Raman Hydrogen Sensor, Phase 1

Abstract

A fast-response (0.25 sec or faster) gaseous hydrogen (H2) sensor is required in process air ducting at AEDC to support the testing of engines for the National Aerospace Plane. A sensitivity of around 0.1% H2, over a sample pressure range of 2 to 15 PSIA is desired at humidity levels of up to 20% by weight. In the Phase I Raman Hydrogen Sensor Program, Spectral Sciences, Inc. (SSI) has built and tested a breadboard laser Raman scattering instrument for H2 concentration monitoring, and has demonstrated the feasibility of building a practical instrument that will meet the requirements of AEDC. All of the technical objectives were successfully accomplished. A detection limit of 0.0013 atm of H2 using 18 mW of optical power was demonstrated, and the fundamental response time was found to be 0.3 sec at 1 atm with the current, non-optimized flow system. In addition, the feasibility of active subtraction of background water signals was demonstrated, and a conceptual design for a Phase II brassboard instrument was also developed.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1991
Accession Number
ADA273783

Entities

People

  • Jung‐Hee Lee
  • S. M. Adler-golden

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Sensors

DTIC Thesaurus Topics

  • Accuracy
  • Air Cooled
  • Argon Lasers
  • Bandpass Filters
  • Detection
  • Detectors
  • Electronics
  • Hydrogen Sensors
  • Ion Lasers
  • Laser Beams
  • Lasers
  • Measurement
  • Raman Scattering
  • Separators
  • Signal Processing
  • Test Facilities
  • Water Vapor

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Software Engineering
  • Spectroscopy.

Technology Areas

  • Directed Energy
  • Space
  • Space - Hall-Effect Thruster