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Air 22
05-09-2008, 09:07 AM
Had this spare eng at the office...:eek!:This HP will undoubtedly be Very Faaaaaaaaast to drive:drive::eek::thumbsup: Beefing up the stringers as we speak...:smash::cool:

Technical data

The AE3007 turbofan engine is a high bypass (5:1), two spool, axial-flow engine, flat rated at 7,580 pounds of thrust, uninstalled, sea level static to 113F ambient temperature.

The design features include:

wide-chord single-stage direct-drive fan
14-stage axial-flow compressor with inlet guide vanes (IGVs) and five variable-geometry-stator stages
full annular type combustion liner with 16 fuel nozzles and two high tension igniters
two-stage HP turbine driving the HP compressor
three-stage LP turbine to drive the fan
dual aircraft mounted, fully-redundant FADECs
accessory-drive gearbox for engine-driven accessories and air system for aircraft pressurisation, engine starting, and cross bleed starts

The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so fast, on so little.

Specifications & Weights
ENGLISH (METRIC)

Maximum Cruise Speed M = 0.92 @ ISA, 37.000 ft (11,278 m) at 30,000 lbs (13,608 kg) mid-cruise weight

Ceiling 51,000 ft (15,545 m) maximum certified

Airspeed Limits Vmo.........350 KIAS (649 km/hr)
Mmo.........0.92

Pressurization Pressure Differential 9.3 psi

Range 3,070 nautical miles (5,686 km) with full fuel and 36,100 lbs (16,375 kg) takeoff weight

Engine Rolls Royce AE3007C1
Takeoff Thrust 6,764 lbs (30.09 kN)

Outside Dimensions Overall length 72 ft 4 in (22.04 m)
Overall height 19 ft 3 in (5.86 m)
Wingspan 63 ft 11 in (19.48 m)

Cabin Dimensions (with typical interior installed) Length (Bulkhead to Bulkhead): 353 in (8.97m)
Height: 68.0 in (1.73m)
Width: 66.0 in (1.68m)

Design Weights & Fuel Capacity
ENGLISH (METRIC)
Maximum ramp weight 36,400 lbs (16,510 kg)
Maximum takeoff weight 36,100 lbs (16,375 kg)
Maximum landing weight 31,800 lbs (14,424 kg)
Maximum zero fuel weight 24,400 lbs (11,068 kg)
Maximum fuel capacity (usable) @ 6.7 lbs/gal. 12,938 lbs (5,869 kg)
Approximate empty weight* 21,700 lbs (9,843 kg)
Two crew and furnishings 400 lbs (181 kg)
Total operating weight empty 22,100 lbs (10,024 kg)
Useful payload and fuel at ramp (over crew) 14,300 lbs (6,486 kg)
Payload with full fuel 1,362 lbs (617 kg)
*Approximate empty weight includes aircraft avionics, typical options, interior, engine oil, trapped fluids, and unusable fuel.
Note: Performance conditions are based on the International Standard Atmosphere.

Carl C
05-09-2008, 09:17 AM
It's a good thing it will be too fast for anyone to get close to the jet blast:eek!:. If the water cops come up just turn on the afterburner.....Toasty Coasties:smash:. Oh, sorry, you work for them don't you?

Kidding aside, I can see more jet turbines in boating's future.

Carl C
05-09-2008, 09:22 AM
Have you checked out the "QSST" (Quiet Supersonic Transport). A civilian jet that can go mach 1.6. Not produced yet but looks like it will be. Google QSST for pics and info.

Air 22
05-09-2008, 09:27 AM
Have you checked out the "QSST" (Quiet Supersonic Transport). A civilian jet that can go mach 1.6. Not produced yet but looks like it will be. Google QSST for pics and info.


Carl..Yes I have seen that..Our company will deploy them for our customers when a builder produces them...:wink: We have customers that want it:cool: Very kool stuff indeed:thumbsup: