´ëÇÑÇ×°ø(KAL)°ú ½ÃÄݽºÅ°ÀÇ KMH

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DESIGN FEATURES: Five-blade, bearingless flexbeam main rotor and eightblade
•an-in-fin?tail rotor; two-stage transmission. Rotor brake designed to
stop and hold rotor, power off, in 74km/h winds. T tailplane.

FLYING CONTROLS: Full-authority, hydromechanical automatic flight control
system, incorporating an electronic stability augmentation system; fly-bywire
back-up system (removable for civil valiants) is incorporated in primary
AFCS to improve overall ballistic lollerance.

STRUCTURE: All-composites rotor blades. Fuselage is composites and metal
mix, with built-in crashworthiness. Front of fuselage employs 'anti-ploughing'
structure to prevent nose from digging into soft ground in event of hard
landing or crash. Crushable floor structure to attenuate energy and reduce
vertical crash g loadings on occupants.

LANDING GEAR: Non-retractable tailwheel type, capable of absorbing 3.05m/
s descent rate at design MTOW.

POWER PLANT: TWO LHTEC T800 series turboshafts (each 1,014kW for T-O
and 1,204kW max contingency). Transmission rating 1.342kW. Self-sealing,
crashworthy fuel tanks with explosion suppression and with non-return valves
to minimise leakage in a crash.

ACCOMMODATION: Two-man flight deck in utility version, with pilot and copilot
side by side in armour-protected seats; two crew members at gunner
positions adjacent to cabin windows; up to 10 fully equipped troops or four
stretchers plus two attendants in main cabin. Pilot and co-pilot/gunner in
tandem in attack version. Crew and passenger seats all crashworthy.

AVIONICS: Comms (both versions): VHF AM/FM, UHF AM, HF, Mode 4 IFF,
intercom and voice security standard; satcom optional.
Flight (both versions): AFCS with digital three-axis autopilot, GPS/INS, VOR/
ILS and radar altimeter standard; Doppler navigation and ADF Tacan
optional.
Mission: Pilotage FUR in both versions, plus PLS (utility version) or TADS and
helmet-mounted display (attack version).
Self-defence: RWR, IRCM and chaff/flare dispenser standard in both versions;
LWR and MWR standard for attack version, optional for utility.

ARMAMENT (utility version): External pylon can be fitted on each side of
cabin for variety of stores, including 12.7mm in self-contained gun pods; or
two rocket pods; or ASMs. Two pintle mounts adjacent to cabin windows each
side, each for a 12.7mm gun or 7.62mm six-barrel Minigun.

ARMAMENT (attack version): Electrically operated, three-barrel 20mm
undernose turret gun with up to 750 rounds; either crew member can fire
this gun, which can be slaved to a helmet-mounted sight or other aiming
device. Four underwing hardpoints for up to 12 Hellfire or Hellfire 2 anti-tank
missiles; or 52 x 70mm FFAR; or 16 AAMs and their launchers; or a
combination of these weapons.

Technical data for KAL KMH (utility)
Main rotor diameter: 11.89m, tail rotor diameter: 1.37m, length overall: 14.45m, height overall: 3.86m, max. take-off weight: 5,896kg, empty weight: 3,243kg, max cruising speed: 278km/h, hovering ceiling OGE: 3,355m, max range: 814km

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