Impact projectile assembly

• US 4,516,502 A
• Filed: 02/01/1983
• Issued: 05/14/1985
• Est. Priority Date: 02/27/1982
• Status: Expired due to Fees

• Current Assignee: Rheinmetall GmbH
• Original Assignee: Rheinmetall GmbH
• Inventors: Bocker, Jurgen, Gersbach, Klaus, Glotz, Gerhard, Klein, Klaus-Walter
• Primary Examiner(s): Tudor, Harold J.
• Application Number:
  US06/462,902
• Time in Patent Office: 833 Days
• Field of Search: 102/514-519, 102/520-523, 102/703, 102/338, 102/489, 102/501, 102/503, 244/3.1
• US Class Current: 102/523
• CPC Class Codes: F42B 12/06 with hard or heavy core; Kinetic energy penetrators F42B12/16, F42B12/74 take precedence
• CPC Class Codes: F42B 12/16 in combination with an additional projectile or charge, acting successively on the target see also F42B12/625
• CPC Class Codes: F42B 12/625 a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other with shaped or hollow charges F42B12/16
• CPC Class Codes: F42B 14/061 Sabots for long rod fin stabilised kinetic energy projectiles, i.e. multisegment sabots attached midway on the projectile
• CPC Class Codes: F42B 14/065 Sabots carrying several projectiles
• CPC Class Codes: F42B 5/03 containing more than one missile
• CPC Class Codes: Y10S 102/703 Flechette

Abstract

A subcaliber projectile assembly especially for attack against active armor has an enabling projectile disposed axially ahead of a main projectile and in line and in end-to-end relationship therewith in a common sabot. The fin structures of the two projectiles are designed to increase the resistance of the main projectile so that it is retarded relative to the enabling projectile and strikes the target only after the enabling projectile has depleted at least one level of defense along the line of attack.

Claims

1. A subcaliber projectile assembly for firing from a barrel-type weapon to attack a multilayer armored target, comprising:

an elongated sabot comprising a plurality of axially extending segments separable along axial planes, said segments defining a recess close to a leading air-catching end of the sabot;

a relatively small inertial enabling projectile received in said end of said sabot and having a fin stabilizer received in said recess;

a relatively large main inertial subsequently attacking projectile received in said sabot behind said enabling projectile and having a fin stabilizer disposed rearwardly of said sabot, said segments and the periphery of said main projectile being formed with mating formations enabling entrainment of said main projectile with said sabot until said segments of said sabot separate, said projectiles having aerodynamic configurations such that said enabling projectile reaches said target ahead of said main projectile; and

at least one band surrounding said segments for releasably retaining same against said projectiles and holding said formations in mutual engagement.

2. The projectile assembly defined in claim 1 wherein the trailing end of said enabling projectile is formed with a recess form-fittingly receiving a nose at the leading end of said subsequently attacking projectile.

3. The projectile assembly defined in claim 2 wherein said sabot is a pull sabot.

4. The projectile assembly defined in claim 2, further comprising means for retarding the flight of said subsequently attacking projectile relative to said enabling projectile to establish a time-spaced sequence of attack of said projectile on said target.

5. The projectile assembly defined in claim 4 wherein the last mentioned means includes means for imparting different aerodynamic resistances to said projectiles.

6. The projectile assembly defined in claim 5 wherein said different aerodynamic resistances are the result of different configurations of said fin structures.