Template:Thrust engine efficiency

Rocket engines in vacuum
Model	Type	First run	Application	TSFC		Isp (by weight)	Isp (by weight)
				lb/lbf·h	g/kN·s	s	m/s
Merlin 1D	liquid fuel	2013	Falcon 9	12	330	310	3000
Avio P80	solid fuel	2006	Vega stage 1	13	360	280	2700
Avio Zefiro 23	solid fuel	2006	Vega stage 2	12.52	354.7	287.5	2819
Avio Zefiro 9A	solid fuel	2008	Vega stage 3	12.20	345.4	295.2	2895
RD-843	liquid fuel		Vega upper stage	11.41	323.2	315.5	3094
Kuznetsov NK-33	liquid fuel	1970s	N-1F, Soyuz-2-1v stage 1	10.9	308	331<ref>"NK33". Encyclopedia Astronautica.</ref>	3250
NPO Energomash RD-171M	liquid fuel		Zenit-2M, -3SL, -3SLB, -3F stage 1	10.7	303	337	3300
LE-7A	cryogenic		H-IIA, H-IIB stage 1	8.22	233	438	4300
Snecma HM-7B	cryogenic		Ariane 2, 3, 4, 5 ECA upper stage	8.097	229.4	444.6	4360
LE-5B-2	cryogenic		H-IIA, H-IIB upper stage	8.05	228	447	4380
Aerojet Rocketdyne RS-25	cryogenic	1981	Space Shuttle, SLS stage 1	7.95	225	453<ref>"SSME". Encyclopedia Astronautica.</ref>	4440
Aerojet Rocketdyne RL-10B-2	cryogenic		Delta III, Delta IV, SLS upper stage	7.734	219.1	465.5	4565
NERVA NRX A6	nuclear	1967				869

Jet engines with Reheat, static, sea level
Model	Type	First run	Application	TSFC		Isp (by weight)	Isp (by weight)
				lb/lbf·h	g/kN·s	s	m/s
Turbo-Union RB.199	turbofan		Tornado	2.5<ref name="jetenginenet"/>	70.8	1440	14120
GE F101-GE-102	turbofan	1970s	B-1B	2.46	70	1460	14400
Tumansky R-25-300	turbojet		MIG-21bis	2.206<ref name="jetenginenet"/>	62.5	1632	16000
GE J85-GE-21	turbojet		F-5E/F	2.13<ref name="jetenginenet"/>	60.3	1690	16570
GE F110-GE-132	turbofan		F-16E/F	2.09<ref name="jetenginenet"/>	59.2	1722	16890
Honeywell/ITEC F125	turbofan		F-CK-1	2.06<ref name="jetenginenet"/>	58.4	1748	17140
Snecma M53-P2	turbofan		Mirage 2000C/D/N	2.05<ref name="jetenginenet"/>	58.1	1756	17220
Snecma Atar 09C	turbojet		Mirage III	2.03<ref name="jetenginenet"/>	57.5	1770	17400
Snecma Atar 09K-50	turbojet		Mirage IV, 50, F1	1.991<ref name="jetenginenet"/>	56.4	1808	17730
GE J79-GE-15	turbojet		F-4E/EJ/F/G, RF-4E	1.965	55.7	1832	17970
Saturn AL-31F	turbofan		Su-27/P/K	1.96<ref name="flanker">"Flanker". AIR International Magazine. 23 March 2017.</ref>	55.5	1837	18010
GE F110-GE-129	turbofan		F-16C/D, F-15EX	1.9<ref name="jetenginenet"/>	53.8	1895	18580
Soloviev D-30F6	turbofan		MiG-31, S-37/Su-47	1.863<ref name="jetenginenet"/>	52.8	1932	18950
Lyulka AL-21F-3	turbojet		Su-17, Su-22	1.86<ref name="jetenginenet"/>	52.7	1935	18980
Klimov RD-33	turbofan	1974	MiG-29	1.85	52.4	1946	19080
Saturn AL-41F-1S	turbofan		Su-35S/T-10BM	1.819	51.5	1979	19410
Volvo RM12	turbofan	1978	Gripen A/B/C/D	1.78<ref name="jetenginenet"/>	50.4	2022	19830
GE F404-GE-402	turbofan		F/A-18C/D	1.74<ref name="jetenginenet"/>	49	2070	20300
Kuznetsov NK-32	turbofan	1980	Tu-144LL, Tu-160	1.7	48	2100	21000
Snecma M88-2	turbofan	1989	Rafale	1.663	47.11	2165	21230
Eurojet EJ200	turbofan	1991	Eurofighter	1.66–1.73	47–49<ref name=mtu>"EJ200 turbofan engine" (PDF). MTU Aero Engines. April 2016.</ref>	2080–2170	20400–21300

Dry jet engines, static, sea level
Model	Type	First run	Application	TSFC		Isp (by weight)	Isp (by weight)
