caa a22 4500 475810074 CHVBK 20180406123756.0 cr unu---uuuuu 170329e20000101xx s 000 0 eng 10.1007/BF02701517 doi (NATIONALLICENCE)springer-10.1007/BF02701517 Consistent definitions for burning-rate measurement in solid-rocket motors [Elektronische Daten] [R. Hessler, R. Glick] Inherent problems in burning-rate measurement in small solid-rocket motors are discussed in terms of subfactors comprising an overall absolute scale factor. A set of data-analysis definitions for burning-rate measurement that is consistent with bulk-mode theory governing pressure in solid-rocket motors is presented. The procedure using these definitions specifically treats the effects of variable exponent, noninstantaneous burnout, mean propellant shrinkage, hardware variations, and nonneutral pressure to reduce bias and scatter in measured burning rates. The present procedure does not address the effects of heat losses, formulation gradients, or nonequilibrium burning. Application of the procedure on motor data is discussed briefly. Kluwer Academic/Plenum Publishers, 2000 Hessler R. 35670, Somerville, AL, USA aut Glick R. 47978, Rensselaer, IN, USA aut Combustion, Explosion and Shock Waves Springer US 36/1(2000-01-01), 76-95 0010-5082 36:1<76 2000 36 10573 https://doi.org/10.1007/BF02701517 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF02701517 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Hessler R. 35670, Somerville, AL, USA aut NATIONALLICENCE 700 1- Glick R. 47978, Rensselaer, IN, USA aut NATIONALLICENCE 773 0- Combustion, Explosion and Shock Waves Springer US 36/1(2000-01-01), 76-95 0010-5082 36:1<76 2000 36 10573 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer