Development of a Rocket Motor Burn Rate Measurement System

The technique chosen to develop into a microwave burn rate sensor was that of the microwave interferometer. Microwave engery is beamed through a 'window' in the rocket motor case and into the propellant. At the burning propellant surface, this microwave energy is reflected and beamed back...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Schuemann,W. C, Zajdel,L. S, Rice,J. H
Format:	Report
Sprache:	eng
Schlagworte:	BURNING RATE CAPTIVE TESTS Combustion and Ignition COMPUTER AIDED ANALYSIS INTERFEROMETERS MEASUREMENT MICROWAVE EQUIPMENT Solid Rocket Propellants T BURNERS TEST METHODS THERMAL ANALYSIS WAVEGUIDE WINDOWS
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