Ring-shaped booster rocket

Patent metadata

Field	Value
Publication number	US-11732677-B2
Application number	US-202117181162-A
Country	US
Kind code	B2
Filing date	Feb 22, 2021
Priority date	Feb 22, 2021
Publication date	Aug 22, 2023
Grant date	Aug 22, 2023

Abstract

A rocket booster has an annular shape, with a casing defining an annular space therewithin, and a solid rocket fuel in the annular spacing. The rocket booster also includes one or more nozzle pieces, mechanically coupled to the casing, that define one or more nozzles at the aft side of the rocket booster. The rocket booster may be mechanically coupled to an object protruding from the back of a fuselage of a flight vehicle, such as a missile. For example, the rocket booster may be placed around an aft turbojet nozzle of the flight vehicle. This allows the rocket booster to be used in situations where primary propulsion must be running both before and after (and perhaps during) the firing of the rocket booster.

First claim

What is claimed is:

1. A booster rocket comprising:
an annular casing defining an annular space therewithin, and having a central opening, wherein the annular casing includes an inner part and an outer part, wherein the inner part includes an annular slot extending along an outer surface of the inner part;
a solid rocket fuel in the annular space; and
one or more nozzle pieces mechanically coupled to the annular casing, defining one or more nozzles at an aft end of the annular casing;
wherein the one or more nozzle pieces includes an annular nozzle piece that defines an annular nozzle between the annular nozzle piece and the annular slot;
wherein the booster rocket is a capable of being placed around and installed around a separate object;
wherein the annular nozzle piece has an inwardly sloped section that directs flow inwardly as the flow approaches the annular nozzle; and
wherein the annular casing includes an inwardly-angled aft section aft of the annular nozzle.

2. The booster rocket of claim 1 , further comprising a seal between the annular nozzle piece and the annular casing.

3. The booster rocket of claim 1 , wherein the annular nozzle piece defines the annular nozzle in combination with an inner nozzle insert that is attached to the annular slot in the annular casing.

4. The booster rocket of claim 3 , wherein the annular nozzle piece and the inner nozzle insert together constitute a throat insert set.

5. The booster rocket of claim 1 , wherein the annular nozzle piece has protrusions protruding inward from an inner edge at the aft end of the one or more annular nozzle pieces, the protrusions facilitating maintaining an annular gap of the annular nozzle.

6. The booster rocket of claim 1 , wherein the annular nozzle piece is made of a metallic material.

7. The booster rocket of claim 1 , wherein the annular nozzle piece is made of a non-metallic material.

8. The booster rocket of claim 1 , wherein the annular nozzle piece is made of a phenolic material.

9. The booster rocket of claim 1 , further comprising an igniter coupled to an outer surface of the annular casing, with the igniter operatively coupled to the solid rocket fuel, to facilitate initiation of combustion of the solid rocket fuel.

10. The booster rocket of claim 9 , further comprising an ignition booster on an inner wall of the annular casing, with the ignition booster operatively coupled to the igniter and the solid rocket fuel, to facilitate initiation of combustion of the solid rocket fuel.

11. The booster rocket of claim 1 , wherein the annular casing includes multiple casing parts.

12. The booster rocket of claim 11 ,
wherein the multiple casing parts include an inner casing part and an outer casing part; and
wherein the inner casing part and the outer casing part are threadedly coupled together.

13. The booster rocket of claim 1 , in combination with the separate object to which the rocket booster is mechanically coupled.

14. The combination of claim 13 , wherein the separate object is an aft part of a flight vehicle.

15. The combination of claim 14 , wherein the separate object is part of a propulsion device at an aft end of the flight vehicle.

16. The combination of claim 14 , wherein the flight vehicle is a missile.

17. The booster rocket of claim 1 ,
in combination with the separate object;
wherein the separate object is part of a propulsion device at an aft end of the flight vehicle; and
wherein an inner surface of the annular casing is in contact with an outer surface of the separate object, but is not fixedly attached to the outer surface of the separate object.

18. A booster rocket comprising:
an annular casing defining an annular space therewithin, and having a central opening, wherein the annular casing includes an inner part and an outer part, wherein the inner part includes an annular slot extending along an outer surface of the inner part;
a solid rocket fuel in the annular space; and
one or more nozzle pieces mechanically coupled to the annular casing, defining one or more nozzles between the one or more nozzle pieces and the annular slot at an aft end of the annular casing;
wherein the one or more nozzle pieces includes multiple nozzle pieces;
wherein the multiple nozzle pieces are circumferentially spaced around an aft end of the annular casing; and
wherein the nozzle pieces extend aft of an aft surface of the annular casing.

19. The booster rocket of claim 18 , wherein the booster rocket is a capable of being placed around and installed around a separate object.

20. A missile comprising:
a fuselage;
a main propulsion system that includes a nozzle protruding aftward from the fuselage; and
a booster rocket around the nozzle, the booster rocket including:
an annular casing defining an annular space therewithin, and having a central opening through which the nozzle protrudes, wherein the annular casing includes an inner part and an outer part, wherein the inner part includes an annular slot extending along an outer surface of the inner part;
a solid rocket fuel in the annular space; and
one or more nozzle pieces mechanically coupled to the annular casing, defining one or more nozzles at an aft end of the annular casing;
wherein the one or more nozzle pieces includes an annular nozzle piece that defines an annular nozzle between the annular nozzle piece and the annular slot;
wherein the annular nozzle piece has an inwardly sloped section that directs flow inwardly as the flow approaches the annular nozzle;
wherein the annular casing includes an inwardly-angled aft section aft of the annular nozzle; and
wherein the booster rocket is a capable of being placed around and installed around a separate object.

Assignees

• Raytheon Co

Inventors

• Starkey Ryan
• Altamirano Dario N
• Meschberger John

Classifications

• F05D2250/281

  threaded · CPC title

• F02K9/08 Primary

  using solid propellants (F02K9/72 takes precedence; using semi-solid or pulverulent propellants F02K9/70) · CPC title

• F02K9/97 Primary

  Rocket nozzles (thrust or thrust vector control F02K9/80) · CPC title

• B64G1/403

  Solid propellant rocket engines · CPC title

• F02K9/32

  Constructional parts; Details not otherwise provided for · CPC title