Two-piece aft closure for a rocket motor case

1. A system for sealing a rocket motor case to an aft closure assembly, wherein the aft closure assembly comprises a retaining ring piece and a closure piece, comprising:

(a) a retaining ring made from a material having a coefficient of expansion similar to the rocket motor case material, the retaining ring piece having a first seal to seal between an outer surface of the retaining ring and the inner surface of the rocket motor case; and

(b) a closure made from a material having a coefficient of expansion different to the coefficient of expansion of the retaining ring, the closure stationarily connected to a fixed location on the retaining ring, the closure having a second seal to seal between the closure and a face of the retaining ring;

(c) wherein the face of the retaining ring that is sealed by the second seal is orthogonal to the outer surface of the retaining ring.

2. The system of claim 1 , further comprising means for connecting the retaining ring to the closure.

3. The system of claim 1 , wherein the retaining ring is generally circular, and the first seal seals the outer circumference of the retaining ring to the rocket motor case.

4. The system of claim 1 , wherein the closure includes an aperture that provides an opening from the interior of the rocket motor case to the exterior.

5. The system of claim 1 , wherein the retaining ring is made from a material having a first coefficient of thermal expansion, and the closure is made from a material having a second coefficient of thermal expansion that is greater than the first coefficient of thermal expansion.

6. The system of claim 1 , wherein the retaining ring is made from a material that is similar to the material of the rocket motor case.

7. The system of claim 1 , wherein the rocket motor case is made from a material having a first coefficient of thermal expansion, and the closure is made from a material having a second coefficient of thermal expansion that is greater than the first coefficient of thermal expansion.

8. The system of claim 1 , wherein the closure is made from a material that is lighter in weight than the material of the rocket motor case.

9. The system of claim 1 , wherein the closure is made from a material that is lighter in weight than the material of the retaining ring.

10. The system of claim 1 , wherein the rocket motor case is made from a material that is stronger than the material of the closure.

11. The system of claim 1 , wherein the retaining ring is made from a material that is stronger than the material of the closure.

12. The system of claim 1 , wherein the retaining ring is made from titanium, steel, alloys of titanium, alloys of steel, or any combination thereof.

13. The system of claim 1 , wherein the closure is made from aluminum, alloys of aluminum, or any combination thereof.

14. The system of claim 1 , wherein the closure partially closes an end of the rocket motor case and is a separate component from the rocket motor case.

15. The system of claim 1 , wherein the first and the second seals comprise an O-ring.

16. A motor case for a rocket engine, comprising the system for sealing of claim 1 .

17. A rocket engine, comprising a motor case and the system for sealing of claim 1 .

18. The system of claim 1 , wherein the second seal is maintained as the closure moves radially relative to the retaining ring.

19. A system for sealing a rocket motor case, comprising a retaining ring inside the rocket motor case, the retaining ring having a proximal end and a distal end, a radial seal to seal between an inside surface of the rocket motor case and the retaining ring, and a closure having a face seal to seal between a distal facing surface of the closure and a proximal facing surface at the proximal end of the retaining ring, the closure connected to a fixed location on the retaining ring, wherein the face seal is maintained as the closure moves relative to the retaining ring.

20. The system of claim 19 , wherein the rocket motor case has an inner diameter and the closure has about the same or smaller outer diameter so that the closure is fitted within the inner diameter of the rocket motor case.

21. The system of claim 19 , wherein the rocket motor case has an inner diameter and the retaining ring has about the same or smaller outer diameter so that the retaining ring is fitted within the inner diameter of the rocket motor case.

22. The system of claim 19 , wherein the retaining ring has a length greater than its thickness and a groove around its outer circumference and an O-ring in the groove.

23. The system of claim 19 , wherein the retaining ring has an inner and an outer diameter and a surface annulus at the proximal and distal end.

24. The system of claim 23 , wherein the closure has a circular flange at one end of the closure, wherein the face of the circular flange faces the surface annulus at the proximal end of the retaining ring, and the flange includes a groove around the face of the flange and an O-ring in the groove.

25. The system of claim 19 , wherein the closure includes an aperture that provides an opening from the interior of the rocket motor case to the exterior.

26. An aft closure assembly for a rocket motor case, comprising:

(a) a retaining ring piece inside the rocket motor case and having a first seal around the outer circumference that seals against an inner circumference of the rocket motor case, the retaining ring piece stationarily attached to the motor case; and

(b) an aft closure piece comprising a blast tube, the closure piece stationarily attached to the retaining ring piece and having a second seal on a face of the retaining ring piece to seal between the retaining ring piece and the closure piece, wherein the rocket motor case is open to the exterior via the blast tube.

27. A system for sealing a rocket motor case having an opening, comprising:

(a) a retaining ring on the inside of the rocket motor case to seal between the rocket motor case and the retaining ring; and

(b) a closure connected to the retaining ring, the closure having a surface orthogonal to the outside circumference of the retaining ring to seal between an end face of the retaining ring and the orthogonal surface, wherein the orthogonal surface contacts the end face and is configured to move radially relative to the end face of the retaining ring, and wherein the closure includes an aperture that provides an opening from the interior of the rocket motor case to the exterior.

28. An aft closure assembly for a rocket motor case, comprising:

(a) a retaining ring piece inside the rocket motor case having a first seal to seal between an outer surface of the retaining ring piece and an interior surface of a rocket motor case, wherein the first seal is maintained as the retaining ring moves relative to the rocket motor case and the retaining ring piece is stationarily attached to the motor case; and

(b) an aft closure piece comprising a blast tube, the closure piece stationarily connected to a fixed location on the retaining ring piece, the closure piece having a distal face formed by a circular flange at the proximal end thereof, the distal face having a second seal to seal between the distal face and a proximal end face of the retaining ring, the proximal end face of the retaining ring in contact with the distal face of the closure piece;

(c) wherein the proximal end face of the retaining ring piece that is sealed by the second seal is orthogonal to the outer surface of the retaining ring piece, and the second seal is maintained as the closure piece moves radially relative to the retaining ring piece; and

(d) wherein the retaining ring piece is made from a material having a first coefficient of thermal expansion similar to the rocket motor case material, and the closure piece is made from a material having a second coefficient of thermal expansion that is different than the first coefficient of thermal expansion.