Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

Autonomous Optical Sensor System for the Monitoring of Nitrogen Dioxide from Aging Rocket Propellant

Technical Report ·
DOI:https://doi.org/10.2172/787637· OSTI ID:787637

An optical sensor system has been developed for the autonomous monitoring of NO{sub 2} evolution in energetic material aging studies. The system is minimally invasive, requiring only the presence of a small sensor film within the aging chamber. The sensor material is a perylene/PMMA film that is excited by a blue LED light source and the fluorescence detected with a CCD spectrometer. Detection of NO{sub 2} gas is done remotely through the glass window of the aging chamber. Irreversible reaction of NO{sub 2} with perylene, producing the non-fluorescent nitroperylene, provides the optical sensing scheme. The rate of fluorescence intensity loss over time can be modeled using a numerical solution to the coupled diffusion and a nonlinear chemical reaction problem to evaluate NO{sub 2} concentration levels. The light source, spectrometer, spectral acquisition, and data processing were controlled through a Labivew program run by a laptop PC. Due to the long times involved with materials aging studies the system was designed to turn on, warm up, acquire data, power itself off, then recycle at a specific time interval. This allowed the monitoring of aging HE material over the period of several weeks with minimal power consumption and stable LED light output. Despite inherent problems with gas leakage of the aging chamber they were able to test the sensor system in the field under an accelerated aging study of rocket propellant. They found that the propellant evolved NO{sub 2} at a rate that yielded a concentration of between 10 and 100 ppm. The sensor system further revealed that the propellant, over an aging period of 25 days, evolves NO{sub 2} with cyclic behavior between active and dormant periods.

Research Organization:
Sandia National Labs., Albuquerque, NM (US); Sandia National Labs., Livermore, CA (US)
Sponsoring Organization:
US Department of Energy (US)
DOE Contract Number:
AC04-94AL85000
OSTI ID:
787637
Report Number(s):
SAND2001-2953
Country of Publication:
United States
Language:
English

Similar Records

FAILURE MECHANISMS OF SOLID PROPELLANT ROCKET NOZZLES
Journal Article · Thu Jan 14 23:00:00 EST 1960 · American Ceramic Society Bulletin (U.S.) · OSTI ID:4207077

Explosive laser light initiation of propellants
Patent · Thu Dec 31 23:00:00 EST 1992 · OSTI ID:868789

Explosive laser light initiation of propellants
Patent · Tue May 18 00:00:00 EDT 1993 · OSTI ID:6252121