Ultraviolet/Visible Spectral Radiance for the Bow Shock of a Projectile Launched at High Velocities in the AEDC Track G Facility

Abstract

An optical arrangement and detector gating scheme for viewing the bow shock spectral radiation from projectiles launched in a hypervelocity ballistic range are reported. Velocities were about 18,000 fps. Range pressure was 49 torr of dried air. A 0.32-m grating spectrometer with a linear array optical detector was used. Gating times of 275 and 100 microsec were employed to view nose cap radiation during the projectile's flight. The spectrum was dominated by a strong continuum in the visible with molecular band structure superimposed on it. The most dominant radiators in the UV were identified as the NO y bands and OH.N2 + First Negative, N2 Second Positive, CN, and NH were identified as emitters in the near-UV and VIS. In addition, there were many unidentified radiators in the VIS.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1991
Accession Number
ADA236503

Entities

People

  • K. L. Dietz
  • W. K. Mcgregor

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Advanced Electronics
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Arrays
  • Band Structures
  • Bow Shock
  • Detectors
  • Electrons
  • Energy Bands
  • Linear Arrays
  • Measurement
  • Nose Caps
  • Noses
  • Optical Detectors
  • Radiance
  • Radiation
  • Shock
  • Spectra

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Sensor Fusion and Tracking Systems.
  • Spectroscopy.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow