ROCKET-BORNE INSTRUMENTATION TO DETERMINE AIR DENSITY BY RAYLEIGH-SCATTERED LIGHT,

Abstract

Based on an earlier feasibility study, a rocket-borne system to measure air density by detecting Rayleigh-scattered light from an onboard light source was developed and flown on a Nike-Iroquois sounding rocket. The system utilized a high intensity mercury arc producing a modulating light beam. Light scattered from air molecules in a portion of the light beam beyond the rocket shock wave was viewed by an optical system. The light receiver output was amplified, synchronously detected, and was telemetered to ground by standard IRIG FM/FM telemetry. Details of the instrumentation are presented and preliminary flight results are discussed. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0675607

Entities

People

  • J. Irvin Swigart
  • L. Carl Howlett

Organizations

  • University of Utah

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Feasibility Studies
  • Instrumentation
  • Intensity
  • Light Sources
  • Molecules
  • Rockets
  • Shock
  • Shock Waves
  • Sounding Rockets
  • Standards
  • Telemetry

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Optical Physics and Photonics.