Spin-damped training round with selectable safety trace

• US 4,905,602 A
• Filed: 05/23/1988
• Issued: 03/06/1990
• Est. Priority Date: 04/29/1986
• Status: Expired due to Fees

• Current Assignee: Royal Ordnance
• Original Assignee: Royal Ordnance
• Inventors: Buckland, Roy W.
• Primary Examiner(s): Tudor, Harold J.
• Application Number:
  US07/199,366
• Time in Patent Office: 652 Days
• Field of Search: 102/395, 102/498, 102/444, 102/445, 102/501, 102/517, 102/520-523, 102/529, 244/3.1, 244/3.24-3.3
• US Class Current: 102/520
• CPC Class Codes: F42B 10/54 Spin braking means

Abstract

High velocity projectiles are able to continue in flight for considerable distances beyond the normal target range. The present invention is a projectile for use in practice firing which becomes unstable after the normal target range has been exceeded and comprises a training round (1) having a body portion (3) engageable with a sabot (4) for projection from a rifled gun barrel, and a tapered nose portion (2) protrusive beyond the sabot, which is provided with a nose tip portion (6) having spin fins (9) extending in planes radial to the longitudinal axis. The fins increase the rate of spin decay and cause instability of the round and the fin geometry is chosen such that the instability occurs when the target range has been exceeded. The finned nose tip portion is separable from the round so as to permit selective attachment of a nose tip portion having fins specifically dimensioned for terminating the trajectory at a chosen safety range.

Claims

1. A training round of ammunition having a longitudinal axis, comprising:

a discarding sabot; and

a sub-caliber projectile engaged partially within an open region within said sabot and having a body portion with a tapered nose portion protruding out of said sabot through an aperture in one end of said open region of said sabot in a direction of intended flight of said projectile, said nose portion including a nose tip portion having an axially symmetric array of spin damping fins each of which is oriented substantially within a plane extending radially of said longitudinal axis and extends radially to an extent not radially beyond the diameter of said aperture, said spin damping fins thereby not protruding radially from said body portion at any point within said sabot, said projectile further including an attachment means for mechanically attaching said nose tip portion with a remaining portion of said body portion to enable said nose tip portion to be attached and detached from said remaining portion, whereby a plurality of different nose tip portions having different spin damping characteristics can be selectively attached and detached to said remaining portion of said body portion.

2. A training round as claimed in claim 1 wherein said attachment means comprises mating end faces of the nose tip portion and the nose portion, said end faces being oriented transverse to the longitudinal axis and respectively provided with a threaded axial spigot and a corresponding threaded axial recess comprising the inter-engageable attachment means.

3. A training round as claimed in claim 1 wherein the spin damping fins are tapered and chamfered at their edges which face forwardly in said intended direction of flight.

4. A training round as claimed in claim 1 wherein the nose tip portion has four spin damping fins extending at mutual right angles.

5. A training round as claimed in claim 3 and wherein the ratio of the surface area of a single side of each fin expressed in mm² to the maximum diameter of the sub-projectile expressed in mm² is not greater than 6.0.