Missile launcher

Claim 2

An airborne missile launcher of modular construction comprising: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which ccoperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section; (e) sub-rail locking means; (f) retracting means for a missile umbilical connection; (g) retraction means for missile striker points; (h) retractable missile hook snubbers; and (i) a nitrogen bottle with a nitrogen supply regulator carried right forward of said main body section.

Claim 3

An airborne missile launcher of modular construction comprising: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail setion and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section; (e) a detachable fairing for attachment forward of said main body; and (f) a nitrogen bottle with a nitrogen supply regulator, said nitrogen bottle and supply regulator being contained within said detachable fairing.

Claim 4

An airborne missile launcher of modular construction comprising: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail setion and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section; (e) a detachable fairing for attachment forward of said main body; and (f) a nitrogen bottle with a nitrogen supply regulator, said nitrogen bottle and supply regulator being contained within said detachable fairing.

Claim 5

A missile launcher according to claim 2 where the aft end of the main body section carries an anti-radar chaff dispenser.

Claim 6

An airborne missile launcher of modular construction comprising: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, hold-back shoes extendible from said body section to the missile being carried, actuating means for extending and retracting said hold back shoes, and linkages between said hold-back shoes and said actuating means where said hold-back shoes, when extended, contact the missile to enable the missile propulsion motor to power up before permitting translation of the missile relative to said sub-rail.

Claim 7

An airborne missile launcher of modular construction comprising: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, hold-back shoes extendible from said body section to the missile being carried, actuating means for extending and retracting said hold back shoes, and linkages between said hold-back shoes and said actuating means where said hold-back shoes, when extended, contact the missile to enable the missile propulsion motor to power up before permitting translation of the missile relative to said sub-rail.

Claim 8

An airborne missile launcher according to claim 4 where said actuation means is a solenoid and said linkage is a pivotable toggle linkage.

Claim 9

An airborne missile launcher of modular construction comprising: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces, first and second oppositely disposed sides, and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length, said first and second sides, respectively, being convexly bulged to decrease vertical stiffness and promote vibration absorption; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section.

Claim 10

An airborne missile launcher of modular construction comprising: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces, first and second oppositely disposed sides, and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length, said first and second sides, respectively, being convexly bulged to decrease vertical stiffness and promote vibration absorption; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section.

Claim 11

Improvements in an airborne missile launcher of modular construction including: (a) a main module, comprising an intermediate main body section having a first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a bus-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, the improvement comprising: (1) a detachable fairing for attachment forward of said main body, (2) a nitrogen bottle with a nitrogen supply regulator, said nitrogen bottle and supply regulator being contained within said detachable fairing.

Claim 12

Improvements in an airborne missile launcher of modular construction including: (a) a main module, comprising an intermediate main body section having a first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a bus-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, the improvement comprising: (1) a detachable fairing for attachment forward of said main body, (2) a nitrogen bottle with a nitrogen supply regulator, said nitrogen bottle and supply regulator being contained within said detachable fairing.

Claim 13

Improvements in an airborne missile launcher of modular construction including: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, the improvement comprising: hold-back shoes extendible from said main body section to the missile being carried, activity means for extending and retracting said hold-back shoes, and linkages between said hold-back shoes and said actuating means where said hold-back shoes, when extended, contact the missile to enable the missile propulsion motor to power up before permitting translation of the missile relative to the sub-rail.

Claim 14

Improvements in an airborne missile launcher of modular construction including: (a) a main module, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, the improvement comprising: hold-back shoes extendible from said main body section to the missile being carried, activity means for extending and retracting said hold-back shoes, and linkages between said hold-back shoes and said actuating means where said hold-back shoes, when extended, contact the missile to enable the missile propulsion motor to power up before permitting translation of the missile relative to the sub-rail.

Claim 15

Improvements in an airborne missile launcher of modular construction including: (a) a main nodule, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, the improvement comprising: convexly bulged sides of the main body section to decrease vertical stiffness and absorb vibrations.

Claim 16

Improvements in an airborne missile launcher of modular construction including: (a) a main nodule, comprising an intermediate main body section having first and second oppositely disposed surfaces and first and second oppositely disposed ends said intermediate main body section usable with all the types of missile to be carried and of a length less than full body length, said main body being adapted for fixing to an aircraft along its first surface, said main body section having a first member of a first cooperating attachment element located proximate to said first end, a first member of a second cooperating attachment element located proximate to said second end and a first member of a third cooperating attachment element proximate to said second surface said main body further adapted to receive a nose section and a tail section to complete the body length; (b) a forward module, comprising a nose section and a second member of the first attachment element which cooperates with the first member to connect the nose section to the main body section in a manner where the nose section is releasably affixed to the first end of the main body section; (c) an aft module, comprising a tail section and a second member of the second attachment element which cooperates with the first member to connect the tail section to the main body section in a manner where the tail section is releasably affixed to the second end of the main body section; and (d) a sub-rail adapted to carry a missile and a second member of the third attachment element which cooperates with the first member to connect the sub-rail to the main body section in a manner where the sub-rail is releasably attached to said main body section, the improvement comprising: convexly bulged sides of the main body section to decrease vertical stiffness and absorb vibrations.

Claim 17

A missile launcher according to claim 1, wherein the sides of the main body section are convexly bulged to reduce vertical stiffness and absorb vibrations.