Log in

Relevant bibliographies by topics / Double-based rocket propellants

Contents

Journal articles
Dissertations / Theses
Book chapters

Academic literature on the topic 'Double-based rocket propellants'

Author: Grafiati

Published: 4 June 2021

Last updated: 10 February 2022

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Double-based rocket propellants.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Double-based rocket propellants"

1

Paraschiv, Titi, Tudor Viorel Tiganescu, George Ovidiu Iorga, Raluca Elena Ginghina, and Octavian Constantin Grigoroiu. "Experimental and Theoretical Study on Three Combustion Models for the Determination of the Performance Parameters of Nitrocellulose - Based Propellants." Revista de Chimie 71, no. 9 (2020): 87–97. http://dx.doi.org/10.37358/rc.20.9.8320.

Full text

Abstract:

Nitrocellulose based propellants are the main materials used for ballistic and rocket applications. The chemical composition of the propellants, the loading density and propellant grain geometry are the decisive parameters that influence the performance parameters in ballistic application. In this paper the authors evaluate three models of combustion for energetic materials for the determination of heat of explosion and specific volume together with the adiabatic flame temperature. The authors select six types of propellant (two simple base propellants, two double base propellants based on nit

APA, Harvard, Vancouver, ISO, and other styles

2

Li, Jun-Qiang, Linlin Liu, Xiaolong Fu, et al. "Transformation of Combustion Nanocatalysts inside Solid Rocket Motor under Various Pressures." Nanomaterials 9, no. 3 (2019): 381. http://dx.doi.org/10.3390/nano9030381.

Full text

Abstract:

In this paper, the dependences of the morphology, particle sizes, and compositions of the condensed combustion products (CCP) of modified double-base propellants (1,3,5-trimethylenetrinitramine (RDX) as oxidizer) on the chamber pressure (<35 MPa) and nickel inclusion have been evaluated under a practical rocket motor operation. It has been shown that higher pressure results in smaller average particle sizes of the CCPs. The CCPs of Ni-containing propellants have more diverse morphologies, including spherical particles, large layered structures, and small flakes coated on large particles dep

APA, Harvard, Vancouver, ISO, and other styles

3

Agrawal, J. P., S. Venugopalan, Javed Athar, J. V. Sabane, and M. Muralidharan. "Polysiloxane-based inhibition system for double-base rocket propellants." Journal of Applied Polymer Science 69, no. 1 (1998): 7–12. http://dx.doi.org/10.1002/(sici)1097-4628(19980705)69:1<7::aid-app2>3.0.co;2-n.

Full text

APA, Harvard, Vancouver, ISO, and other styles

4

Agrawal, J. P., and K. S. Kulkarni. "Tetrachloro Phthalic Anhydride Based Chloropolyesters for Inhibition of Double Base Rocket Propellants." Defence Science Journal 36, no. 4 (1986): 409–20. http://dx.doi.org/10.14429/dsj.36.5989.

Full text

APA, Harvard, Vancouver, ISO, and other styles

5

Bellamy, A. J., J. M. Bellerby, and M. H. Sammour. "Stabilizer reactions in cast double base rocket propellants. Part VII: Effect of lead-based ballistic modifiers on the reactions of propellant stabilizers during simulated aging of cast double base solid propellants." Propellants, Explosives, Pyrotechnics 21, no. 2 (1996): 85–89. http://dx.doi.org/10.1002/prep.19960210207.

Full text

APA, Harvard, Vancouver, ISO, and other styles

6

Ommi, Fathollah, Koros Nekofar, Amir Kargar, and Ehsan Movahed. "Experimental investigation of characteristics of a double-base swirl injector in a liquid rocket propellant engine." Thermal Science 14, no. 2 (2010): 479–91. http://dx.doi.org/10.2298/tsci1002479o.

