A Superconducting Magnet Dewar Missile for Launching in Ballistic Ranges

Abstract

One concept for magnetic guidance of projectiles in hypervelocity ballistic ranges is the use of a superconducting magnet within the projectile. The magnet must survive the large launch loads (250,000 g's) necessary to achieve test velocities (20,000 ft/sec). This report describes a conceptual design of a dewar which contains a superconducting magnet and its performance limitations. Thermal holding time for the preposed dewar would be in excess of 90 min. Structural strength aspects of the dewar components limit the launch load to 15,000 g's. consequently the current launcher at AEDC (50 ft long) would be limited to velocities of about 5,000 ft/sec or alternatively, an 830- ft-long launcher would be required to produce the desired velocity (20,000 ft/ sec). The use of new launch techniques or magnet configurations could affect these results.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1976
Accession Number
ADA021957

Entities

People

  • E. E. Erickson

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Elastic Properties
  • Government Procurement
  • Governments
  • Heat Capacity
  • Heat Energy
  • Heat Transfer
  • Launch Tubes
  • Launchers
  • Launching
  • Magnetic Guidance
  • Magnets
  • Modulus Of Elasticity
  • Superconducting Magnets
  • Tennessee
  • Thermal Conductivity
  • United States

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Missile Defense Systems.
  • Superconducting Magnet Technology

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow