Altitude Concorde

CONCORDE SSTSIM -- B38

ROUTE INFORMATION

For detailed instructions on how to fly this aircraft, see the Aircraft Operation Manual
and Simulator Tutorial documents located in the aircraft’s folder.

Technical Specifications:

Performance

Weights

Powerplant

Cruise Chart:

Cruise/Climb Performance Chart

Descent and Landing Charts:

Descent Chart

Descent to FL410

Autoland Max Winds

Landing V_REF Speeds

Performance
Maximum Operation Cruise Speed	Mach 2.04 (1350 mph)
Maximum Permissable Range	4500 miles (3900 nm)
Average Take-Off Speed	250 mph
Average Landing Speed	185 mph
Maximum Landing Gear Speed	270 kts
Maximum Operating Altitude	60,000 ft
Maximum Visor Down Speed	325 kts
Maximum Nose Down 5° Speed	325 kts
Maximum Nose Down 12.5° Speed	270 kts below FL200
Maximum Fuel Jettison Speed Mach	0.93
Maximum Total Air Temp (TMO)	127° C (Nose)

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Weights
Max Zero Fuel Weight	203,000 lbs (92,080 kgs)
Operating Weight Empty	173,500 lbs (78,700 kgs)
Max Payload	29,500 lbs (13,380 kgs)
Max Take-Off Weight	408,000 lbs (185,000 kgs)
Max Taxi Weight	412,000 lbs (186,880 kgs)
Max Landing Weight	245,000 lbs (111,130 kgs)
Max Weight of Fuel	26,400 gal (95,680 kgs)

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Powerplant
Engine Model	Olympus 593 Mrk610 turbojet
Engine Manufacturer	Rolls-Royce/SNECMA
Max thrust at TO (per engine)	38,050 lbs (w/ afterburner)
Max thrust at supersonic cruse (per engine)	10,000 lbs
Fuel Type	A1 Jet fuel
Fuel Capacity	26,400 gal /95,680 kgs
Fuel Consumption (at Idle Power)	1100 kgs/hr (302 Gallons/hr)
Fuel Consumption (at Full Power)	10500 kgs/hr (2885 Gallons/hr)
Fuel Consumption (at Full Re-heated power)	22500 kgs/hr (6180 Gallons/hr)

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Cruise/Climb Performance Chart
ISA	-30	-20	-15	-10	-5	0	+5	+10	+15
FL600	125	115	110	105	100	095	095	-	-
FL580	135	125	120	115	110	105	100	095	-
FL560	150	135	130	125	120	115	115	105	095
FL540	165	150	145	135	130	130	125	115	105
FL520	165	165	160	150	145	140	135	130	115

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CONSTANT ALTITUDE DECELERATION AND DESCENT ISA + 5° C AND ABOVE
				DISTANCE COVERED (nm)
FLIGHT LEVEL	MEAN TAS (kts)	FUEL (kg)	TIME (min)	50 KT HEAD	ZERO WIND	50 KT TAIL
600	618	2690	19	174	189	204
580	609	2630	19	172	186	201
560	603	2570	18	169	184	198
540	597	2550	18	166	180	194
520	590	2530	18	161	174	188
500	579	2510	17	155	167	181
480	564	2430	17	143	155	168
460	470	1850	13	91	101	110
450	467	1820	13	89	98	107
430	456	1770	12	83	92	101
410	445	1720	12	78	86	95
390	438	1670	11	73	81	89
370	430	1620	11	69	76	84
350	418	1580	10	65	71	79
330	410	1550	10	61	67	75
310	406	1520	9	57	63	69
290	400	1490	9	52	58	64
270	395	1460	8	48	54	59
250	382	1430	8	44	49	54
230	375	1400	7	40	45	50
210	367	1370	7	37	41	45
190	364	1340	6	33	37	41
170	354	1300	6	30	33	37
150	341	1270	5	27	29	32
130	326	1240	5	23	25	28
110	322	1210	4	20	22	24
100	316	1190	4	19	20	22
90	377	120	2	11	12	14
70	372	90	1	8	9	10
50	367	60	1	5	6	7
30	362	20	1	2	2	3
* Lookup current altitude then lookup descent altitude * Subtract the two figures to obtain descent distance * Add the difference between ISA and +5° C. Add this figure to the decsent distance obtained in the previous step.

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CONSTANT ALTITUDE DECELERATION AND DESCENT TO FL410 AND M1.00 ISA + 5° C AND ABOVE
*PROCEDURE:*
DECELERATE TO 35O KT IAS AT 350 KT IAS, DESCEND TO FL410 DECELERATE AT CONSTANT ALTITUDE TO M1.00
FLIGHT LEVEL	FUEL (kg)	TIME (min)	MEAN TAS (kts)	DISTANCE COVERED (nm)
				TAILWIND (kts)						HEADWIND (kts)
				100	80	60	40	20	SA	20	40	60	80	100
600	950	7.8	853	123	121	118	116	114	111	108	106	102	100	97
590	940	7.7	854	121	118	116	114	112	109	107	104	101	98	96
580	930	7.6	846	119	116	114	112	110	107	105	102	99	96	94
570	900	7.4	848	116	114	111	110	108	105	103	100	97	95	92
560	900	7.4	838	114	112	109	108	106	103	101	99	96	93	91
550	910	7.3	837	113	110	108	107	105	102	100	98	95	93	90
540	910	7.2	843	111	109	107	105	103	101	98	96	94	92	90
530	900	7.0	842	108	106	104	102	100	98	96	93	91	89	87
520	890	6.8	840	105	103	101	99	97	95	93	91	89	87	85
510	880	6.6	838	101	99	98	96	94	92	90	88	86	84	82
500	870	6.3	840	98	96	94	92	90	88	86	85	83	81	79
490	830	5.9	836	91	89	87	86	84	82	80	79	77	75	73
480	780	5.6	816	84	82	81	79	78	76	74	73	71	69	68
470	740	5.2	810	78	76	75	73	72	70	69	67	66	64	63

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*AUTOLAND MAX WINDS*
HEAD	25 kts
TAIL	10 kts
CROSS	15 kts

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LANDING V_REF SPEEDS
LANDING WEIGHT (kg)	V_REF
96 ...................	................... 150
98 ...................	................... 152
100 ...................	................... 154
102 ...................	................... 155
104 ...................	................... 157
106 ...................	................... 158
108 ...................	................... 160
110 ...................	................... 161
111 ...................	................... 162
115 ...................	................... 165
120 ...................	................... 168
125 ...................	................... 172
130 ...................	................... 175
135 ...................	................... 179
140 ...................	................... 182
145 ...................	................... 185
150 ...................	................... 188
155 ...................	................... 191
160 ...................	................... 194
165 ...................	................... 197
170 ...................	................... 201
175 ...................	................... 204
180 ...................	................... 207