The integration of civilian nitrocellulose in propellant with highly improved mechanical property and thermal stability, and study on its combustion behavior

https://doi.org/10.1016/j.polymdegradstab.2024.110689Get rights and content

Highlights

  • CNC with similar molecular structure and composition to NC can be used in propellant.

  • Civilian nitrocellulose can further plasticize high-nitrogen nitrocellulose.

  • The thermal stability of CNC based-propellant was enhanced and presented stable combustion behavior.

Abstract

Developing binders for propellants with balanced mechanical and energy properties is important and challenging. Herein, high-viscosity civilian nitrocotton (CNC) was used as reinforcing binder to prepare CNC-based propellant by solvent method. The influence of viscosity and content of CNC on mechanical properties, thermal stability, and combustion performance of propellants was investigated. The plasticizing process of nitrocellulose fibers can be well described by swelling mass changes and has a strong correlation with mechanical properties. The impact test combined with morphology observation by scanning electron microscope (SEM) and evaluation about matrix, fiber, and structure systems revealed that the subsidiary plasticizing mechanism of CNC and the homogeneous system of CNC-based propellant play the dominant role in enhancement of macroscopic mechanical properties. Besides, the structure of propellant was investigated using FTIR, XRD, and Raman, which indicated that propellant containing CNC exerting similar structure with NC-based propellant. Moreover, the analysis of thermal decomposition kinetics demonstrated that the introduction of CNC could further enhance the thermal stability of propellant, like the increased activation energy. Finally, the study of combustion performance demonstrated that CNC-based propellant can burn steadily, and energy out-put was further enhanced as compared with NC propellant. Therefore, this design and adjustment for the introduction of CNC in propellant could provide fundamental theory and data support for the development of CNC in propellants.

Introduction

The consumption of ammunition resources in information warfare has increased exponentially due to its shorter duration and accelerated processes, thus the timely and accurate supply of ammunition plays a critical role in winning the war [1], [2], [3]. Research into raw material sources and production has important implications for ammunition preparation and supply. Nitrocellulose (NC), also known as nitrocotton made from refined cotton, is one of the basic raw materials used in ammunition production, particularly in the manufacture of conventional propellants and high-energy mixing explosives. Gun propellants in service include single, double, and triple base propellants and others, of which nitrocotton as a binder is the basic component [4,5]. Of these, the maximum nitrocotton content in single-base propellants could be 98 %, while the content of nitrocellulose in triple base propellants is smaller at 30 % [6]. Therefore, the supply ability of nitrocotton determins the production capacity of gun propellants.

In the search for binders to replace nitrocotton in solid propellants, various new polymer binder propellants have been developed in recent decades to satisfy the requirements of safety, energy, and process for propellant [7,8]. Generally, it can be divided into energetic binders and non-energetic binders. Non-energetic binders have been commonly studied in composite propellant systems for rocket engines, such as the hydroxyl‑terminated polybutadiene (HTPB) system [9,10], the polyurethane (PU) system [11,12], the nitrated bacterial cellulose system [13,14], and so forth. The addition of a non-energetic binder, on the other hand, reduces the energy level of the gun propellant. Notably, the way of enhancing the energy of propellant by adding huge volumes of energetic explosives, will not only diminish the mechanical strength of the propellant but will also promote barrel ablation and drastically reduce the weapon's service life [15,16]. Therefore, the research about non-energetic binders focused on applying composite propellants in rocket motors. Energetic binders, which contain energetic groups in the main or side chains, such as nitro (-NO2), nitrate (-ONO2), and azido (-N3), are also mainly used in the field of rocket propellants and explosives. At present, the application of energy-containing thermoplastic elastomers (ETPE) [17], [18], [19], glycidyl azide polymers (GAP) [20], and poly glycidyl nitrate (PGN) [21,22] in gun propellant has been reported. However, most of these energetic binders are used in small quantities as additives in formulations, and some processing problems prevent them from being used in large quantities as the base material for gun propellants. Thus, nitrocotton, or a mixture of nitrocotton and a polymer, was still the main binder for solid propellants.

Nitrocellulose derived from cotton fibers is widely used for the production of propellants owing to its high purity and ease processing. However, the propellant prepared with NC derived from cotton fibers faces two main problems:(a) There are nearly no other raw fibers except cotton, while the use of other plant fibers requires the replacement of the corresponding production equipment and the adjustment of process conditions. (b) It has fewer production lines and a lower level of capacity efficiency. Civilian Nitrocellulose (CNC) is a type of nitrocellulose created from wood, bamboo pulp, cotton and other plant fiber sources, and it is primarily used in civilian products such as paint, nail polish, film, and varnish [23], [24], [25]. It has the same spatial network structure and composition as NC. Furthermore, beneficial from the excellent production technology and equipment, CNC has high purity, a wide range of viscosities, and good mechanical qualities, and its production and consumption are much higher than that of military NC.As a potential propellant binder that can be supplied in large quantities and at short notice in certain cases, CNC could be an excellent alternative to military nitrocellulose to overcome the shortfall in military NC production. Moreover, a study of the nitrogen content characteristics of nitrocellulose revealed that increasing its nitrogen content improved the overall stiffness of the propellant system while decreasing the mechanical properties. The application of CNC with 12N% nitrogen content and excellent mechanical properties in propellant formulation means that the mechanical properties of gun propellants can be satisfied while adding more energetic components to increase the energy, which provides a new way to achieve a balance between the energetic and mechanical properties of artillery propellants [15]. Additionally, due to their excellent performance characteristics and relatively simple and economical manufacture and use, modern solid propellants have been applied in a variety of civil applications, including signaling and fireworks, various special devices in the automotive and aeronautical industries, and the destruction of hazardous biological or chemical agents and persistent pollutants [26]. Hence, the utilization of CNC as a binder for solid propellants may also lead to developments in some civil applications.

