UGC Approved Journal no 63975(19)
New UGC Peer-Reviewed Rules

ISSN: 2349-5162 | ESTD Year : 2014
Volume 12 | Issue 10 | October 2025

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Published in:

Volume 12 Issue 7
July-2025
eISSN: 2349-5162

UGC and ISSN approved 7.95 impact factor UGC Approved Journal no 63975

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Unique Identifier

Published Paper ID:
JETIR2507066


Registration ID:
565729

Page Number

a612-a634

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Title

Advanced Fuel Injector Systems for Guided Missile Propulsion: Design Principles, Atomization Dynamics, and Performance Characterization

Abstract

This report presents a comprehensive analysis of an advanced pintle-type fuel injector system tailored for guided missile propulsion. Integrating experimental cold-flow testing with water as a simulant, analytical fluid dynamics, and design comparison, the study deciphers the interplay of injector geometry, internal flow mechanics, and atomization behavior. Results reveal that multi-orifice configurations (e.g., 4-hole caps) enhance atomization quality, broaden spray cone angles, and improve combustion efficiency — critical factors for agile missile maneuvering and thrust modulation. Leveraging principles of Bernoulli, Navier–Stokes, and Venturi effect, the injector architecture strategically induces turbulence and cavitation to promote droplet breakup. Though preliminary tests used water, findings underscore the design’s potential for improved specific impulse, combustion stability, and reduced emissions in operational scenarios. Future work includes quantitative droplet sizing, CFD validation, and hot-fire testing with actual propellants to complete the performance envelope and validate the injector’s role in next-generation missile systems.

Key Words

Pintle injector, guided missile propulsion, atomization dynamics, fluid dynamics, CFD analysis, combustion efficiency.

Cite This Article

"Advanced Fuel Injector Systems for Guided Missile Propulsion: Design Principles, Atomization Dynamics, and Performance Characterization", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.12, Issue 7, page no.a612-a634, July-2025, Available :http://www.jetir.org/papers/JETIR2507066.pdf

ISSN


2349-5162 | Impact Factor 7.95 Calculate by Google Scholar

An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 7.95 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator

Cite This Article

"Advanced Fuel Injector Systems for Guided Missile Propulsion: Design Principles, Atomization Dynamics, and Performance Characterization", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.12, Issue 7, page no. ppa612-a634, July-2025, Available at : http://www.jetir.org/papers/JETIR2507066.pdf

Publication Details

Published Paper ID: JETIR2507066
Registration ID: 565729
Published In: Volume 12 | Issue 7 | Year July-2025
DOI (Digital Object Identifier):
Page No: a612-a634
Country: Bhubaneshwar, Odisha, India .
Area: Science & Technology
ISSN Number: 2349-5162
Publisher: IJ Publication


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