text: Chapter 5
  Table 5–5. RQ-7B Shadow unmanned aircraft system characteristics
  Specifications:
  Length RQ-7Bv1: 11 feet 4 inches
  RQ-7Bv2: 12 feet
  Height 3 feet 2 inches
  Main Wing Span RQ-7Bv1: 14 feet
  RQ-7Bv2: 20 feet 5 inches
  Endurance RQ-7Bv1: 5+ hours
  RQ-7Bv2: 8+ hours
  Maximum Gross Take-Off Weight: RQ-7Bv1: 404 pounds
  RQ-7Bv2: 467 pounds
  Maximum Altitude 15,000+ feet mean sea level
  Launch and Recovery Requirements 220 meters by 50 meters area; may land on
  unimproved surfaces
  Cruise Airspeed 70-80 knots
  Max Dash Airspeed 110 knots
  Normal Fuel Endurance RQ-7Bv1: 6 hours
  RQ-7Bv2: 9 hours
  Optics:
  Electro-optical, IR, and laser pointer/laser rangefinder and laser designator.
  Datalink Equipment:
  RQ-7Bv1 S-band/UHF-band
  Video: C-band
  RQ-7Bv2–TCDL TCDL Ku-band/
  UHF-band
  Video: UHF-band
  Additional Capabilities:
  Laser classification: Class IV designator, Class III-b rangefinder, Class III-b pointer
  Frequency modulation radio communications relay package
  Limitations:
  Aircraft uses 100 low lead aviation gasoline. Aircraft is sensitive to weather conditions. Dust, rain, and
  low ceilings ground aircraft.
  IR-infrared
  TCDL-tactical common data link
  UHF-ultra high frequency
  C-12 SERIES AIRCRAFT
  5-9. The C-12 series of aircraft are pressurized, low wing, all metal aircraft powered by two PT6A-42
  turboprop engines. The aircraft has all-weather capability and is distinguishable by its slender, streamlined
  engine nacelles, four-blade propellers, T-tail, and dual aft body strakes. The basic mission of the aircraft is
  to provide scheduled or unscheduled air transportation of passengers and/or cargo in any area of the world.
  Figure 5-6, page 5-9, depicts the basic parameters of the C-12. Table 5-6, page 5-9, depicts characteristics.
  More information can be found in the appropriate technical manuals.