Herein, a kind of novel CNC-based propellants were prepared by the traditional solvent method. The effect of CNC on the processability, morphology, mechanical properties, thermal stability, and combustion behavior and energy performance of the gun propellant was investigated. To the best knowledge of us, the use of CNC in gun propellant has not been reported before. Therefore, this study will provide a new strategy of selecting a gun propellant binder, controlling production costs, and developing engineering applications.

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Section snippets

Material

The civil nitrocotton (abbreviated as CNC, 12.0 % nitrogen) with a viscosity ranging from 0.38 °E to 9.42 °E was provided by Hubei Xuefei Chemical Co., Ltd. B#NC (13.1 % nitrogen) was provided by Luzhou Northern Chemical Co., Ltd.; diphenylamine (DPA) was purchased from Sinopharm Chemical Reagent Co., Ltd. Anhydrous ethanol and acetone were purchased from Nanjing Chemical Reagent Co., Ltd.

Experimental

The preparation process of the CNC-base propellant by the solvent method was presented in Fig. 1. Firstly,

Fabricability analysis

Photos of CNC-based propellants with various CNC types prepared by the solvent method are shown in Fig. 2. It can be observed that there are significant differences in their manufacturability by comparing all obtained samples of propellant. From the differences in raw material characteristics, one can be found that the viscosity of CNC plays an important role in the processability of CNC-based propellants. For the 1/16#CNC, the propellant could not be processed properly (Fig. 2a). The main

Conclusions

In summary, this work firstly introduced the CNC into gun propellant system to prepare a novel CNC-based gun propellant. It was found that the obtained CNC-based propellant exhibited significantly lower mechanical strength by using a viscosity lower than 1.44 E civil nitrocotton, which makes it cannot be extruded normally. The propellant prepared with 800#CNC has a smooth surface, dense structure, and excellent mechanical properties. For mechanical properties, the maximum impact strengths of

Ethics approval and consent to participate

Not applicable.

Consent for publication

All the authors listed have approved the enclosed manuscript for publication.

CRediT authorship contribution statement

Heng Gao: Data curation, Methodology, Writing – original draft, Writing – review & editing. Ling Chen: Conceptualization, Funding acquisition, Resources, Writing – review & editing. Fengqiang Nan: Conceptualization, Resources, Funding acquisition, Investigation. Binbin Wang: Data curation. Xiang Cao: Writing – review & editing. Derong Meng: Writing – review & editing. Weidong He: Conceptualization, Funding acquisition, Writing – review & editing.

Declaration of competing interest

We declare that this manuscript have no any commercial or associative interest that represents a conflict of interest.

Acknowledgment

This work thanks to the supporting of Jiangsu Funding Program for Excellent Postdoctoral Talent (2023ZB472), China Postdoctoral Science Foundation (2023TQ0158), and the National Funding Postdoctoral Researcher Program (GZC20233496).This study thanks to Dr Xu Bin, Engineer Yu Yannian, Engineer Yin Shenglai for their experimental help and technical support. Thanks to the analysis and testing center of Nanjing university of science and technology for their experimental help and technical

References (31)

  • S. Chaturvedi et al.

    Solid propellants: AP/HTPBcomposite propellants

    Arab. J. Chem.

    (2019)
  • Y. Wang et al.

    Three-dimensional network structure nitramine gun propellant with nitrated bacterial cellulose

    J. Mater. Res. Technol.

    (2020)
  • Y. Tian et al.

    Durable and room-temperature curable superhydrophobic composite coating on nitrocellulose lacquer

    Surf. Coat. Technol.

    (2017)
  • H.B. Liu et al.

    Construction and effectiveness evaluation of ammunition supply guarantee system based on DoDAF

    J. Ordnance Equip. Eng.

    (2023)
  • C.Y. Wang et al.

    Brief discussion on ammunition-supply guarantee of civilian-military integration

    Dual-Use Goods Technol.

    (2017)
  • S. Hamid et al.

    Disruption management in the defense ammunition industrial base

    Secur. J.

    (2013)
  • L. Chen et al.

    Sol–gel synthesis of insensitive nitrated bacterial cellulose/cyclotrimethylenetrinitramine nano-energetic composites and its thermal decomposition property

    Cellulose

    (2022)
  • Y. Song et al.

    Preparation and properties of NC/TATB/Bu-NENA/TMETN low sensitive gun propellants

    Prop. Explos. Pyrotech.

    (2021)
  • Z. Wang et al.

    Theory and practice of explosives

    (2004)
  • K. Lysien et al.

    Solid propellant formulations: a review of recent progress and utilized components

    Materials. (Basel)

    (2021)
  • B.P. Mason et al.

    Solid propellants

    Rubber Chem. Technol.

    (2019)
  • H. Abusaidi et al.

    Development of composite solid propellant based on nitro functionalized hydroxyl-terminated polybutadiene

    Prop. Explos. Pyrotech.

    (2017)
  • S. Touidjine et al.

    Preparation and characterization of polyurethane/nitrocellulose blends as binder for composite solid propellants

    Propellants Explo. Pyrotech.

    (2022)
  • C. Shen et al.

    Influence of fluorinated polyurethane binder on the agglomeration behaviors of aluminized propellants

    Polymers. (Basel)

    (2022)
  • L. Chen et al.

    Nitrated bacterial cellulose-based energetic nanocomposites as propellants and explosives for military applications

    ACS Appl. Nano Mater.

    (2021)
  • Cited by (1)

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