Rocket motor construction from porous binder core

• US 5,386,777 A
• Filed: 02/10/1992
• Issued: 02/07/1995
• Est. Priority Date: 02/10/1992
• Status: Expired due to Fees

• Current Assignee: Aerojet-General Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Aero-Metric General Incorporated
• Inventors: Clark, George M., Mittermaier, Norman, Lou, Richard L.
• Primary Examiner(s): Nelson, Peter A.
• Application Number:
  US07/833,235
• Time in Patent Office: 1,093 Days
• Field of Search: 86/10, 86/17, 86/47, 102/291, 102/349
• US Class Current: 102/291
• CPC Class Codes: C06B 45/00 Compositions or products which are defined by structure or arrangement of component of product explosive charges of particular form or shape F42B1/00, F42B3/00
• CPC Class Codes: C06B 45/12 having contiguous layers or zones
• CPC Class Codes: F02K 9/24 Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges
• CPC Class Codes: F02K 9/34 Casings; Combustion chambers; Liners thereof

Abstract

Rocket motors are constructed by encasing a solid porous poly(vinyl alcohol) core in the shape of the propellant grain with motor casing material in the same manner as motor casing material is conventionally applied over a disposable or removable mandrel. The motor is then completed by filling the open passages of the core with liquid oxidizer. When the liquid oxidizer permeates the poly(vinyl alcohol), the result is a solid continuous propellant grain of rubbery consistency. Aluminum powder may be incorporated in either the porous poly(vinyl alcohol) or the liquid oxidizer to achieve a fuel-enhanced propellant.

Claims

1. A method for the manufacture of a solid propellant-based rocket motor, said method comprising:

(a) forming a body of solid foraminous poly(vinyl alcohol) in the shape of a propellant grain of a solid propellant-based rocket motor with an axial passage;

(b) encasing said body of solid foraminous poly(vinyl alcohol) in a solid inert shell;

(c) with said axial passage blocked, filling the interstitial volume of said body of solid foraminous poly(vinyl alcohol) with a liquid oxidizer; and

(d) permitting said liquid oxidizer to permeate said poly(vinyl alcohol) and to thereby form a solid continuous mass.

2. A method in accordance with claim 1 in which said body of solid foraminous poly(vinyl alcohol) has a void space of from about 30% to about

3. A method in accordance with claim 1 in which said body of solid foraminous poly(vinyl alcohol) has a void space of from about 50% to about

4. A method in accordance with claim 1 in which said liquid oxidizer is a composition comprising one or more members selected from the group consisting of ammonium nitrate, lower alkylammonium nitrate, lower alkylhydroxylammonium nitrate, hydroxylammonium nitrate, hydrazinium nitrate, lithium nitrate, ammonium perchlorate, lower alkylammonium perchlorate, lower alkylhydroxylammonium perchlorate, hydroxylammonium perchlorate, hydrazinium perchlorate, and lithium perchlorate, selected such that the lowest temperature at which said composition is entirely in the liquid phase is within the range of about 30°

C. or below.

5. A method in accordance with claim 1 in which said liquid oxidizer is a composition selected from the group consisting of:

(i) ammonium or lower alkyl ammonium nitrate and hydroxylammonium nitrate;

(ii) hydrazinium nitrate and hydroxylammonium nitrate;

(iii) ammonium or lower alkyl ammonium nitrate, hydrazinium nitrate and hydroxylammonium nitrate;

(iv) ammonium or lower alkyl ammonium nitrate, hydrazinium nitrate and lithium nitrate; and

(v) lower alkylhydroxylammonium nitrate and hydroxylammonium nitrate;

the proportion of components in each said composition selected such that the lowest temperature at which said composition is entirely in the liquid phase is within the range of about 30°

C. or below.

6. A method in accordance with claim 1 in which said liquid oxidizer is a nonaqueous mixture containing ammonium or lower alkyl ammonium nitrate and hydroxylammonium nitrate, the proportion of said ammonium or lower alkyl ammonium nitrate in said mixture selected such that the lowest temperature at which said mixture is entirely in the liquid phase is within the range of about 30°

C. or below.

7. A method in accordance with claim 1 further comprising incorporating metallic fuel particles into said solid continuous mass.

8. A method in accordance with claim 7 in which said metallic fuel particles are incorporated in at least one of said corrugated and non-corrugated sheets of poly(vinyl alcohol).

9. A method in accordance with claim 7 in which said metallic fuel particles are dispersed in said liquid oxidizer.

10. A method in accordance with claim 7 in which said metallic fuel particles comprise from about 10% to about 40% of said solid continuous mass.

11. A method in accordance with claim 1 further comprising coating the exterior surface of said cylindrical body of foraminous poly(vinyl alcohol) with an elastomeric material prior to step (b) to seal all openings therein.

12. A method in accordance with claim 1 in which step (b) comprises:

(i) winding around said cylindrical body a strip of fiber matrix impregnated with resin; and

(ii) curing said resin.

13. A method for the manufacture of a solid propellant-based rocket motor, said method comprising:

(a) combining a corrugated sheet of poly(vinyl alcohol) with at least one non-corrugated sheet of poly(vinyl alcohol) into a composite sheet and winding said composite sheet around a mandrel to form a cylindrical body of foraminous poly(vinyl alcohol) with an axial passage defined by said mandrel;

(b) encasing said cylindrical body of foraminous poly(vinyl alcohol) in a solid inert shell;

(c) with said axial passage blocked, filling the interstitial volume of said cylindrical body of said foraminous poly(vinyl alcohol) with a liquid oxidizer; and

(d) permitting said liquid oxidizer to permeate said poly(vinyl alcohol) and to thereby form a solid continuous mass.

14. A method in accordance with claim 13 in which said poly(vinyl alcohol) in said corrugated and non-corrugated sheets has a moisture content of at least about 2% by weight, and said method further comprises lowering said moisture content by an amount sufficient to increase the rigidity of said poly(vinyl alcohol) between steps (a) and (b).

15. A method in accordance with claim 13 in which said poly(vinyl alcohol) in said corrugated and non-corrugated sheets has a moisture content of at least about 2% by weight, and said method further comprises exposing said cylindrical body of foraminous poly(vinyl alcohol) to a stream of dry gas at an elevated temperature between steps (a) and (b) to lower said moisture content by an amount sufficient to increase the rigidity of said poly(vinyl alcohol).

16. A method in accordance with claim 13 further comprising incorporating metallic fuel particles into said solid continuous mass.

17. A method in accordance with claim 16 in which said metallic fuel particles are incorporated in at least one of said corrugated and non-corrugated sheets of poly(vinyl alcohol).

18. A method in accordance with claim 16 in which said metallic fuel particles are dispersed in said liquid oxidizer.

19. A method in accordance with claim 16 in which said metallic fuel particles comprise from about 10% to about 40% of said solid continuous mass.

20. A method in accordance with claim 13 in which said cylindrical body of foraminous poly(vinyl alcohol) has a void space of from about 30% to about 90%.

21. A method in accordance with claim 13 in which said cylindrical body of foraminous poly(vinyl alcohol) has a void space of from about 50% to about 80%.

22. A method in accordance with claim 13 further comprising coating the exterior surface of said cylindrical body of foraminous poly(vinyl alcohol) with an elastomeric material prior to step (b) to seal all openings therein.

23. A method in accordance with claim 13 in which step (b) comprises:

(i) winding around said cylindrical body a strip of fiber matrix impregnated with resin; and

(ii) curing said resin.

24. A method in accordance with claim 13 in which said liquid oxidizer is a composition comprising one or more members selected from the group consisting of ammonium nitrate, lower alkylammonium nitrate, lower alkylhydroxylammonium nitrate, hydroxylammonium nitrate, hydrazinium nitrate, lithium nitrate, ammonium perchlorate, lower alkylammonium perchlorate, lower alkylhydroxylammonium perchlorate, hydroxylammonium perchlorate, hydrazinium perchlorate, and lithium perchlorate, selected such that the lowest temperature at which said composition is entirely in the liquid phase is within the range of about 30°

C. or below.

25. A method in accordance with claim 13 in which said liquid oxidizer is a composition selected from the group consisting of:

(i) ammonium or lower alkyl ammonium nitrate and hydroxylammonium nitrate;

(ii) hydrazinium nitrate and hydroxylammonium nitrate;

(iii) ammonium or lower alkyl ammonium nitrate, hydrazinium nitrate and hydroxylammonium nitrate;

(iv) ammonium or lower alkyl ammonium nitrate, hydrazinium nitrate and lithium nitrate; and

(v) lower alkylhydroxylammonium nitrate and hydroxylammonium nitrate;

the proportion of components in each said composition selected such that the lowest temperature at which said composition is entirely in the liquid phase is within the range of about 30°

C. or below.

26. A method in accordance with claim 13 in which said liquid oxidizer is a nonaqueous mixture containing ammonium or lower alkyl ammonium nitrate and hydroxylammonium nitrate, the proportion of said ammonium or lower alkyl ammonium nitrate in said mixture selected such that the lowest temperature at which said mixture is entirely in the liquid phase is within the range of about 30°

C. or below.

27. A method in accordance with claim 13 further comprising forming said composite sheet and winding said composite sheet around said mandrel in step (a) such that said solid continuous mass formed in step (d) has a variable burn rate which decreases radially through the cross section of said liquid oxidizer-permeated poly(vinyl alcohol).

28. A method in accordance with claim 27 in which said variable burn rate is achieved by a spatial variation in the chemical composition of said poly(vinyl alcohol) of at least one of said corrugated and non-corrugated sheets of poly(vinyl alcohol).

29. A method in accordance with claim 27 in which said variable burn rate is achieved by a variation in the void volume of said cylindrical body of foraminous poly(vinyl alcohol).

