초록 ▼

Methods and apparatus for a multiple part missile according to various aspects of the present invention may operate in conjunction with a first missile part having a first groove formed in a surface of the first missile part and a second missile part having a second groove. A snap ring may be config

Methods and apparatus for a multiple part missile according to various aspects of the present invention may operate in conjunction with a first missile part having a first groove formed in a surface of the first missile part and a second missile part having a second groove. A snap ring may be configured to engage the first groove and the second groove.

대표청구항 ▼

1. A missile, comprising: a first missile part having a first adapter comprising a first annular groove formed in a surface of the first missile part and a first electrical connector;a second missile part having a second adapter comprising a second annular groove formed in a surface of the second mi

1. A missile, comprising: a first missile part having a first adapter comprising a first annular groove formed in a surface of the first missile part and a first electrical connector;a second missile part having a second adapter comprising a second annular groove formed in a surface of the second missile part and a second electrical connector configured to mate with the first electrical connector; anda snap ring configured to engage the first groove and the second groove and to thereby couple the first missile part and the second missile part, and wherein the first and second electrical connectors are mated with each other when the first and second missile parts are coupled to each other to thereby facilitate electrical communication between the first missile part and the second missile part. 2. A missile according to claim 1, wherein the first adapter is connected to a first missile body part and the second adapter is connected to a second missile body part, wherein the first annular groove is formed in a surface of the first adapter and the second annular groove is formed in a surface of the second adapter. 3. A missile according to claim 2, wherein at least a portion of an exterior surface of the first missile body part is flush with at least a portion of an exterior surface of the first adapter and at least a portion of an exterior surface of the second missile body part is flush with at least a portion of an exterior surface of the second adapter. 4. A missile according to claim 1, wherein at least one of the first missile part and the second missile part further comprises a ramp configured to engage the snap ring. 5. A missile according to claim 1, wherein at least one of the first missile part and the second missile part includes an alignment guide configured to facilitate rotational alignment of the first missile part with the second missile part such that the first and second electrical connectors are rotationally aligned with each other and rigidly maintained in rotational position with respect to each other. 6. A missile according to claim 1, wherein the first electrical connector and the second electrical connector form a blind mate connection. 7. A missile according to claim 1, wherein at least one of the first missile part and the second missile part includes an alignment guide configured to facilitate rotational alignment of the first missile part with the second missile part. 8. A missile according to claim 7, wherein the alignment guide comprises a pin attached to the first missile part and a surface defining a hole attached to the second missile part, wherein the pin is configured to be inserted into the hole. 9. A missile according to claim 1 wherein the first adapter comprises a hollow cylinder with an interior surface that comprises the first annular groove, and wherein the second adapter comprises a second hollow cylinder with an exterior surface that comprises the second annular groove. 10. A missile according to claim 9, wherein at least one of the first adapter and the second adapter further comprises a ramp configured to engage the snap ring. 11. A missile according to claim 9, wherein at least a portion of an exterior surface of the first adapter is configured to be flush with at least a portion of an exterior surface of the first missile body part and wherein at least a portion of the exterior surface of the second adapter is configured to be flush with at least a portion of an exterior surface of the second missile body part. 12. A missile according to claim 9, wherein at least one of the first adapter and the second adapter includes an alignment guide configured to facilitate rotational alignment of the first adapter with the second adapter. 13. A missile according to claim 12, wherein the alignment guide comprises a pin attached to the first adapter and a surface defining a hole attached to the second adapter, wherein the pin is configured to be inserted into the hole. 14. The missile of claim 9 wherein the first adapter is configured to be attached to the first missile body part using at least one fastener. 15. The missile of claim 9 wherein the snap ring comprises a threaded connector configured to align with a hole in the first adapter and to receive a screw that is actuatable to deform the snap ring and to thereby allow disengagement of the first and second adapters. 16. A missile according to claim 1, wherein the first electrical connector and the second electrical connector form a blind mate connection when mated. 17. A missile, comprising: a first missile part;a first adapter attached to the first missile part and having an interior surface comprising a first annular groove, wherein the first adapter comprises a first electrical conductor;a second missile part;a second adapter attached to the second missile part and having an exterior surface comprising a second annular groove, wherein the second adapter comprises a second electrical conductor; anda snap ring configured to engage the first groove and the second groove when the first and second missile parts are connected, and wherein the first and second electrical connectors are configured to mate with each other when the first and second missile parts are connected to thereby facilitate electrical communication between the first missile part and the second missile part. 18. The missile of claim 17 wherein at least one of the first adapter and the second adapter further comprises a ramp configured to engage the snap ring. 19. The missile of claim 18 wherein the second electrical conductor is configured to align with the first electrical conductor. 20. The missile of claim 19 wherein the first and second electrical connectors are configured to form a blind mate connection. 21. The missile of claim 17 further comprising an alignment guide configured to rotationally align the first adapter with the second adapter. 22. The missile of claim 21 further comprising a pin attached to the first adapter and into a hole defined in a surface attached to the second adapter.