Effect of electromagnetic launch on armature/sabot discard

IEEE Transactions on Magnetics

Volumn 37, Issue 1 I, 2001, Pages 67-72

  Erengil, Mehmet E ^a   Zielinski, Alexander E ^b  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

^b U S ARMY RESEARCH LABORATORY   (United States)

Author keywords

Accuracy; Aeroballistics; Armature sabot discard; Electrodynamics

Indexed keywords

ACCELERATION; DECELERATION; PROJECTILES; TRAJECTORIES;

ARMATURE; ELECTROMAGNETIC LAUNCH; SABOT DISCARD;

ELECTROMAGNETIC LAUNCHERS;

EID: 0035035799     PISSN: 00189464     EISSN: None     Source Type: Journal    
DOI: 10.1109/20.911793     Document Type: Article

References (11)

1. Aerodynamic interference during sabot discard
2. Intermediate ballistics model for hypervelocity projectiles launched from EM guns
3. An investigation of the ballistic performance for an electromagnetic gun-launched projectile
4. Electromagnetic and aeromechanical analysis of sabot discard for railgun projectiles
5. Projectile/sabot discard aerodynamics
6. Wind tunnel measurements of sabot discard aerodynamics
7. Computation of sabot discard
8. A numerical and experimental investigation of sabot separation dynamics
9. Pressure distribution on sabots in hypervelocity flight
10. An aerodynamic model for symmetric sabot separation
11. IAT report