				lb/lbf·h	g/kN·s	s	m/s
GE J85-GE-21	turbojet		F-5E/F	1.24<ref name="jetenginenet"/>	35.1	2900	28500
Snecma Atar 09C	turbojet		Mirage III	1.01<ref name="jetenginenet"/>	28.6	3560	35000
Snecma Atar 09K-50	turbojet		Mirage IV, 50, F1	0.981<ref name="jetenginenet"/>	27.8	3670	36000
Snecma Atar 08K-50	turbojet		Super Étendard	0.971<ref name="jetenginenet"/>	27.5	3710	36400
Tumansky R-25-300	turbojet		MIG-21bis	0.961<ref name="jetenginenet"/>	27.2	3750	36700
Lyulka AL-21F-3	turbojet		Su-17, Su-22	0.86	24.4	4190	41100
GE J79-GE-15	turbojet		F-4E/EJ/F/G, RF-4E	0.85	24.1	4240	41500
Snecma M53-P2	turbofan		Mirage 2000C/D/N	0.85<ref name="jetenginenet"/>	24.1	4240	41500
Volvo RM12	turbofan	1978	Gripen A/B/C/D	0.824<ref name="jetenginenet"/>	23.3	4370	42800
RR Turbomeca Adour	turbofan	1999	Jaguar retrofit	0.81	23	4400	44000
Honeywell/ITEC F124	turbofan	1979	L-159, X-45	0.81<ref name="jetenginenet"/>	22.9	4440	43600
Honeywell/ITEC F125	turbofan		F-CK-1	0.8<ref name="jetenginenet"/>	22.7	4500	44100
PW J52-P-408	turbojet		A-4M/N, TA-4KU, EA-6B	0.79	22.4	4560	44700
Saturn AL-41F-1S	turbofan		Su-35S/T-10BM	0.79	22.4	4560	44700
Snecma M88-2	turbofan	1989	Rafale	0.782	22.14	4600	45100
Klimov RD-33	turbofan	1974	MiG-29	0.77	21.8	4680	45800
RR Pegasus 11-61	turbofan		AV-8B+	0.76	21.5	4740	46500
Eurojet EJ200	turbofan	1991	Eurofighter	0.74–0.81	21–23<ref name=mtu/>	4400–4900	44000–48000
GE F414-GE-400	turbofan	1993	F/A-18E/F	0.724<ref name="uomgr">Kottas, Angelos T.; Bozoudis, Michail N.; Madas, Michael A. "Turbofan Aero-Engine Efficiency Evaluation: An Integrated Approach Using VSBM Two-Stage Network DEA" (PDF). doi:10.1016/j.omega.2019.102167.</ref>	20.5	4970	48800
Kuznetsov NK-32	turbofan	1980	Tu-144LL, Tu-160	0.72-0.73	20–21	4900–5000	48000–49000
Soloviev D-30F6	turbofan		MiG-31, S-37/Su-47	0.716<ref name="jetenginenet"/>	20.3	5030	49300
Snecma Larzac	turbofan	1972	Alpha Jet	0.716	20.3	5030	49300
IHI F3	turbofan	1981	Kawasaki T-4	0.7	19.8	5140	50400
Saturn AL-31F	turbofan		Su-27 /P/K	0.666-0.78<ref name="flanker"/><ref name="uomgr"/>	18.9–22.1	4620–5410	45300–53000
RR Spey RB.168	turbofan		AMX	0.66<ref name="jetenginenet"/>	18.7	5450	53500
GE F110-GE-129	turbofan		F-16C/D, F-15	0.64<ref name="uomgr"/>	18	5600	55000
GE F110-GE-132	turbofan		F-16E/F	0.64<ref name="uomgr"/>	18	5600	55000
Turbo-Union RB.199	turbofan		Tornado ECR	0.637<ref name="jetenginenet"/>	18.0	5650	55400
PW F119-PW-100	turbofan	1992	F-22	0.61<ref name="uomgr"/>	17.3	5900	57900
Turbo-Union RB.199	turbofan		Tornado	0.598<ref name="jetenginenet"/>	16.9	6020	59000
GE F101-GE-102	turbofan	1970s	B-1B	0.562	15.9	6410	62800
PW TF33-P-3	turbofan		B-52H, NB-52H	0.52<ref name="jetenginenet"/>	14.7	6920	67900
RR AE 3007H	turbofan		RQ-4, MQ-4C	0.39<ref name="jetenginenet"/>	11.0	9200	91000
GE F118-GE-100	turbofan	1980s	B-2	0.375<ref name="jetenginenet"/>	10.6	9600	94000
GE F118-GE-101	turbofan	1980s	U-2S	0.375<ref name="jetenginenet"/>	10.6	9600	94000
General Electric CF6-50C2	turbofan		A300, DC-10-30	0.371<ref name="jetenginenet"/>	10.5	9700	95000