Full text

Abstract:

In this work the fundamentals of swirl injector calculation is investigated and new design procedure is proposed. The design method for double-base liquid-liquid injectors is presented based on this theory and experimental results. Then special conditions related to double based liquid-liquid injectors are studied and the corresponding results are applied in design manipulation. The behavior of injector in various performing conditions is studied, and the design procedure is presented based on obtained results. A computer code for designing the injector is proposed. Based on this code, four in

APA, Harvard, Vancouver, ISO, and other styles

7

Szala, Mateusz. "Development trends in artillery ammunition propellants." Materiały Wysokoenergetyczne / High Energy Materials, November 25, 2020, 5–16. http://dx.doi.org/10.22211/matwys/0196.

Full text

Abstract:

A short history of nitrocellulose (NC) use in propellants is discussed. The advantages and disadvantages of NC as a semi-synthetic component of powders and rocket propellants are presented. Based on the conventional classification of propellants, the options of eliminating nitrocellulose in different types of powders and rocket propellants are discussed in detail. The analysis shows that in the foreseeable future, the elimination of NC in single-base and double-base propellants is highly unlikely. The observed trends in triple-base propellant development also does not show any tendencies in th

APA, Harvard, Vancouver, ISO, and other styles

8

de Vasconcelos Figueiredo, Paulo Alexandre Rodrigues, and Francisco Miguel Ribeiro Proença Brojo. "Theoretical Analysis of Ammonium-perchlorate Based Composite Propellants with RDX Containing Small Size Particles of Beryllium." KnE Engineering, June 2, 2020. http://dx.doi.org/10.18502/keg.v5i6.7058.

Full text

Abstract:

Rocket engines have been developed for at least the last six decades. There is a need to improve the actual solid propellant grain for rocket engines through the addiction of metallic fuels in the mixture as well as the addiction of energetic binders to stabilize the combustion. The rocket industry expects the launchers to be reliable, to be faster, stable and to have longer times of operation for the most possible payload weight (operational envelope). New propellants should have optimized ignition and combustion time rates reducing the possibility of negative oxygen balance thus reducing det

APA, Harvard, Vancouver, ISO, and other styles

9

Motyl, Krzysztof, Bogdan Zygmunt, Andrzej Cholewiak, and Mirosław Szczepanik. "Ballistic tests of double-based propelling charges with different carbon black content." Materiały Wysokoenergetyczne / High Energy Materials, November 25, 2020, 73–80. http://dx.doi.org/10.22211/matwys/0193.

Full text

Abstract:

Nitrocellulose and nitroglycerin are the main components of double-base propellants comprising up to 95% of their total mass. A chemical stabiliser and a burn rate modifier are required components, added in amounts of several percent. The study analyses the effect of carbon black content, contributing less than 1% of the propellant mass, on the burning rate of differently shaped propelling charges. The experiments, carried out on high energetic, double-base propelling charges, showed that the carbon black content significantly affects the burning rate of the propelling charge in the rocket mot

APA, Harvard, Vancouver, ISO, and other styles

Dissertations / Theses on the topic "Double-based rocket propellants"

1

Tucker, J. "A whole life assessment of extruded double base propellants." Thesis, Cranfield University, 2013. http://dspace.lib.cranfield.ac.uk/handle/1826/8032.

Full text

Abstract:

The manufacturing process for solventless extruded double base propellants involves a number of rolling and reworking stages. Throughout these processes a decrease in weight average molecular weight was observed, this was attributed to denitration. Differential scanning calorimetery data indicated that the reworking stages of extruded double base propellant manufacture were crucial to the homogenisation of the propellant mixture. To determine the homogeneity of the final extruded product, a sample was analysed across its diameter. No variations in stabiliser concentration, molecular weight, or

APA, Harvard, Vancouver, ISO, and other styles

Book chapters on the topic "Double-based rocket propellants"

1

Vetlický, B., and T. Dosoudil. "Utilisation of Double-Based Powders and Rocket Propellants for Production of “Dry Explosives of Slurry Type”." In Application of Demilitarized Gun and Rocket Propellants in Commercial Explosives. Springer Netherlands, 2000. http://dx.doi.org/10.1007/978-94-011-4381-3_4.

Full text

APA, Harvard, Vancouver, ISO, and other styles

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!