Spin-stabilized guided projectile

• US 5,669,581 A
• Filed: 11/17/1995
• Issued: 09/23/1997
• Est. Priority Date: 04/11/1994
• Status: Expired due to Term

• Current Assignee: Motorola Solutions, Inc.
• Original Assignee: Aerojet-General Corporation (L3Harris Technologies, Inc.)
• Inventors: Ringer, Hayden N.
• Primary Examiner(s): Carone, Michael J.
• Assistant Examiner(s): MONTGOMERY, CHRISTOPHER KEITH
• Application Number:
  US08/560,132
• Time in Patent Office: 676 Days
• Field of Search: 244/3.22, 244/3.16, 244/3.23, 244/3.15, 102/384, 102/213, 102/492, 342/62
• US Class Current: 244/3.16
• CPC Class Codes: F41G 7/222 for spin-stabilized missiles
• CPC Class Codes: F41G 7/2253 Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
• CPC Class Codes: F41G 7/2293 using electromagnetic waves other than radio waves
• CPC Class Codes: F42B 10/661 using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
• CPC Class Codes: F42C 13/02 operated by intensity of light or similar radiation

Abstract

A spin-stabilized projectile for destroying distant targets uses the projectile'"'"'s spin to carry out other functions such as target imaging, course-correction and warhead aiming. By using the spin to carry out such functions, in addition to stabilization, the projectile can be implemented with fewer or no moving parts. The projectile may utilize either right or skewed-core fusing for the warhead.

Claims

1. A spin-stabilized ballistic projectile for destroying a selected target;

the projectile having a longitudinal axis and comprising;

an imaging array of infrared detectors for scanning images in at least one of a plurality of concentric circular patterns about the projectile axis, said scanning being implemented by the spin of said projectile about said axis; and

at least one course-correction explosive device located on said projectile for applying a course correcting impulse through the center of gravity of said projectile in a direction perpendicular to said axis, the precise direction of said impulse being determined by the spin of said projectile and the timing of said impulse relative to said spin;

said imaging array having a wide angle field of view provided by a plurality of detectors configured as a radial array;

said array being configured for tracking said target to intercept based upon a skewed seeker cone using said course-correction explosive device, the skewed cone having a generatrix which is the vector sum of projectile velocity course correction divert velocity and the negative of target velocity.

2. The projectile recited in claim 1 further comprising:

a directional mass-focus warhead selectively projectable from said projectile in at least one selected direction relative to said projectile axis, the precise direction of said warhead being determined by the spin of said projectile and the timing of detonating said warhead relative to said spin.

4. The projectile recited in claim 1 further comprising:

a forward projecting terminal warhead selectively projectable from said projectile, the precise direction of said warhead being dependent upon the spin of said projectile and the timing of detonation of said warhead.

3. A spin-stabilized ballistic projectile for destroying a selected target;

the projectile having a longitudinal axis and comprising;

an imaging array of infrared detectors for scanning images in at least one of a plurality of concentric circular patterns about the projectile axis, said scanning being implemented by the spin of said projectile about said axis; and

a directional mass-focus warhead selectively projectable from said projectile in at least one selected direction relative to said projectile axis, the precise direction of said warhead being determined by the spin of said projectile and the timing of detonating said warhead relative to said spin;

said imaging array having a wide angle field of view provided by a plurality of detectors configured as a radial array;

said array being configured for tracking said target to intercept based upon a skewed fuzing cone and for selectively projecting said directional mass-focus warhead at a vulnerable area of said target, the skewed cone having a generatrix which is the vector sum of projectile velocity warhead velocity and the negative of target velocity.

5. A spin-stabilized ballistic projectile for destroying a selected target;

the projectile having a longitudinal axis and comprising;

an imaging array of infrared detectors for scanning images in at least one of a plurality of concentric circular patterns about the projectile axis, said scanning being implemented by the spin of said projectile about said axis; and

a planar warhead selectively projectable from said projectile;

said imaging array having a wide angle field of view provided by a plurality of detectors configured as a radial array;

said array being configured for tracking said target to intercept based upon a skewed fuzing cone and for selectively projecting said directional mass-focus warhead at a vulnerable area of said target, the skewed cone having a generatrix which is the vector sum of projectile velocity, warhead velocity and the negative of target velocity.

6. The spin-stabilized ballistic projectile recited in claim 5 and further comprising:

at least one course-correction explosive device located on said projectile for applying a course correcting impulse through the center of gravity of said projectile in a direction perpendicular to said axis, the precise direction of aid impulse being determined by the spin of said projectile and the timing of said impulse relative to said spin.