GE TF34-GE-100	turbofan		A-10	0.37<ref name="jetenginenet"/>	10.5	9700	95000
CFM CFM56-2B1	turbofan		C-135, RC-135	0.36<ref name="cfm562"/>	10	10000	98000
Progress D-18T	turbofan	1980	An-124, An-225	0.345	9.8	10400	102000
PW F117-PW-100	turbofan		C-17	0.34<ref name="civjetenginenet"/>	9.6	10600	104000
PW PW2040	turbofan		Boeing 757	0.33<ref name="civjetenginenet"/>	9.3	10900	107000
CFM CFM56-3C1	turbofan		737 Classic	0.33	9.3	11000	110000
GE CF6-80C2	turbofan		744, 767, MD-11, A300/310, C-5M	0.307-0.344	8.7–9.7	10500–11700	103000–115000
EA GP7270	turbofan		A380-861	0.299<ref name="uomgr"/>	8.5	12000	118000
GE GE90-85B	turbofan		777-200/200ER/300	0.298<ref name="uomgr"/>	8.44	12080	118500
GE GE90-94B	turbofan		777-200/200ER/300	0.2974<ref name="uomgr"/>	8.42	12100	118700
RR Trent 970-84	turbofan	2003	A380-841	0.295<ref name="uomgr"/>	8.36	12200	119700
GE GEnx-1B70	turbofan		787-8	0.2845<ref name="uomgr"/>	8.06	12650	124100
RR Trent 1000C	turbofan	2006	787-9	0.273<ref name="uomgr"/>	7.7	13200	129000

Jet engines, cruise
Model	Type	First run	Application	TSFC		Isp (by weight)	Isp (by weight)
				lb/lbf·h	g/kN·s	s	m/s
	Ramjet		Mach 1	4.5	130	800	7800
J-58	turbojet	1958	SR-71 at Mach 3.2 (Reheat)	1.9<ref name="jetenginenet">Nathan Meier (21 Mar 2005). "Military Turbojet/Turbofan Specifications". Archived from the original on 11 February 2021.</ref>	53.8	1895	18580
RR/Snecma Olympus	turbojet	1966	Concorde at Mach 2	1.195<ref name="Large Turbofan Engines">Ilan Kroo. "Data on Large Turbofan Engines". Aircraft Design: Synthesis and Analysis. Stanford University. Archived from the original on 11 January 2017.</ref>	33.8	3010	29500
PW JT8D-9	turbofan		737 Original	0.8<ref name="tumde">David Kalwar (2015). "Integration of turbofan engines into the preliminary design of a high-capacity short-and medium-haul passenger aircraft and fuel efficiency analysis with a further developed parametric aircraft design software" (PDF).</ref>	22.7	4500	44100
Honeywell ALF502R-5	GTF		BAe 146	0.72<ref name="civjetenginenet">Nathan Meier (3 Apr 2005). "Civil Turbojet/Turbofan Specifications". Archived from the original on 17 August 2021.</ref>	20.4	5000	49000
Soloviev D-30KP-2	turbofan		Il-76, Il-78	0.715	20.3	5030	49400
Soloviev D-30KU-154	turbofan		Tu-154M	0.705	20.0	5110	50100
RR Tay RB.183	turbofan	1984	Fokker 70, Fokker 100	0.69	19.5	5220	51200
GE CF34-3	turbofan	1982	Challenger, CRJ100/200	0.69	19.5	5220	51200
GE CF34-8E	turbofan		E170/175	0.68	19.3	5290	51900
Honeywell TFE731-60	GTF		Falcon 900	0.679<ref name="tfe731">"Purdue School of Aeronautics and Astronautics Propulsion Web Page - TFE731".</ref>	19.2	5300	52000
CFM CFM56-2C1	turbofan		DC-8 Super 70	0.671<ref name="civjetenginenet"/>	19.0	5370	52600
GE CF34-8C	turbofan		CRJ700/900/1000	0.67-0.68	19–19	5300–5400	52000–53000
CFM CFM56-3C1	turbofan		737 Classic	0.667	18.9	5400	52900
CFM CFM56-2A2	turbofan	1974	E-3, E-6	0.66<ref name="cfm562">Élodie Roux (2007). "Turbofan and Turbojet Engines: Database Handbook" (PDF). p. 126. ISBN 9782952938013.</ref>	18.7	5450	53500
RR BR725	turbofan	2008	G650/ER	0.657	18.6	5480	53700
CFM CFM56-2B1	turbofan		C-135, RC-135	0.65<ref name="cfm562"/>	18.4	5540	54300
