Accession Number:

ADA482455

Title:

Design and Analysis of a Composite Tailcone for the XM-1002 Training Round

Descriptive Note:

Final rept. Mar 2004-Apr 2005

Corporate Author:

ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD WEAPONS AND MATERIALS RESEARCH DIRECTORATE

Report Date:

2008-04-01

Pagination or Media Count:

84.0

Abstract:

A long-fiber thermoplastic LFT composite XM-1002 tailcone has been designed and fabricated to explore the technical feasibility of substituting aluminum-machined tailcones with low-cost, fiber-reinforced polymer tailcones. The design phase of the project involved developing a material model and numerically evaluating the stresses on the projectile using a simulated launch environment. A detailed ANSYS-based finite element analysis FEA was undertaken to investigate the behavior of the LFT tailcone compared to the existing aluminum version for various fiber loading. In the analysis, the tailcone was subjected to a variety of mechanical- and thermal-loading conditions. This report summarizes the detailed design and FEA of two versions of the XM-1002 composite tailcone. These are referred to as hollow-back and filled-back. For the hollow-back geometry, the objective was to mimic the external geometry of the presently used aluminum tailcone. The hollow-back tailcone was further investigated for two metal insert geometries, beaded and threaded. Weight reduction with respect to the all-metal aluminum version of the tailcone is not desirable hence a metal insert was used in conjunction with the LFT material. Three conditions with respect to the firing of a projectile have also been discussed in-bore, transition, and out-of-bore. The response of the LFT composite tailcone to pressure, gravitational load, and temperature has been evaluated. The testing trial held at Aberdeen Proving Ground, MD, demonstrated that the LFT filled-back glassnylon tailcone with 40 glass loading successfully passed the firing conditions. By implementing the proposed LFT composite tailcone, significant cost savings are projected compared to the existing aluminum version.

Subject Categories:

  • Laminates and Composite Materials
  • Plastics
  • Ammunition and Explosives
  • Mechanics
  • Thermodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE