable throat is also defined in part by the plug housing.
18. The decompressive extinguishing plug nozzle of claim 17 , wherein
the plug housing comprises a first lip,
the outer cowl or a cowl housing comprises a second lip, and
the first lip and the second lip are configured to limit a range of motion of the outer cowl as the decompressive extinguishing plug nozzle transitions from the active configuration to the decompressive configuration.