제원

Specifications
Performance Factors: EC-135 EC-18B
Max Takeoff Gross Wt (lb): 300,500 326,000
Normal Cruise Speed (kt TAS): 430 450
Max Cruise Speed (kt TAS): 490 470
Nominal Support Speed -
30kft (kt TAS): 360/420 360/420
Nominal Turning Radius -
30 kft, 30 deg bank (nm): 3.3/4.5 3.3/4.5
Minimum Turning Radius -
30 kft, 45 deg bank (nm): 1.9/2.6 1.9/2.6
Nominal Turn Time, 180 deg -
30 kft, 30 deg bank (min): 1.7/1.8 1.7/1.8
Minimum Turn Time, 180 deg -
30 kft, 45 deg bank (min): 1.0/1.2 1.0/1.2
Nominal Operating Altitude (ft MSL): 30,000 30,000
Maximum Operating Altitude (ft MSL): 33,000 42,000
Mission Operating Altitude (ft MSL): 5,000 to 33,000 500 to 42,000
Range The range capability of the ARIA is influenced by:
Aerial refueling capability
Runway length, obstacle clearance, and noise abatement restrictions
Runway elevation
Runway air temperature
Distance to alternate base
Fuel reserve requirements
Enroute wind conditions
Aircraft altitude during data run
Application of the above factors to some 25 worldwide airports produces maximum ranges varying from 2,800 to 4,500 nm without aerial refueling. Two ARIA currently have the capability to take on fuel while in flight. This greatly extends the maximum attainable range.
Navigation Dual TACAN
Dual VOR
ADF radio
Omega
N-1 compass system*
True airspeed indication system
APN-59 search radar on EC-135E; RDR-1F on EC-18B
APN-218 Doppler radar*
Periscopic sextant
Dual Inertial Navigation System (INS)
Global Positioning System (GPS)
*EC-135E only