The Application of Energetic Materials Genome Approach for Development of the Solid Propellants Through the Space Debris Recycling at the Space Platform

Author(s):  
Amrith Mariappan ◽  
Hanlim Choi ◽  
Victor S Abrukov ◽  
Darya A. Anufrieva ◽  
Alexander N. Lukin ◽  
...  
Nanomaterials ◽  
2021 ◽  
Vol 12 (1) ◽  
pp. 133
Author(s):  
Weiqiang Pang ◽  
Chongqing Deng ◽  
Huan Li ◽  
Luigi T. DeLuca ◽  
Dihua Ouyang ◽  
...  

As a hot research topic, nano-scale energetic materials have recently attracted much attention in the fields of propellants and explosives. The preparation of different types of nano-sized energetic materials were carried out, and the effects of nano-sized energetic materials (nEMs) on the properties of solid propellants and explosives were investigated and compared with those of micro-sized ones, placing emphasis on the investigation of the hazardous properties, which could be useable for solid rocket nozzle motor applications. It was found that the nano-sized energetic materials can decrease the impact sensitivity and friction sensitivity of solid propellants and explosives compared with the corresponding micro-sized ones, and the mechanical sensitivities are lower than that of micro-sized particles formulation. Seventy-nine references were enclosed.


2021 ◽  
Vol 1027 ◽  
pp. 123-129
Author(s):  
Ya Hao Liu ◽  
Jian Zheng ◽  
Gui Bo Yu ◽  
Jing Qia ◽  
Quan Qun Xu ◽  
...  

Owing to its remarkable mechanical, electrical and thermal properties, graphene has been a hot area of composites research in the past decade, including the field of energetic materials. Graphene has been widely applied in enhancing the physical properties of energetic materials, such as solid composite propellants. Through the way of adding different forms of graphene into the matrix of solid propellants, their thermal decomposition performance can be effectively improved. In this paper, we reviewed the status and challenges of the application of graphene in the thermal decomposition of composite solid propellant. Moreover, the main preparation methods and material structures of graphene are reviewed. We can conclude that graphene and its derivatives can enhance the catalytic effect remarkably, which can be attributed to the large specific surface area of graphene that makes the uniformly dispersed catalyst particles and the more catalyst active sites. Meanwhile, graphene possesses the high thermal conductivity, making the rapider heat diffusion, which can promote the decomposition reactions of the energetic components in solid propellants. Graphene and catalyst work synergistically in their thermal decomposition. More than this, the main methods to improve the thermal decomposition of energetic components of composite propellants and their effects on decomposition temperature reduction are systematically summarized, respectively.


2017 ◽  
Vol 67 (1) ◽  
pp. 68-77 ◽  
Author(s):  
Guangpu Zhang ◽  
Tianfu Zhang ◽  
Jinqing Li ◽  
Yunjun Luo

Author(s):  
Wen-Li Yuan ◽  
Ling He ◽  
Guo-Hong Tao ◽  
Jean’ne M. Shreeve

1999 ◽  
Vol 15 (5) ◽  
pp. 713-718 ◽  
Author(s):  
Bruno D’Andrea ◽  
Francesca Lillo

2019 ◽  
Vol 92 (1) ◽  
pp. 1-24 ◽  
Author(s):  
B. P. Mason ◽  
C. M. Roland

ABSTRACT Solid propellants are energetic materials used to launch and propel rockets and missiles. Although their history dates to the use of black powder more than two millennia ago, greater performance demands and the need for “insensitive munitions” that are resistant to accidental ignition have driven much research and development over the past half-century. The focus of this review is the material aspects of propellants, rather than their performance, with an emphasis on the polymers that serve as binders for oxidizer particles and as fuel for composite propellants. The prevalent modern binders are discussed along with a discussion of the limitations of state-of-the-art modeling of composite motors.


2020 ◽  
Vol 6 (49) ◽  
pp. eabb1899
Author(s):  
Wen-Li Yuan ◽  
Lei Zhang ◽  
Guo-Hong Tao ◽  
Shuang-Long Wang ◽  
You Wang ◽  
...  

A new generation of rocket propellants for deep space exploration, ionic liquid propellants, with long endurance and high stability, is attracting more and more attention. However, a major defect of ionic liquid propellants that restricts their application is the inadequate hypergolic reactivity between the fuel and the oxidant, and this defect results in local burnout and accidental explosions during the launch process. We propose a visualization model to show the features of structure, density, thermal stability, and hypergolic activity for estimating propellant performances and their application abilities. This propellant materials genome and visualization model greatly improves the efficiency and quality of developing high-performance propellants, which benefits the discovery of new advanced functional molecules in the field of energetic materials.


2016 ◽  
Vol 108 (10) ◽  
pp. 101903 ◽  
Author(s):  
Qiang Wu ◽  
Qingming Zhang ◽  
Renrong Long ◽  
Kai Zhang ◽  
Jun Guo

2020 ◽  
Vol 330 ◽  
pp. 01048
Author(s):  
Victor Abrukov ◽  
Darya Anufrieva ◽  
Alexander Lukin ◽  
Charlie Oommen ◽  
V. R. Sanalkumar ◽  
...  

The results of usage of data science methods, in particular artificial neural networks, for the creation of new multifactor computational models of the solid propellants (SP) combustion that solve the direct and inverse tasks are presented. The own analytical platform Loginom was used for the models creation. The models of combustion of double based SP with such nano additives as metals, metal oxides, termites were created by means of experimental data published in scientific literature. The goal function of the models were burning rate (direct tasks) as well as propellants composition (inverse tasks). The basis (script) of a creation of Data Warehouse of SP combustion was developed. The Data Warehouse can be supplemented by new experimental data and metadata in automated mode and serve as a basis for creating generalized combustion models of SP and thus the beginning of work in a new direction of combustion science, which the authors propose to call "Propellant Combustion Genome" (by analogy with a very famous Materials Genome Initiative, USA). "Propellant Combustion Genome" opens wide possibilities for accelerate the advanced propellants development Genome" opens wide possibilities for accelerate the advanced propellants development.


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