GE CF34-10A	turbofan		ARJ21	0.65	18.4	5540	54300
CFE CFE738-1-1B	turbofan	1990	Falcon 2000	0.645<ref name="civjetenginenet"/>	18.3	5580	54700
RR BR710	turbofan	1995	G. V/G550, Global Express	0.64	18	5600	55000
GE CF34-10E	turbofan		E190/195	0.64	18	5600	55000
General Electric CF6-50C2	turbofan		A300B2/B4/C4/F4, DC-10-30	0.63<ref name="civjetenginenet"/>	17.8	5710	56000
PowerJet SaM146	turbofan		Superjet LR	0.629	17.8	5720	56100
CFM CFM56-7B24	turbofan		737 NG	0.627<ref name="civjetenginenet"/>	17.8	5740	56300
RR BR715	turbofan	1997	717	0.62	17.6	5810	56900
GE CF6-80C2-B1F	turbofan		747-400	0.605<ref name="Large Turbofan Engines" />	17.1	5950	58400
CFM CFM56-5A1	turbofan		A320	0.596	16.9	6040	59200
Aviadvigatel PS-90A1	turbofan		Il-96-400	0.595	16.9	6050	59300
PW PW2040	turbofan		757-200	0.582<ref name="civjetenginenet"/>	16.5	6190	60700
PW PW4098	turbofan		777-300	0.581<ref name="civjetenginenet"/>	16.5	6200	60800
GE CF6-80C2-B2	turbofan		767	0.576<ref name="civjetenginenet"/>	16.3	6250	61300
IAE V2525-D5	turbofan		MD-90	0.574<ref name="jenkinson">Lloyd R. Jenkinson & al. (30 Jul 1999). "Civil Jet Aircraft Design: Engine Data File". Elsevier/Butterworth-Heinemann.</ref>	16.3	6270	61500
IAE V2533-A5	turbofan		A321-231	0.574<ref name="jenkinson"/>	16.3	6270	61500
RR Trent 700	turbofan	1992	A330	0.562<ref name=AvWeek28jan2008>"Gas Turbine Engines" (PDF). Aviation Week. 28 January 2008. pp. 137–138.</ref>	15.9	6410	62800
RR Trent 800	turbofan	1993	777-200/200ER/300	0.560<ref name=AvWeek28jan2008/>	15.9	6430	63000
Progress D-18T	turbofan	1980	An-124, An-225	0.546	15.5	6590	64700
CFM CFM56-5B4	turbofan		A320-214	0.545	15.4	6610	64800
CFM CFM56-5C2	turbofan		A340-211	0.545	15.4	6610	64800
RR Trent 500	turbofan	1999	A340-500/600	0.542<ref name=AvWeek28jan2008/>	15.4	6640	65100
CFM LEAP-1B	turbofan	2014	737 MAX	0.53-0.56	15–16	6400–6800	63000–67000
Aviadvigatel PD-14	turbofan	2014	MC-21-310	0.526	14.9	6840	67100
RR Trent 900	turbofan	2003	A380	0.522<ref name=AvWeek28jan2008/>	14.8	6900	67600
GE GE90-85B	turbofan		777-200/200ER	0.52<ref name="civjetenginenet"/><ref name="elodieroux">Élodie Roux (2007). "Turbofan and Turbojet Engines: Database Handbook". ISBN 9782952938013.</ref>	14.7	6920	67900
GE GEnx-1B76	turbofan	2006	787-10	0.512<ref name="tumde"/>	14.5	7030	69000
PW PW1400G	GTF		MC-21	0.51<ref name=AIN19aug2019>Vladimir Karnozov (August 19, 2019). "Aviadvigatel Mulls Higher-thrust PD-14s To Replace PS-90A". AIN Online.</ref>	14.4	7100	69000
CFM LEAP-1C	turbofan	2013	C919	0.51	14.4	7100	69000
CFM LEAP-1A	turbofan	2013	A320neo family	0.51<ref name=AIN19aug2019/>	14.4	7100	69000
RR Trent 7000	turbofan	2015	A330neo	0.506<ref group="lower-alpha">10% better than Trent 700</ref>	14.3	7110	69800
RR Trent 1000	turbofan	2006	787	0.506<ref group="lower-alpha">10% better than Trent 700</ref>	14.3	7110	69800
RR Trent XWB-97	turbofan	2014	A350-1000	0.478<ref group="lower-alpha">15 per cent fuel consumption advantage over the original Trent engine</ref>	13.5	7530	73900
PW 1127G	GTF	2012	A320neo	0.463<ref name="tumde"/>	13.1	7780	76300