30. A method in accordance with claim 29 in which said void volume variation is achieved by varying the number of non-corrugated sheets of poly(vinyl alcohol) used in the formation of said composite sheet in step (a).

31. A method in accordance with claim 29 in which said void volume variation is achieved by varying the ratio of flute diameter to film thickness in said corrugated sheet of poly(vinyl alcohol).

32. A method in accordance with claim 13 in which the thickness of said poly(vinyl alcohol) in both said corrugated and said non-corrugated sheets is from about 0.003 cm to about 0.2 cm.

33. A method in accordance with claim 13 in which the thickness of said poly(vinyl alcohol) in both said corrugated and said non-corrugated sheets is from about 0.01 cm to about 0.05 cm.

34. A method for the manufacture of an encased foraminous propellant binder for combination with a liquid oxidizer to form a solid propellant-based rocket motor, said method comprising:

(a) combining a corrugated sheet of poly(vinyl alcohol) with at least one non-corrugated sheet of poly(vinyl alcohol) into a composite sheet and winding said composite sheet around a mandrel to form a cylindrical body of foraminous poly(vinyl alcohol) with an axial passage defined by said mandrel; and

(b) encasing said cylindrical body of foraminous poly(vinyl alcohol) in a solid inert shell.

35. A method in accordance with claim 34 in which said poly(vinyl alcohol) in said corrugated and non-corrugated sheets has a moisture content of at least about 2% by weight, and said method further comprises lowering said moisture content by an amount sufficient to increase the rigidity of said poly(vinyl alcohol) between steps (a) and (b).

36. A method in accordance with claim 34 in which said poly(vinyl alcohol) in said corrugated and non-corrugated sheets has a moisture content of at least about 2% by weight, and said method further comprises exposing said cylindrical body of foraminous poly(vinyl alcohol) to a stream of dry gas at an elevated temperature between steps (a) and (b) to lower said moisture content by an amount sufficient to increase the rigidity of said poly(vinyl alcohol).

37. A method in accordance with claim 34 further comprising incorporating metallic fuel particles into at least one of said corrugated and noncorrugated sheets of poly(vinyl alcohol).

38. A method in accordance with claim 37 in which said metallic fuel particles comprise from about 40% to about 70% by weight of said corrugated and non-corrugated sheets.

39. A method in accordance with claim 34 in which said cylindrical body of foraminous poly(vinyl alcohol) has a void space of from about 10% to about 50%.

40. A method in accordance with claim 34 in which said cylindrical body of foraminous poly(vinyl alcohol) has a void space of from about 15% to about 40%.

41. A method in accordance with claim 34 further comprising coating the exterior surface of said cylindrical body of foraminous poly(vinyl alcohol) with an elastomeric material prior to step (b) to seal all openings therein.

42. A method in accordance with claim 34 in which step (b) comprises:

(i) winding around said cylindrical body a strip of fiber matrix impregnated with resin; and

(ii) curing said resin.

43. A method in accordance with claim 34 further comprising forming said composite sheet and winding said composite sheet around said mandrel in step (a) such that said cylindrical body of foraminous poly(vinyl alcohol) has a variable burn rate which decreases radially through the cross section of said liquid oxidizer-permeated poly(vinyl alcohol).

44. A method in accordance with claim 43 in which said variable burn rate is achieved by a spatial variation in the chemical composition of said poly(vinyl alcohol) of at least one of said corrugated and non-corrugated sheets of poly(vinyl alcohol).

45. A method in accordance with claim 43 in which said variable burn rate is achieved by a variation in the void volume of said cylindrical body of foraminous poly(vinyl alcohol).

46. A method in accordance with claim 45 in which said void volume variation is achieved by varying the number of non-corrugated sheets of poly(vinyl alcohol) used in the formation of said composite sheet in step (a).

47. A method in accordance with claim 45 in which said void volume variation is achieved by varying the ratio of flute diameter to film thickness in said corrugated sheet of poly(vinyl alcohol).

48. A method in accordance with claim 34 in which the thickness of said poly(vinyl alcohol) in both said corrugated and said non-corrugated sheets is from about 0.003 cm to about 0.2 cm.

49. A method in accordance with claim 34 in which the thickness of said poly(vinyl alcohol) in both said corrugated and said non-corrugated sheets is from about 0.01 cm to about 0.05 cm.

50. A binder-filled motor case for use in forming a solid propellant-based rocket motor by addition of a liquid oxidizer, said binder-filled motor case comprising a body of solid foraminous poly(vinyl alcohol) in the shape of a propellant grain of a solid propellant-based rocket motor with an axial passage, encased in a solid inert shell.

51. A binder-filled motor case in accordance with claim 50 in which said body of solid foraminous poly(vinyl alcohol) has a void space of from about 30% to about 90%.

52. A binder-filled motor case in accordance with claim 50 in which said body of solid foraminous poly(vinyl alcohol) has a void space of from about 50% to about 80%.