Ultrasonic measurement of solid propellant burning rate
Abstract
Considering the inadequacy of current methods for measuring the burning rate of solid propellants, an ultrasonic device has been developed that measures the grain thickness at a rate up to 5000 Hz. Satisfactory results have been obtained on specimens up to 40 mm thick in steady or slowly varying conditions, such as erosive combustion. Composite, double base and autopyrolyzing propellants have been tested in various temperature and pressure conditions, and intermediate materials between grain and transducer have been determined. The precision during fast transient phases or unsteady combustion is still wanting, but this drawback may be overcome by further studies, especially on signal processing.
- Publication:
-
La Recherche Aerospatiale
- Pub Date:
- February 1979
- Bibcode:
- 1979ReAer.......55K
- Keywords:
-
- Burning Rate;
- Solid Propellant Combustion;
- Solid Rocket Propellants;
- Ultrasonic Spectroscopy;
- Ultrasonic Wave Transducers;
- Acoustic Impedance;
- Composite Propellants;
- Couplings;
- Double Base Rocket Propellants;
- Emission Spectra;
- Impulse Generators;
- Plastics;
- Signal Processing;
- Thickness;
- Thyristors;
- Transducers;
- Instrumentation and Photography