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P400-PRO Turbine Engine, 89 lbs Thrust, by JetCat

P400-PRO Turbine Engine, 89 lbs Thrust, by JetCat

 

Item:   JC P400-PRO
Price: $11,999.00 
$125.00 Flat Rate Ground Shipping (48 States)
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P400-PRO Turbine Engine, 89 lbs Thrust, by JetCat



JetCat PRO engines provide the highest level of integration and maximum ease of installation. Engine sided fully integrated (no further external equippment necessary):



  • ECU (Electronic control unit), watertight conformal coated.

  • Brushless fuel pump (completely sealed, salt water resistant, high efficient)

  • Internal routed EGT probe (easily user replaceable).

  • Electric starter (user replaceable).

  • Direct Kerosene startup.

  • Shut-Off valves (solenoids) for main fuel and start fuel.

  • Threaded fuel supply connection via 8mm tubing, internal fuel filter.

  • 4-pin “Power-Bus” expansion connector (e.g. for direct connection of a smoker pump, or additional fuel transfer pump)

  • Power supply: 3-4 cell LiFePo, 3-cell Lipo, 6cell Lead battery (=8-15V DC/ @25A peak)

  • Control interface options: Analog (e.g. 0-5V), 1 or 2x Servo PWM, RS232, RS485, CAN-Bus (control and data reporting)

  • Precise calibrated “fuel consumed/rest fuel” estimation and report

  • Electrical connection via 2x pigtail cables/connectors (Power & data/control)

  • Control cable connector: Autosport (9-pin) on 35cm pigtail, other connectors are also possible.


Options:



  • Bleed air port (e.g. for pressurisation of fuel tanks)

  • Brushless generator / starter (alternator) with integrated stabilized voltage output (e.g 80W @12.5V, different voltages/powers available on request).

  • Additional high power, 3-phase AC output (e.g. 500W/1000W @9-36VAC).

  • Autonomous charge/control /buffering of connected supply battery

  • Water tight sealed brushless alternator/starter

  • Salt water resistant engine shaft and bearings (for seawater recovery)
  • Idle RPM: 30000
  • Max RPM: 98000
  • Thrust at idle (N): 14
  • Thrust at idle (lbs.): 3.15
  • Thrust @ max RPM (N): 397
  • Thrust @ max RPM (lbs.): 89.25
  • EGT range (°C): 480-750
  • Pressure Ratio: 3.8
  • Mass Flow (kg/s): 0.67
  • Exhaust Gas Velocity (km/h): 2122
  • Exhaust Gas Power Output (kW): 116.4
  • Fuel Consumption @ max RPM(ml/min): 1300
  • Fuel Consumption @ max RPM (kg/min): 1.04
  • Fuel Consumption @ max RPM (oz/min): 43.96
  • Fuel Consumption @ idle (ml/min): 200
  • Fuel Consumption @ idle (kg/min): 0.16
  • Fuel Consumption @ idle (oz/min): 6.76
  • SFC @ max RPM (kg/Nh): 0.158
  • Weight (g): 3650
  • Weight (lbs.): 8.05
  • Diameter (mm): 148.4
  • Diameter (.in): 5.84
  • Length (mm) incl. starter: 353
  • Length (.in) incl. starter: 13.9

Operating Conditions:

  • Maximum Startup Altitude: 2600m (@STP)
  • Maximum Operating Altitude: 10000m / 32800ft
  • Fuel: Jet-A1 with 5% oil
  • Max Axial (Forward) Acceleration: 25G

*All data at STP +/- 3% ; STP: Standard temperature and pressure: 15°C, 1013mbar

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