text: Chapter 5
  5-6. Figure 5-4 depicts the Gray Eagle in a basic configuration; table 5-4 outlines air vehicle
  characteristics. More information can be found in the appropriate technical manual.
  Figure 5–4. MQ-1C Gray Eagle unmanned aircraft
  Table 5–4. MQ-1C Gray Eagle unmanned aircraft characteristics
  Specifications:
  Fuselage Length 29 feet
  Height 9 feet 8 inches
  Main Wing Span 56.3 feet
  Endurance 22+ hours without armament
  Propulsion Heavy fuel engine (1. 7 or 2. 0 liter)
  Maximum Gross Take-Off Weight 1.7L 3,200 pounds/2. 0L 3,600 pounds
  Maximum Altitude 25,000 feet above mean seal level
  Runaway Requirement 4500 feet at 9000 feet density altitude; hard
  surface only
  Cruise Airspeed 80 knots*
  Max Continuous Airspeed 130 knots
  Normal Fuel Endurance 22 hours
  Armament:
  4 Hellfire missiles
  Optics:
  Electro-optical, IR, laser pointer, laser rangefinder, laser designator, laser spot tracker
  Datalink Equipment:
  Ku SATCOM, Ku TCDL
  Additional Capabilities:
  SAR, GMTI
  Limitations:
  Aircraft endurance is reduced when armed with Hellfire missiles.
  *Varies with environmental conditions and mission factors
  IR – infrared
  SAR – synthetic aperture radar
  GMTI – ground moving target indicator
  TCDL – tactical common data link
  SATCOM – satellite communication