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Analysis and Determination of Technological Trends of the Development of an Afterburning Chamber of Turbofan Engines Cover

Analysis and Determination of Technological Trends of the Development of an Afterburning Chamber of Turbofan Engines

Open Access
|Dec 2025

Figures & Tables

Fig. 1.

K
1 plotted by year of aircraft development.
K 1 plotted by year of aircraft development.

Fig. 2.

K
2 plotted by year of aircraft development.
K 2 plotted by year of aircraft development.

Fig. 3.

K
3 plotted by year of aircraft development.
K 3 plotted by year of aircraft development.

Fig. 4.

KNORM
 plotted by year of aircraft development.
KNORM plotted by year of aircraft development.

Aircraft Included in the Study: Purpose and Main Technical Characteristics_

AircraftPurposeYear in ServiceEngines (Number & Type)Engine Weight (kg)Thrust (AFB), kNMax Takeoff Weight (kg)Thrust-to-Weight Ratio (AFB)SFC (AFB), kg/N·h
T-38 TalonCTA19612 × J85-GE-5A26517.1256706.580.224
F-5BCTA19642 × J85-GE-1327118.1592986.820.227
Su-15FI19672 × Tumansky R-13120564.7179005.470.213
SEPECAT JaguarAA19732 × Adour Mk 10270030.89157004.490.265
F-15 EagleF19762 × F1001375106308457.850.2161
F-16 Fighting FalconMRF19781 × F1001375106192007.850.2161
TornadoMRFB19792 × RB19990071.13280008.050.2651
F/A-18A/B HornetMRF19832 × F40498071.2254007.400.177
MiG-29MRF19832 × RD-33-2S104083180008.130.214
Mirage 2000MRF1984SNECMA M53147088.2170006.110.209
Su-27F19852 × AL-31F1530122.4304508.150.196
B-1B LancerSB19864 × F1011815133.42164007.490.2243
AIDC F-CK-1 Ching-kuoMRF19942 × F12590042122004.750.21
RafaleMRF20012 × M8889775.62245008.590.1733
Eurofighter TyphoonMRF20032 × EJ20098990235009.270.1764
F-22 RaptorMRF20052 × F-1191769155.6380008.960.221
Hongdu L-15CTA20132 × AI-222-25F4404295009.730.19
Su-35SMRF20142 × AL-41F1C1608140345008.870.192
HAL TejasMRF20151 × GTX-35VS118081155006.990.207
F-35 Lightning IIMRF20151 × F-1351701191.33175111.460.198
Mitsubishi X-2 ShinshinF20162xIHI XF-51420122-8.75-
Su-57MRF20202 × AL-41F11700160370009.590.19
Language: English
Page range: 1 - 27
Submitted on: Aug 19, 2025
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Accepted on: Oct 10, 2025
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Published on: Dec 24, 2025
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2025 Volodymyr Rublev, Vasyl Loginov, Dmytro Kozel, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.