Research and Experimental Validation of Precise Internal Ballistic Modeling for Hydrogen Gun-launched Unmanned Aerial Vehicles

ZHANG Wei; JIA Qiang; LU Jiongbiao; REN Jie

doi:10.12382/bgxb.2025.0504

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Research and Experimental Validation of Precise Internal Ballistic Modeling for Hydrogen Gun-launched Unmanned Aerial Vehicles

更新时间：2026-05-07

- Research and Experimental Validation of Precise Internal Ballistic Modeling for Hydrogen Gun-launched Unmanned Aerial Vehicles
- Acta Armamentarii (2026)
- 作者机构：
  
  1. 南京理工大学机械工程学院,江苏,南京,210094
  2. 西北机电工程研究所,陕西,咸阳,712099
  3. 湖北三江航天江河化工科技有限公司,湖北,宜昌,444200
- 作者简介：
- 基金信息：
- DOI：10.12382/bgxb.2025.0504
  CLC： TJ012.1
- Received：13 June 2025，
  
  Online First：07 May 2026，
- 稿件说明：
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张薇，贾强，卢炯彪，等. 氢能炮射无人机精确内弹道模型研究与试验验证[J/OL]. 兵工学报, 2026(2026-05-07). https://doi.org/10.12382/bgxb.2025.0504.

ZHANG W, JIA Q, LU J, et al. Research and experimental validation of precise internal ballistic modeling for hydrogen gun-launched unmanned aerial vehicles[J/OL]. Acta Armamentarii, 2026(2026-05-07). https://doi.org/10.12382/bgxb.2025.0504. (in Chinese)
张薇，贾强，卢炯彪，等. 氢能炮射无人机精确内弹道模型研究与试验验证[J/OL]. 兵工学报, 2026(2026-05-07). https://doi.org/10.12382/bgxb.2025.0504. DOI：

ZHANG W, JIA Q, LU J, et al. Research and experimental validation of precise internal ballistic modeling for hydrogen gun-launched unmanned aerial vehicles[J/OL]. Acta Armamentarii, 2026(2026-05-07). https://doi.org/10.12382/bgxb.2025.0504. (in Chinese) DOI：

摘要

针对传统火药发射技术在无人机集群作战中面临的成本高、污染重及火工品管控等问题，提出基于氢能推进的炮射无人机技术并试验验证了其可行性。对比多种真实气体状态方程在特定温度及压强工况下的压缩因子，表明Peng-Robinson方程可更准确描述氢能炮射无人机系统真实气体热力学特性。构建了考虑真实气体效应的精确内弹道理论模型，分析在恒定初始压力和燃料配比条件下，氮气含量对氢能系统发射性能的影响，进而提出以空气替代纯氧作为氧化剂的优化方案，显著提升了系统的内弹道性能并提高了经济性。建立控制阀喷口面积变化规律二元函数模型，有效降低了无人机发射过程中的最大过载。研究结果为氢能炮射无人机内弹道性能优化及集群作战应用提供了关键技术支撑。

Abstract

Traditional gunpowder launching for unmanned aerial vehicle (UAV) clusters faced three problems: high cost

heavy pollution

and pyrotechnic control difficulties. To address these

we proposed a hydrogen-propelled gun-launched UAV technology. Experimental verification confirmed its feasibility.We compared compressibility factors of various real gas equations under specific temperature and pressure. The Peng-Robinson equation is more accurate in describing the real gas thermodynamic characteristics of hydrogen gun-launched UAV systems.An internal ballistic model incorporating real gas effects was constructed. This model analyzed nitrogen content's impact on launch performance at constant initial pressure and fuel ratios. Replacing pure oxygen with air as oxidizer was proposed. This optimization significantly improved internal ballistic performance while enhancing cost-effectiveness. A binary function model for control valve nozzle area variation was established. This effectively reduced maximum launch velocity overload during UAV ejection. These results provide key technical support for optimizing hydrogen gun-launched UAV systems and advancing cluster warfare applications.

关键词

Keywords

references

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