A facility for solid-propellent response measurements under pressure-driven conditions

Measurement Science and Technology

Volumn 11, Issue 1, 2000, Pages 51-58

  Lee, Young Joo ^a   Kudva, Gautam N ^a   Litzinger, Thomas A ^a  

^a The Pennsylvania State University   (United States)

Author keywords

Amplitude and phase information; Force transducer; Miniature load cell; Pressure driven facility, combustion instability; Solid propellants; Thrust response

Indexed keywords

ATMOSPHERIC PRESSURE; CERAMIC MATERIALS; COMBUSTION; MACHINE VIBRATIONS; MATHEMATICAL MODELS; PRESSURE EFFECTS; SIGNAL TO NOISE RATIO; SOLID PROPELLANTS; ULTRASONIC TRANSDUCERS;

ACOUSTIC DRIVER SYSTEMS; SOLID PROPELLANT RESPONSE MEASUREMENT;

ROCKET ENGINES;

EID: 0033703643     PISSN: 09570233     EISSN: None     Source Type: Journal    
DOI: 10.1088/0957-0233/11/1/308     Document Type: Article

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