Experimental determination of sold) propellant combustion response

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Disalvo, R ^a   Frederick, R A ^a   Moser, M D ^a  

^a UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOMBS (ORDNANCE); NITROGEN; PRESSURIZATION; PROPELLANTS; PROPULSION; SOLID PROPELLANTS; TRANSIENTS; ULTRASONIC APPLICATIONS;

COMBUSTION RESPONSE; DIRECT MEASUREMENT; EXPERIMENTAL DETERMINATION; PRESSURE MODULATIONS; PRESSURIZATION RATES; REASONABLE ACCURACY; REDUCTION TECHNIQUES; ULTRASONIC DIAGNOSTICS;

DATA REDUCTION;

EID: 84963804486     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Finlinson, Jerry C., “Laser Recoil Response of HMX, RDS, N5, GAP/BTTN and Others from 1 to 6 Atmospheres,” AIAA Paper 97-0698, 1997.
2. R.S. Brown, I.E. Erikson, and W.R. Babcock, “Combustion Response Function Measurements by the Rotating Valve Method,” AIAA Journal, Vol.12, No. 11, Nov. 1974.
3. Kuentzmann, P. and Nadaud, L., “Reponse des Propergols Solides aux Oscillations de Pression et de Vitesse,” Combustion Science and Technology, Vol. 11, 1975, pp. 119-139.
4. Cauty, Franck, “Solid Propellant Combustion Response Function from Direct Measurement Methods: A Review of ONERA Experience,” Office National d’Etudes et de Recheches Aerospatiales (ONERA).
5. Personal Communication with F. Cauty, January 1998.
6. McQuade, W. W., “Ultrasonic Technique Resolution for Solid Propellant Burning Rate Measurement,” Master’s Thesis, The University of Alabama in Huntsville, Huntsville Al, 1998.