Published January 1991 | Version v1
Journal article

Design limitations for small caliber electromagnetic saboted rod projectiles

  • 1. Army Armament Research and Development Command, Aberdeen Proving Ground, MD (United States). Ballistics Research Lab.

Description

In any application of electromagnetic launch, the armature package must conform to the barrel and provide the desired terminal performance. Finned long rod projectiles have proven to be viable candidates for both flight bodies and terminal effectiveness. This paper describes the criteria necessary for integrating a solid armature with a conventional type finned rod. An initial design is presented for a rod projectile, launched from a 15.24 mm (.60 caliber) augmented railgun with a sinusoidal driving current. Other designs are assessed in order to explore improvements and scalability to other bore diameters. The authors evaluate the final armature design considering: launch, flight, and terminal effects. ohmic heating, structural limitations, and barrel parameters are also discussed. Flight and aerodynamic data are scaled from existing finned rod projectile data bases to calculate horizontal flat-trajectory performance. Finally, terminal effects are incorporated for a simple rolled homogeneous armor (RHA) target

Additional details

Publishing Information

Journal Title
IEEE Transactions on Magnetics
Journal Volume
27
Journal Issue
1
Series
IEEE Trans. Magn.
Journal Page Range
521-526
ISSN
0018-9464
CODEN
IEMGA

Conference

Title
5. IEEE symposium on electromagnetic launcher technology.
Dates
1-5 Apr 1990.
Place
Destin, FL (United States).

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
23051866
Subject category
S70: PLASMA PHYSICS AND FUSION TECHNOLOGY;
Resource subtype / Literary indicator
Conference
Descriptors DEI
AERODYNAMICS; ARMATURES; DESIGN; ELECTROMAGNETIC RADIATION; PLASMA ACCELERATION; PROJECTILES; RAILGUN ACCELERATORS; RODS; SPACE FLIGHT; TARGETS
Descriptors DEC
ACCELERATION; ELECTRICAL EQUIPMENT; EQUIPMENT; FLUID MECHANICS; IMPACT FUSION DRIVERS; MECHANICS; RADIATIONS

Optional Information

Secondary number(s)
CONF-9004136--.