Short Communication - (2025) Volume 13, Issue 1
Received: 01-Feb-2025, Manuscript No. jaat-25-168460;
Editor assigned: 03-Feb-2025, Pre QC No. P-168460;
Reviewed: 17-Feb-2025, QC No. Q-168460;
Revised: 22-Feb-2025, Manuscript No. R-168460;
Published:
28-Feb-2025
, DOI: 10.37421/2329-6542.2025.13.341
Citation: Haddad, Noura. "Experimental Study of Jet Propulsion Efficiency Using Novel Fuels." J Astrophys Aerospace Technol 13 (2025): 341.
Copyright: © 2025 Haddad N. This is an open-access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.
The experimental investigation was conducted using a modified small-scale turbojet engine test bench equipped with advanced sensors and real-time data acquisition systems. Four fuel types were selected for testing: standard Jet-A (control), a second-generation biofuel derived from camelina oil, a Synthetic Paraffinic Kerosene (SPK) blend, and a hydrogen-enriched biofuel mixture. Each fuel underwent pre-combustion analysis to determine energy density, flash point, and viscosity, ensuring compatibility with engine hardware. Combustion chamber modifications, including fuel nozzle adaptors and reinforced seals, were implemented to accommodate the varying properties of the alternative fuels. The engine was run through a series of operating points simulating different flight regimes, from idle to maximum thrust, with data recorded for each scenario.
Results showed that the hydrogen-enriched biofuel produced the highest combustion efficiency, demonstrating a 7â??10% improvement in Thrust-Specific Fuel Consumption (TSFC) compared to Jet-A. This improvement is attributed to hydrogenâ??s high flame speed and clean combustion characteristics, which facilitated more complete fuel oxidation. The SPK blend also performed competitively, with slightly better efficiency than Jet-A and significantly lower particulate emissions. The camelina-derived biofuel, while sustainable and biodegradable, exhibited a moderate drop in efficiency due to its lower energy density. However, its performance was still within acceptable operational limits and met emissions regulations, showcasing its viability as a low-carbon alternative.
Thermal and emissions analysis revealed distinct combustion patterns for each fuel. The hydrogen-enriched blend displayed the lowest CO and unburned hydrocarbon emissions, with near-zero soot formation. The SPK blend also exhibited a cleaner burn, while camelina biofuel showed higher COâ?? output due to incomplete combustion at lower temperatures. Infrared thermography of the exhaust plume confirmed the correlation between flame temperature and emission profiles, supporting the hypothesis that fuel chemistry significantly influences propulsion thermodynamics. Additionally, engine wear and deposits were examined post-experiment, with alternative fuels showing reduced carbon buildup compared to conventional Jet-A.
A key component of the study was the comparative analysis of fuel-to-thrust efficiency. This metric, defined as the ratio of chemical energy input to mechanical thrust output, demonstrated that hydrogen enrichment offers a promising route to high-performance, low-emission propulsion. The SPK fuelâ??s synthetic formulation allowed precise control over molecular composition, resulting in consistent and efficient combustion. Conversely, the biofuelâ??s variability, rooted in feedstock and production methods, suggests a need for further refinement and standardization before widespread adoption. Nonetheless, the experimental data affirmed the feasibility of integrating these fuels into existing propulsion systems with minimal retrofitting [2].
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