Missile canister and method of fabrication

• US 5,115,711 A
• Filed: 03/25/1991
• Issued: 05/26/1992
• Est. Priority Date: 03/25/1991
• Status: Expired due to Term

• Current Assignee: FMC Corporation
• Original Assignee: FMC Corporation
• Inventors: Bovee, Stan P., Vaske, James G., Bushagour, Abubaker M.
• Primary Examiner(s): BROWN, DAVID
• Application Number:
  US07/675,365
• Time in Patent Office: 428 Days
• Field of Search: 89/1.816, 89/1.817, 89/1.818, 523/218, 521/54
• US Class Current: 89/1.816
• CPC Class Codes: F41F 3/042 the launching apparatus being used also as a transport container for the rocket F41F3/065 takes precedence

Abstract

A missile canister for storing, transporting and launching missiles includes inner and outer skins and a compression resistant honeycomb type material between the skins. An alternative embodiment on the missile canister has an epoxy syntactic foam material between the skins of the cells which are attached one to another by threaded fasteners which cooperate with tapped holes in the cell walls.

Claims

1. A missile canister for storing, transporting and launching missiles comprising:

an outer canister skin surrounding a longitudinal canister axis;

a plurality of missile cells within said canister skin, each of said missile cells having a longitudinal cell axis generally parallel to said canister axis and a cell skin surrounding said cell axis, said canister skin and said cell skins together defining an interstitial space; and

,

a compression resistant material, including honeycomb type material, within said interstitial space.

2. A missile cell for storing, transporting and launching a missile comprising:

an outer missile cell skin surrounding a longitudinal missle cell axis;

an inner missile cell skin surrounding said longitudinal missle cell axis such that an interstitial space is defined between said inner and outer missile cell skins; and

a compression resistant material including a honeycomb type material within said interstitial space.

3. A missile cannister for storing, transporting and launching missiles comprising:

a plurality of missile cells, each missile cell having a cell wall generally surrounding a longitudinal missile cell axis;

releasable attachment for releasably fastening said cells together including means for releasably attaching one of said cells in fixed relation to another one of said cells;

each of said cell walls including an outer missile cell skin surrounding said londitudinal missile cell axis and an inner missile cell skin surrounding said longitudinal cell axis, such that an interstitial space is defined between said inner missile cell skin and said outer missle cell skin, and a compression resistant material including a honeycomb type material within said interstitial space.

4. A missile canister as in claim 3 in which said releasable attachment means comprises:

a tie strip having a longitudinal axis lying generally between a first and a second edge portion;

first means for releasably connecting said first edge portion to the wall of a first cell; and

,

second means for releasably connecting said second edge portion to the wall of a second cell.

5. A missile canister as in claim 3, in which said compression resistant material includes a foam material.

6. A missle cell as in claim 5 in which said foam has a density of about 40 pcf.

7. A missile cell as in claim 5, in which said foam is an epoxy syntactic comprising glass microspheres within an epoxy polymer matrix.

8. A missile cell as in claim 7 in which said microspheres are of a diameter of about five microns.

9. A missile cell as in claim 8, in which said epoxy syntactic foam is formed by mixing about 55 percent epoxy resin, 22 percent epoxy hardener, 5 percent cure accelerator and 17 percent glass microspheres by weight.

10. A missile cannister for storing, transporting and launching missiles comprising:

a plurality of missile cells, each missile cell having a cell wall generally surrounding a longitudinal missle cell axis;

releasable fastening means for releasably fastening said cells together;

each of said cell walls including an outer missile cell skin surrounding said longitudinal missile cell axis and an inner missle cell skin surrounding said longitudinal cell axis, such that an interstitial space is defined between said inner missile cell skin and said outer missile cell skin, and a compression resistant material including a honeycomb type material within said interstitial space.

11. A missile cannister for storing, transporting and launching missiles comprising:

a plurality of missile cells, each missile cell having a cell wall generally surrounding a longitudinal missile cell axis;

releasable fastening means for releasably fastening said cells together;

each of said cell walls including an outer missile cell skin surrounding said longitudinal missile cell axis and an inner missile cell skin surrounding said longitudinal cell axis, such that an interstitial space is defined between said inner missile cell skin and said outer missile cell skin, and a compression resistant material within said interstitial space;

said releasable fastening means comprising;

a tie strip having a longitudinal axis lying generally between a first and a second edge portion;

first means for releasably connecting said first edge portion to the wall of a first cell;

second means for releasably connecting said edge portion to the wall of a second cell;

said first and second releasable connecting means each including threaded fasteners adapted to cooperate with threaded holes formed in said first and second cell walls.

12. A missile cannister as in claim 11 in which said cell axes are generally parallel to one another and said cells have a generally square cross section.

13. A missile canister as in claim 12 in which each of said cells comprises a longitudinal corner fitting at a corner of the cell and said threaded holes are formed in said corner fitting.

14. A missile canister as in claim 13 in which said compression resistant material includes a honeycomb type material.

15. A missle cell as in claim 14 in which said compression resistant material includes a foam material.

16. A missile cell as in claim 15 in which said foam is an epoxy syntactic foam comprising glass microspheres within an epoxy polymer matrix.

17. A missile cell as in claim 16 in which said epoxy syntactic foam is formed by mixing about 55 percent epoxy resin, 22 percent epoxy hardener, 5 percent cure accelerator and 17 percent glass microspheres by weight.