Ranged limited projectile using augmented roll damping

• US RE38,261 E1
• Filed: 07/31/2001
• Issued: 10/07/2003
• Est. Priority Date: 09/09/1997
• Status: Expired due to Term

• Current Assignee: General Dynamics Ordnance and Tactical Systems Incorporated (General Dynamics Corporation)
• Original Assignee: General Dynamics Ordnance and Tactical Systems Incorporated (General Dynamics Corporation)
• Inventors: White, Charles O.
• Primary Examiner(s): TUDOR, HAROLD JAY
• Application Number:
  US09/919,460
• Time in Patent Office: 798 Days
• Field of Search: 102/395, 102/430, 102/439, 102/444, 102/498, 102/501, 102/517, 102/519, 102/526, 102/529, 244/3.1, 244/3.23, 244/3.24
• US Class Current: 102/529
• CPC Class Codes: F42B 10/22 Projectiles of cannelured type
• CPC Class Codes: F42B 10/48 Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retardingF42B10/34 takes precedence
• CPC Class Codes: F42B 10/54 Spin braking means

Abstract

A training projectile that utilizes flutes or flats to augment roll damping characteristics and thereby cause the projectile to crossover into a gyroscopically unstable trajectory pattern at a predetermined time. Prior to the crossover, the training projectile maintains a gyroscopically stable trajectory, which enables extrapolation to ascertain the trajectory of a non-training projectile that does not have an augmented roll damping section. The unstable trajectory pattern substantially reduces the distance the training projectile can traverse, thereby reducing the amount of area required for a training range.

Claims

1. A spin-stabilizer projectile comprising:

an ogival nose portion;

a posterior portion; and

a midportion disposed between said nose portion and said posterior portion, said projectile defining an elongated, aerodynamically-shaped body having an axis of rotation;

said midportion comprising a longitudinally extending roll damping augmentation section disposed in a circumferential surface recess thereof, said roll damping augmentation section comprising a plurality of members which extend outwardly no more than about the depth of said recess and at least twice as high as the projectile boundary layer momentum height, for causing said projectile to become gyroscopically unstable at a predetermined range and continuously gyroscopically unstable thereafter .

2. The spin-stabilized projectile as described in claim 1 wherein said nose portion is substantially conical in shape throughout the axial dimension thereof.

3. The spin-stabilized projectile as described in claim 1, wherein said roll damping augmentation section members comprises a plurality of elongated juxtaposed flutes in said body and extending longitudinally between said nose portion and said posterior portion wherein the flutes extend outwardly no more than about the depth of said recess in said midportion.

4. The spin-stabilized projectile as described in claim 3 wherein the number of flutes is between 4 and 12.

5. The spin-stabilized projectile of claim 3 further comprising a series of slots of sufficient size for receiving a terminal portion of an associated flute.

6. The spin-stabilized projectile as described in claim 3 wherein the flutes extend radially outward perpendicular to the axis of rotation.

7. The spin-stabilized projectile of claim 1 wherein the roll damping section members are canted relative to the longitudinal axis in the direction of oncoming air.

8. The spin-stabilized projectile as described in claim 7, wherein the roll damping section members are canted at an angle between about 3°

and 5°

from the longitudinal axis in the direction of oncoming air.

9. The spin-stabilized projectile as described in claim 1, wherein said roll damping augmentation section members comprise a plurality of juxtaposed flats defining grooves formed in the body and extending longitudinally between the nose portion and the posterior portion, said flats extending outwardly approximately no higher than the depth of the recess in the midportion.

10. The spin-stabilized projectile as described in claim 9 wherein the number of flats is between 4 and 12.

11. The spin-stabilized projectile as described in claim 10, wherein the flats are spaced equi-distant around the circumference of the projectile.

12. The spin-stabilized projectile as described in claim 1, wherein the length of the roll damping augmentation section is up to 2.0 times the body diameter of the projectile;

and defines a plurality of air cavities each having a depth of between 3% and 7% of the body diameter of the projectile.

13. The spin-stabilized projectile as described in claim 1, wherein said roll damping augmentation section is disposed at the center of gravity of said projectile.

14. The spin-stabilized projectile as described in claim 1, wherein an obturation band is disposed between said roll damping augmentation section and said posterior portion.