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US4522356A Expired / Lapsed US ⏱️ 0.0 years remaining

Multiple target seeking clustered munition and system

Assignee: Hughes Missile Systems Co
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Filing: 1973-11-12
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Granted: 1985-06-11
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Expires: 1993-11-12
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Abstract

Abstract A clustered munition in a system for low altitude aerial delivery, which releases multiple rocket powered missiles, each having the capability to cruise at a constant altitude and search for a target. Once a target is identified, the missile homes on and strikes the target. In the preferred form the target seeking means is a radiometric seeker operating in the millimeter wavelength range, in which metal or similarly reflective targets stand out against the background and provide a significant signal which is used to program the terminal action of the missile.

Inventors

  • 👤 Clair K. Lair
  • 👤 Jules Jonas
  • 👤 Keith D. Anderson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 05:48
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/60; F42B10/62; F42B10/64; F41; F41G; F41G7/00; F41G7/20; F41G7/22; F41G7/2233; F42B15/00; F42B15/10; F42B15/105; F42B23/00; F42B23/04

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 252 words
A multiple target seeking clustered munition system, comprising: a plurality of target seeking missiles arranged in a cluster, each of said missiles having a body with aerodynamic sustaining and controlling surfaces mounted thereon; conveyance means for holding and carrying said clustered missiles, and including means for releasing the missiles therefrom in the vicinity of a target; target seeking means operably mounted in said missile body, the target seeking means including a receiver sensitive to radiation from a target and its surroundings, and having means for identifying the target against the background; a receiving antenna coupled to said receiver; drive means for driving the antenna in a search scan pattern, and being responsive to signals from the target seeking means to drive the antenna in a target tracking scan upon identification of a target; target identification means having pulse amplitude and pulse width discriminating means for identifying a target signal pulse in a background signal of different and substantially constant level, and including pulse counting means for determining the number of target pulses in each scan of the antenna; propulsion means operably mounted in said missile body for propelling said missile in cruising flight after release from the conveyance means; a warhead operably mounted in said missile body; and guidance means coupled to said controlling surfaces, said guidance means being responsive to signals from said target seeking means to guide said missile in cruising flight and, upon identification of a target, to operate said controlling surfaces and guide the missile to the target.
Claim 2
Dependent Claim 252 words
A multiple target seeking clustered munition system, comprising: a plurality of target seeking missiles arranged in a cluster, each of said missiles having a body with aerodynamic sustaining and controlling surfaces mounted thereon; conveyance means for holding and carrying said clustered missiles, and including means for releasing the missiles therefrom in the vicinity of a target; target seeking means operably mounted in said missile body, the target seeking means including a receiver sensitive to radiation from a target and its surroundings, and having means for identifying the target against the background; a receiving antenna coupled to said receiver; drive means for driving the antenna in a search scan pattern, and being responsive to signals from the target seeking means to drive the antenna in a target tracking scan upon identification of a target; target identification means having pulse amplitude and pulse width discriminating means for identifying a target signal pulse in a background signal of different and substantially constant level, and including pulse counting means for determining the number of target pulses in each scan of the antenna; propulsion means operably mounted in said missile body for propelling said missile in cruising flight after release from the conveyance means; a warhead operably mounted in said missile body; and guidance means coupled to said controlling surfaces, said guidance means being responsive to signals from said target seeking means to guide said missile in cruising flight and, upon identification of a target, to operate said controlling surfaces and guide the missile to the target.
Claim 3
Dependent Claim 36 words
A multiple target seeking clustered munition system according to claim 1, wherein said guidance means is responsive to a predetermined combination of pulse amplitude, pulse width and pulse count to guide the missile to the target.
Claim 4
Dependent Claim 28 words
A multiple target seeking clustered munition system according to claim 2, wherein said receiver is a radiometric receiver having an effective frequency on the order of 35 GHz.
Claim 5
Dependent Claim 30 words
A multiple target seeking clustered munition system according to claim 1, and including altitude sensing means coupled to said guidance means for holding the missile at a predetermined cruising altitude.

References Cited (Backward Citations)

US2450910A Cited
US2585030A Cited
US3064924A Cited
US2951658A Cited
US2961928A Cited
US3048086A Cited
US3196793A Cited
US3712562A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-06-10 1988-12-10 1989-06-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-06-10 1992-12-10 1993-06-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-06-10 1996-12-10 1997-06-11 $7700.00 Window Closed / Lapsed

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