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ArticlePeer ReviewedOpen AccessPlagiarism Passed
Paper ID:IJSREM62717

A Critical Review on Study And Analysis Of Cap-Base Igniters For Reliable Initiation Systems

Stream/Area:

-

Subject:

-

Paper ID:

IJSREM62717

Volume:

10 |

5 |

May 2026

Pages:

1-3

Publication Frequency:

Monthly (12 issues per year)

DOI
Digital Object Identifier
10.55041/IJSREM62717

License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.

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Authors

Vinesh Sadashiv Bagade

Vinesh Sadashiv Bagade

Department of Mechanical Enigineering

Priyadarshini College of Engineering, Nagpur

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Dr.Subhash N Waghmare

Dr.Subhash N Waghmare

Department of Mechanical Enigineering

Priyadarshini College of Engineering, Nagpur

S

S.D.Shelare

Department of Mechanical Enigineering

Priyadarshini College of Engineering, Nagpur

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Abstract

It is developed to form a rigorous and technically based assessment of cap-based (nozzle-cap type) igniters, with particular emphasis on their practical reliability in the initiation of high-energy systems such as solid rocket motors and explosive transfer chains. The reliable operation of such igniters can hardly be overestimated, because any deviation or failure of the initiation sequence can be further propagated into the overall malfunction of the entire system, leading to a failure in the mission or a serious safety hazard. The systematically studied coupled thermo-mechanical processes that control the transformation of an input stimulus, usually electrical or mechanical, into a controlled ignition event, to assure consistent flame propagation and the transfer of energy to the primary energetic material. The analysis confirms that a geometric configuration is a prevailing factor that affects the igniter performance.

KEYWORDS

Key Words: Cap-Base Igniter Initiation Systems Ignition Reliability Pyrotechnic Devices Ballistic Ignition

Cite This Article

Vinesh Sadashiv Bagade, Dr.Subhash N Waghmare, S.D.Shelare, "A Critical Review on Study And Analysis Of Cap-Base Igniters For Reliable Initiation Systems," International Journal of Scientific Research in Engineering and Management, vol. 10, no. 5, pp. 1-3, May 2026. https://doi.org/10.55041/IJSREM62717

Full Article/Conclusion

Cap-base igniters are essential components of reliable initiation systems used in ammunition and defense applications. This review highlights the importance of igniter design, energetic material selection, combustion characteristics, and pressure generation in achieving consistent ignition performance. Recent developments in materials and simulation techniques have improved ignition reliability, safety, and efficiency. However, challenges such as sensitivity control, thermal stability, and performance under extreme conditions still require further research. Future studies should focus on advanced energetic materials and optimized igniter designs to enhance the reliability and safety of modern initiation systems.

References

1. Panagiotou, P., Kaparos, P., Salpingidou, C., Yakinthos, K. (2016). Aerodynamic design of an MALE UAV. Aerospace Science and Technology. 2. Singh, R., Kumar, P., Sharma, V. (2018). Thermal and Chemical Behavior of Ignition Systems. Defence Science Journal. 3. Zhang, W., Wang, L. (2020). Material Influence on Ignition Delay Characteristics. Propellants, Explosives, Pyrotechnics. 4. Gupta, A. (2022). Numerical Modeling of Primer-Based Ignition Systems. Journal of Energetic Materials. 5. El Adawy, M. (2023). Design and fabrication of a fixed-wing Unmanned Aerial Vehicle. Ain Shams Engineering Journal. 6. Bahadursha, A. V. L. Sainadh (2024). Optimization of fixed-wing aerodynamic shape through Genetic Algorithm and PyFluent Simulation. IJCRT. 7. Mehta, G.D. (2023). Reliability Studies of Pyrotechnic Igniters for Defence Applications. Defence Technology Reports. 8. Taylor, J. (2010). Unmanned Aircraft Systems, UAVs design, development, and Deployment. Wiley. 9. Lei Niu et al. (2022), Reliability Analysis of Pyrotechnic Igniter for Hydrogen–Oxygen Rocket Engine, Applied Sciences. 10. Sukandi N. Rohili et al. (2025), Design of Igniter for Solid Rocket Motor RX‑420/4000, The journal name is Indonesian Journal of Aerospace.

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Publication Date

5/6/2026

Peer Review Type

Double-Blind Peer Review

Review Rounds: 2

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