Closed-bomb Combustion of Hivelite-based Very High Burn Rate (VHBR) Propellant

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ISBN 13 :
Total Pages : 117 pages
Book Rating : 4.:/5 (817 download)

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Book Synopsis Closed-bomb Combustion of Hivelite-based Very High Burn Rate (VHBR) Propellant by : Calspan Corporation

Download or read book Closed-bomb Combustion of Hivelite-based Very High Burn Rate (VHBR) Propellant written by Calspan Corporation and published by . This book was released on 1985 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Closed-Bomb Combustion of Hivelite-Based, Very High Burn Rate (VHBR) Propellant

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Publisher :
ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Closed-Bomb Combustion of Hivelite-Based, Very High Burn Rate (VHBR) Propellant by : E. B. Fisher

Download or read book Closed-Bomb Combustion of Hivelite-Based, Very High Burn Rate (VHBR) Propellant written by E. B. Fisher and published by . This book was released on 1985 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the combustion characteristics of a Hivelite-based, very-high-burn-rate (VHBR) propellant was conducted. The experiments were performed in a closed chamber, called the VHBR bomb, that was specially designed and constructed for these experiments. The device was designed with the same diameter as the propellant samples in order to maintain one dimensional combustion processes and transient wave phenomena to simplify subsequent interpretation and analysis. Propellant combustion was characterized by a low burn rate (about 1 m/s) until a pressure in the vicinity of 15-20 MPa is reached. After this pressure, which may represent the propellant crushing or break pressure, the combustion rate accelerated to levels from 10 to 180 m/s, depending on other test parameters. Tests conducted at different loading densities indicated that combustion rate was a strong function of pressure. Variation of sample weight at constant loading density demonstrated that increasing the amount of unburned propellant at the time the break pressure was reached also causes burn rate and thrust to increase. A coating that makes the outside surface of the sample slippery tended to reduce the apparent burn rate but use of a coating which retarded transmission of gas pressure along the periphery of the sample increased the apparent burn rate as well as thrust. Change of mounting interface properties caused significant differences in the dynamic characteristics leading to increased thrust.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 828 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1985 with total page 828 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Gun Propulsion Technology

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Publisher : AIAA (American Institute of Aeronautics & Astronautics)
ISBN 13 :
Total Pages : 600 pages
Book Rating : 4.X/5 (1 download)

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Book Synopsis Gun Propulsion Technology by : Ludwig Stiefel

Download or read book Gun Propulsion Technology written by Ludwig Stiefel and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1988 with total page 600 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Abstract Bulletin

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Publisher :
ISBN 13 :
Total Pages : 172 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1981 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Thrust Characterization of Very High Burning Rate Propellants

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ISBN 13 :
Total Pages : 61 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Thrust Characterization of Very High Burning Rate Propellants by : I. W. May

Download or read book Thrust Characterization of Very High Burning Rate Propellants written by I. W. May and published by . This book was released on 1984 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of closed bomb combustion tests were conducted on several very high burning rate (VHBR) propellants in which, in addition to the standard pressure measurements, the thrust produced by a burning propellant column was measured using a dynamic force gage located at the end of the propellant column. The results indicate that in several instances the total force imparted to the force gage substantially exceeded that due to the gas pressure alone. The difference is ascribed to the thrust or impulse resulting from very high apparent burning rates. In fact, an analysis of the data for two VHBR propellants indicates that effective burning rates from 100 to 300 m/s are required to produce the observed thrust levels. Such burning rates are not yet explainable by conventional combustion models. Additional physical processes such as convective flamespread or stress-induced surface fracture must be invoked to explain such high apparent burning rates.

Annual Department of Defense Bibliography of Logistics Studies and Related Documents

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ISBN 13 :
Total Pages : 1210 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Annual Department of Defense Bibliography of Logistics Studies and Related Documents by : United States. Defense Logistics Studies Information Exchange

Download or read book Annual Department of Defense Bibliography of Logistics Studies and Related Documents written by United States. Defense Logistics Studies Information Exchange and published by . This book was released on 1986 with total page 1210 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Combustion Studies of Very High Burning Rate (VHBR) Propellants

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ISBN 13 :
Total Pages : 49 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Combustion Studies of Very High Burning Rate (VHBR) Propellants by : Arpad A. Juhasz

Download or read book Combustion Studies of Very High Burning Rate (VHBR) Propellants written by Arpad A. Juhasz and published by . This book was released on 1982 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt: The burning and impetus characteristics of a family of very high burning rate (VHBR) boron-hydride-based propellants were determined using the closed chamber technique. A systematic examination of burning behaviour vs chemical composition was made. The samples studied included bare, steel cased, and larger full bore cylindrical samples. Pressure time data were reduced to apparent linear burning rates using the conventional laminar burning assumptions made in closed chamber reductions. The results indicate that tailoring sample burning rates between 1 and 500 m/s may be possible. On the other hand, unlike conventional propellants, VHBR propellant burning rates are thought to depend not only on sample formulation but also on porosity, physical integrity, sample diameter, and confinement. These results point to a possible burning-with-breakup mechanism for these materials.

