Some Basic Data

Engine	SLS Thrust	SLS SFC	Max Diam	Length	Wt	BPR	Cruise sfc	Applications
ALF502R-6	7500	0.415	50	65.6	1375	-	-	Bae-146
TFE731-2	3500	0.493	39.4	51	725	2.67	0.87	Citation
TFE731-20	3650	0.441	39.4	51	885	-	-	Lear 45
BR710	20000	0.39	52.9	87	3520	-	-	G-V, Global Express
AE3007	7580	0.39	43.5	106.5	1581	-	-	Citation10, Embraer RJ145
CFM56-2-C1	22200	0.36	72	95.7	4635	6	0.64	A340
CF34-3B	9220	0.35	49	103	1670		-	Canadair Challenger, RJ
CF6-80C2B1F	58000	0.316	106	168	9499		0.605	B747-400
GE90-90B	90000		134	204	16644	9	.55 (est)	B777-200/300
GEnx-2B67	66500	0.27 (est)	127	185	--	10	--	B787-8
Trent 1000-A1	63800	--	112	153	11924	10	--	B787-8
V2500-A1	25000	0.36	67.5	126	5210	5.4	0.543	A319-321
RB211-524H	60600		86.3	125	9499	4.1	0.603	747-400 / 767-300
Tay 620	13850	0.43	60	102	3185	3.04	0.69	Fokker 70/100
Trent 800	92000	0.35	110	172	14400	6.5	0.56	777
JT8D-217	20850	0.53	56.3	154	4430	1.74	0.71	MD-80
PW2037	38250	0.33	84.8	146.8	7160	5.8	0.563	757, C-17
PW4098	98000		112	191.7	16165	5.8	.56 (est)	777
FJ44-1	1900	0.456	20.9	41.9	445			CitationJet
FJ44-2	2300		23.7	40.2	448	3.28		Raytheon Premier
JT3-D-7	19000	0.55	52.9	134.4	4300		0.79
JT8D-11	15000	0.62	43	120	3310		0.82
JT9D-3A	43500	0.346	95.6	128.2	8608		0.6
ADP	65500		120	200	9500	12	0.53	Hypothetical 2015 Engine
ADP	70000		144	200	12500	20	0.49
GE4	69000	0.9	90	296.04	13243		1.47	B2707 SST Design Mach 2.7
GE21J11B14	65000	0.8	74.16	282			1.35	SCAR study Mach 2.6
Olympus 593	38000	1.39	49	150	6780		1.195	Concorde
TBE-M1.6	70600	0.875			9252		1.12	NASA MACH 1.6 STUDY
TBE-M2.0	69000	0.873			9278		1.2	NASA MACH 2.0 STUDY
TBE-2.4	65500	0.929			9587		1.31	NASA MACH 2.4 STUDY
Rolls VCE	49460	0.55					1.1	HSCT Design Study
Rolls Tandem	49460	0.55					1.09	HSCT Design Study