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Ultrasonic Technique Resolution For Solid Propellant Burning Rate Measurement
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Book Synopsis Ultrasonic Technique Resolution for Solid Propellant Burning Rate Measurement by : William W. McQuade
Download or read book Ultrasonic Technique Resolution for Solid Propellant Burning Rate Measurement written by William W. McQuade and published by . This book was released on 1998 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Uncertainty Analysis of the Ultrasonic Technique Applied to Solid Propellant Burning Rate Measurement by : Frederic-Thomas Dauch
Download or read book Uncertainty Analysis of the Ultrasonic Technique Applied to Solid Propellant Burning Rate Measurement written by Frederic-Thomas Dauch and published by . This book was released on 1999 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Demonstration of an Ultrasonic Technique to Measure Solid Propellant Burning Rates Under Actual Combustion Conditions by : Hubbert Jackson Hale
Download or read book The Demonstration of an Ultrasonic Technique to Measure Solid Propellant Burning Rates Under Actual Combustion Conditions written by Hubbert Jackson Hale and published by . This book was released on 1967 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Ultrasound Measurements of Solid Propellant Burning Rates by : Jeffrey J. Murphy
Download or read book Ultrasound Measurements of Solid Propellant Burning Rates written by Jeffrey J. Murphy and published by . This book was released on 1998 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Development of an Ultrasonic Burning Rate Measurement Technique by : P.-K. Wu
Download or read book Development of an Ultrasonic Burning Rate Measurement Technique written by P.-K. Wu and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurement of Solid Propellant Burning Rates in a Slab-motor Environment Using a Microwave Technique by : Joseph Joshua Kliger
Download or read book Measurement of Solid Propellant Burning Rates in a Slab-motor Environment Using a Microwave Technique written by Joseph Joshua Kliger and published by . This book was released on 1984 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Evaluation of Methods for Solid Propellant Burning Rate Measurement by :
Download or read book Evaluation of Methods for Solid Propellant Burning Rate Measurement written by and published by . This book was released on 2002 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The NATO Research and Technology Organization (RTO), Advanced Vehicle Technology (AVI), Working Group (WG) 016 (formerly AGARD/PEP Working Group (27) undertook to evaluate methods in use within the NATO propulsion community to measure burning rate in solid propellant rocket systems, with the purpose of identifying similarities and differences between the participating nations. This WG was formed in 1996, consisting of active representatives from 6 of the 15 member nations of NATO, with inputs accepted from 4 other member nations and a couple non-member nations. The NATO RTO/AVT WG 016 sought to contribute to improvements in the burning rate tools to address issues that have plagued the solid propulsion industry for over 40 years. This paper reviews the final results of this study by summarizing the objectives, approach, findings, and recommendations of this working group based on activity from October 1997 to March 2001. Recommendations are reviewed on direct and non-intrusive burning rate measurement methods, data analysis, and performance scaling to support improved prediction of internal ballistics of a full-scale solid propellant motor. AVT WG 016 activities have identified that manufacturer burning rate data may not easily be compared without accounting for industry-wide differences in subscale devices, test methods and scaling analysis methods. The WG recommends the NATO propulsion community review these findings as a means of advancing their own burning rate measurement and analysis methods.
Book Synopsis Review of Ultrasonic Technique for Steady State Burning Rate Measurements by : Robert A. Frederick
Download or read book Review of Ultrasonic Technique for Steady State Burning Rate Measurements written by Robert A. Frederick and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Evaluation of Methods for Solid Propellant Burning Rate Measurements by :
Download or read book Evaluation of Methods for Solid Propellant Burning Rate Measurements written by and published by . This book was released on 2002 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 2000-3800 - 2000-3849 by :
Download or read book 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 2000-3800 - 2000-3849 written by and published by . This book was released on 2000 with total page 574 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Nonsteady Burning and Combustion Stability of Solid Propellants by : Martin Summerfield
Download or read book Nonsteady Burning and Combustion Stability of Solid Propellants written by Martin Summerfield and published by AIAA. This book was released on 1992 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Solid propellant burning rate measurement in a closed bomb by : Alvars Celmins
Download or read book Solid propellant burning rate measurement in a closed bomb written by Alvars Celmins and published by . This book was released on 1975 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 10-13 July 2005, Tucson, Arizona: 05-3600 - 05-3649 by :
Download or read book 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 10-13 July 2005, Tucson, Arizona: 05-3600 - 05-3649 written by and published by . This book was released on 2005 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Laser Scanning Technique for Measuring Solid Propellant Burning Rates by : Heng Hok
Download or read book A Laser Scanning Technique for Measuring Solid Propellant Burning Rates written by Heng Hok and published by . This book was released on 1999 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Solid Propellant Burning Rate Measurement in a Closed Bomb by :
Download or read book Solid Propellant Burning Rate Measurement in a Closed Bomb written by and published by . This book was released on 1975 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experiments show that the burning rate of solid propellants is a function of the pressure under which the burning takes place. An often used method to determine that burning rate function is to burn a sample of the propellant in a closed container and to register the corresponding pressure-time data. With the aid of formulas from thermodynamic theory these observations can be manipulated to yield the desired parameters of the burning rate function. This analysis is typically done under a number of restrictive assumptions, e.g., the assumption of constant temperature in the container throughout the experiment. In spite of such assumptions the corresponding algorithms published are complicated and an error analysis of the results has apparently never been reported. In the present paper new formulas are derived under relaxed assumptions. With the aid of these formulas the data analysis is reduced to a curve fitting task. For such tasks standard theories and computer programs are available, which furnish the unknown parameters of the burning rate function together with estimates of their variances and co-variances. The new formulas can be replaced by simpler ones under conditions, which are controllable by the design of the experiment. It is found that for such simplifications the temperature's behavior is not relevant. In general the simplifications are permissible if the maximum pressure achieved during the experiment remains essentially smaller than the chemical energy released per unit volume of the propellant. The latter is typically of the order of 10 to 10th power Pa (10 to 5th power). An example illustrates the application of the new algorithm.
Book Synopsis Continuous Measurement of Solid Propellant Burning Rate in a Rocket Motor by : C.F. Yin
Download or read book Continuous Measurement of Solid Propellant Burning Rate in a Rocket Motor written by C.F. Yin and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurement of Solid Propellant Burning Rates During Rapid Depressurization by : Albert Thurston Clary
Download or read book Measurement of Solid Propellant Burning Rates During Rapid Depressurization written by Albert Thurston Clary and published by . This book was released on 1971 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt: A microwave continuous measurement technique has been used to measure burning rates of a carboxyl-terminated polybutadiene and ammonium perchlorate composite solid propellant during rapid decompression. A microwave signal oscillating at a known source frequency is passed through the end of a burning propellant strand opposite the burning surface and allowed to reflect off the burning surface. By continuously comparing the phase angle of this reflected signal with the phase angle of another signal oscillating at the orginal source frequency, a relative phase angle of another signal oscillating at the original source frequency, a relative phase angle between the two signals is obtained. The rate of change of this relative phase angle with time is proportional to the propellant's burning rate. Possible errors were investigated and conclusions reached concerning them. (Author).