Solid propellant burning rate measurement in a closed bomb

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (977 download)

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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:

Simulation of Closed Chamber Burning of Very-High Rate Propellant

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ISBN 13 :
Total Pages : 31 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Simulation of Closed Chamber Burning of Very-High Rate Propellant by : Paul G. Baer

Download or read book Simulation of Closed Chamber Burning of Very-High Rate Propellant written by Paul G. Baer and published by . This book was released on 1988 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: Closed chamber firings of very-high burning rate (VHBR) propellants have been conducted at the Ballistic Research Laboratory as part of the traveling charge gun program. Using standard closed chamber data reduction techniques, burning rates in the range of 10 to 300 m/s over a pressure range of 50 to 300 MPa have been measured. Pressure-time records from the firings of VHBR propellants exhibit severe pressure wave phenomena which are removed by digital filtering prior to transformation to burning rate data. Burning rate data for four VHBR propellants were used in a 1-D traveling charge code set up to simulate VHBR propellant being fired in a closed chamber. Objectives were to check consistency of the data, obtain better estimates of the data, obtain an understanding of the gas dynamic phenomena occurring in the chamber, and assess the validity of simulations produced by the 1-D traveling charge gun code. The procedure used was to match simulated data to experimental pressure-time data and adjust the burning rate data until the two curves matched. It is concluded that consistency of burning rate data in excess of 35 m/s over the pressure range of 50-150 MPa is poor. High amplitude pressure waves in the chamber create severe errors in the derived propellant burning rates.

Closed Chamber Burning Characteristics of New VHBR (Very High Burning Rate) Formulations

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ISBN 13 :
Total Pages : 41 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Closed Chamber Burning Characteristics of New VHBR (Very High Burning Rate) Formulations by : Kevin J. White

Download or read book Closed Chamber Burning Characteristics of New VHBR (Very High Burning Rate) Formulations written by Kevin J. White and published by . This book was released on 1985 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: Combustion studies were carried out on VHBR propellants in order to determine formulation and fabrication parameters that control the burning characteristics of these compounds. Formulation parameters such as type of fuel, oxidizer, type and percent of binder, oxidizer/binder ration and percent of theoretical maximum density were varied and the effects on combustion were studied using both a closed chamber and an optically transparent bomb. Although numerous facets of the combustion mechanisms remain unclear, the following picture has emerged for the specific formulations studied. The first phase of combustion is a relatively slow porous burning that proceeds down throughout the sample. The original form of the sample remains, although the residue is porous and is filled with hot combustion products. Depending on the composition, percent theoretical density and sample confinement, a transition to a very rapid combustion takes place throughout the entire sample, accompanied by some deconsolidation. For some conditions (composition or confinement) this second phase does not occur. The transition pressure to and the velocity of the second phase varies with the formulation parameters. The details of these results are discussed in the remainder of the paper.

Government Reports Annual Index

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ISBN 13 :
Total Pages : 1150 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Government Reports Annual Index by :

Download or read book Government Reports Annual Index written by and published by . This book was released on 1985 with total page 1150 pages. Available in PDF, EPUB and Kindle. Book excerpt: Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.

Government Reports Annual Index: Keyword A-L

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ISBN 13 :
Total Pages : 976 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Government Reports Annual Index: Keyword A-L by :

Download or read book Government Reports Annual Index: Keyword A-L written by and published by . This book was released on 1985 with total page 976 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Solid Propellant Burning Rate Measurement in a Closed Bomb

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ISBN 13 :
Total Pages : 53 pages
Book Rating : 4.:/5 (227 download)

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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.

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 1224 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Government Reports Announcements & Index by :

Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1985 with total page 1224 pages. Available in PDF, EPUB and Kindle. Book excerpt:

11th International Symposium on Ballistics: Propulsion dynamics, launch dynamics, flight dynamics

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Publisher :
ISBN 13 :
Total Pages : 878 pages
Book Rating : 4.:/5 (38 download)

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Book Synopsis 11th International Symposium on Ballistics: Propulsion dynamics, launch dynamics, flight dynamics by :

Download or read book 11th International Symposium on Ballistics: Propulsion dynamics, launch dynamics, flight dynamics written by and published by . This book was released on 1989 with total page 878 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Cities and Their Vital Systems

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Publisher : National Academies Press
ISBN 13 : 9780309037860
Total Pages : 1298 pages
Book Rating : 4.0/5 (378 download)

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Book Synopsis Cities and Their Vital Systems by : Advisory Committee on Technology and Society

Download or read book Cities and Their Vital Systems written by Advisory Committee on Technology and Society and published by National Academies Press. This book was released on 1989 with total page 1298 pages. Available in PDF, EPUB and Kindle. Book excerpt: Cities and Their Vital Systems asks basic questions about the longevity, utility, and nature of urban infrastructures; analyzes how they grow, interact, and change; and asks how, when, and at what cost they should be replaced. Among the topics discussed are problems arising from increasing air travel and airport congestion; the adequacy of water supplies and waste treatment; the impact of new technologies on construction; urban real estate values; and the field of "telematics," the combination of computers and telecommunications that makes money machines and national newspapers possible.