Flight measurements of low velocity bow shock ultraviolet radiation

Peter W. Erdman, Edward C. Zipf, Patrick Espy, Carl Howlett, Deborah A. Levin, Richard Loda, Robert J. Collins, Graham V. Candler

Research output: Contribution to conferencePaper

Abstract

The ultraviolet spectrum, atomic oxygen 130. 4nm radiation intensity, total plasma density, and electron temperature of a Mach 12 bow shock was obtained by a sounding rocket experiment launched from the Wallops Flight Facility on April 25, 1990, at 12:32 AM EST. A two-stage, Terrier Malamute rocket, which attained an apogee of 720 km, was used in this experiment. Optical data in the 200-400 nm wavelength range were obtained from 37 to 75 km at a vehicle velocity of 3. 5 km/sec. Electron probe and VUV OI 130. 4nm measurements were obtained near nose cone ejection at 37 km.

Original languageEnglish (US)
StatePublished - Jan 1 1991
EventAIAA 26th Thermophysics Conference, 1991 - Honolulu, United States
Duration: Jun 24 1991Jun 26 1991

Other

OtherAIAA 26th Thermophysics Conference, 1991
CountryUnited States
CityHonolulu
Period6/24/916/26/91

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ASJC Scopus subject areas

  • Mechanical Engineering
  • Aerospace Engineering

Cite this

Erdman, P. W., Zipf, E. C., Espy, P., Howlett, C., Levin, D. A., Loda, R., Collins, R. J., & Candler, G. V. (1991). Flight measurements of low velocity bow shock ultraviolet radiation. Paper presented at AIAA 26th Thermophysics Conference, 1991, Honolulu, United States.