| OCR Text |
Show 81 driven the of intensity combustion corrected transducer signal in real time, tended surface was the non-planar maintained for non-flat surface was to course of each as an inhibitor grease, long enough that An or two The loss of a to transducer and Honeywell determine the and burning tions, it rate was not the Time about 0.5 photo second, . a fairly The effects of flat the halocarbon, Kel-F #90 consistent, meaningful data the suggested signal amplitude during effectively postponed pressure, a of use the The strand surface one seconds. of as one regressed, although cause test. of it burning propellants, r of averaging time as very fast use plotted chosen for the data reduction. was become to determined and were by theoretical considerations. Average values signal. diode the were em/sec signal Model Delay Correlator, the of coning obtained. at were 9410, correlation coefficient between the sample For atmospheric processed by in attempt an applied flux However, because of equipment limita response. possible to obtain uniform signals of long enough duration to determine accurate correlations. The phase angle between the also measured. A AD-YU Model 405 chart recorder for direct phase angles determined signal quality, although high an signal and phase analog output error the P.D. coupled meter used. was to Because of confidence could be ±10 of the degrees placed in signal was strip a The resultant propellant were plotted for each by theoretical considerations. poor K.U. short test as suggested times and existed in these data the trends observed. |
