수직이착륙형고속비행무인기로임무효율성및운용편의성증대 자동수직이착륙으로높은운용성 ( 고정익대비 ) 고도 / 속도 / 체공성능우월로임무효율성제고 ( 회전익대비 ) EO/IR, LRF 탑재및임무장비교체가능한다목적용무인기

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Maximilian Gordon
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헬기처럼뜨고비행기처럼나는수직이착륙형고속무인항공기 KUS-TR 수직이착륙틸트로터무인항공기

2 m 순항속도 200 km/h 자동수직이착륙으로높은운용성 ( 고정익대비 ) 고도 / 속도

탑재및임무장비교체가능한다목적용무인기 최대중량 Payload 엔진 200 kg 30 kg

1 헬기처럼뜨고비행기처럼나는수직이착륙형고속무인항공기 KUS-TR 수직이착륙틸트로터무인항공기 천이비행 순항비행 천이비행 수직이륙 수직착륙 틸트로터천이비행 개요 제원 / 성능 수직이착륙형고속비행무인기로임무효율성및운용편의성증대 전장 3.5 m 최대속도 250 km/h 특징 전폭 5.2 m 순항속도 200 km/h 자동수직이착륙으로높은운용성 ( 고정익대비 ) 고도 / 속도 / 체공성능우월로임무효율성제고 ( 회전익대비 ) EO/IR, LRF 탑재및임무장비교체가능한다목적용무인기 최대중량 Payload 엔진 200 kg 30 kg 55 마력로타리 최대고도운용반경운용시간 4.5 km 60~200 km 6 h 용도 군사용 : 해상 / 육상부대원거리정찰 / 감시및표적획득용 민간용 : 해안 / 산불 / 환경감시및재해 / 재난모니터링

2 Takes off like a rotary aircraft and flies like a fixed wing aircraft KUS-TR Tilt-Rotor VTOL UAV Transition Cruise Transition Vertical Take-off Vertical Landing Tilt rotor Transition Mode Overview Technical Specification High speed VTOL UAS providing high efficiency in mission & operation Length 3.5 m Max. Speed 250 km/h Key Features Autonomous Flight and VTOL provides high operational efficiency Provide aerodynamic advantages in ceiling, speed and endurance compare to rotary VTOL UAVs Versatile UAV with EO/IR, LRF and changeable extra payload system Width MTOW Payload Engine 5.2 m 200 kg 30 kg 55 HP Rotary Cruise Speed Ceiling Range Endurance 200 km/h 4.5 km 60~200 km 6 hrs Usage Military : Tactical ISR(Intelligence, Surveillance and Reconnaissance), communication relay and/or electronic warfare Civil : Maritime, border, environment and scientific surveillance & monitoring

3 산악야지최적운용성보장, 고성능전술급무인항공기 KUS-DUAS 사단정찰용무인항공기 개요 대한항공이체계개발중인사단정찰용무인항공기 특징 산악 / 야지의협소지역운용가능 ( 발사대이륙, 후크제동착륙 ) - 활주로가용시활주이착륙가능 ( 휠또는스키드착륙 ) 낮은착륙속도를통한착륙거리최소화 군용항공기감항인증기준적용으로안전신뢰도증대 용도 육군 / 해병대사단급부대의정찰감시및표적획득 해군 / 해양경찰등의해상정찰감시및표적획득 제원 / 성능 전장 3.4 m 최대속도 전폭 4.2 m 순항속도 최대중량 150 kg 최대고도 0 km Payload 00 kg 운용반경 00 km 엔진 38 마력로타리 운용시간 0 h

4 High performance tactical UAV, assuring optimal operability in open-fields & mountainous region KUS-DUAS Divisional Surveillance UAS Overview Divisional surveillance UAS for ROK Army & Marine Corps Key Features Optional catapult launcher and net recovery system removes geo-spatial limitation in its operation Low stall speed provides STOL capability, requiring only a 150km long runway The first airworthiness certified UAV system in Korea assuring its system reliability and safety Usage Non-stop tactical surveillance, reconnaissance, target acquisition and firepower guidance for divisions of ROK Army and Marine Corps Technical Specification Length 3.4 m Max. Speed Width 4.2 m Cruise Speed MTOW 150 kg Ceiling 0 km Payload 00 kg Range 00 km Engine 38 HP Rotary Endurance 0 hrs

5 차세대스텔스무인전투기 KUS-X 스텔스형상의무인전투기개념모델 저피탐성능의무인전투기 저피탐형상설계 RCS 감소형상설계 RAS 설계 / 적용 RAM 적용 비행제어시스템 무미익비행제어 자율비행시스템 개요 제원 / 성능 미래스텔스무인전투기개념모델 전장 10 m 최대속도 특징 전폭 16 m 순항속도 무미익 (Tailless) 비행체비행제어기술적용 레이더단면적 (RCS) 감소비행체형상설계기술적용 정밀유도무장내부탑재 전고엔진최대중량 3 m Turbo-jet 0,000 kg 최대고도운용반경운용시간 30,000 ft 000 km 6 h 용도 군사용 : 향후무인공격및폭격기로활용

Next generation stealth Unmanned Combat Aerial Vehicle KUS-X UCAV conceptual model Very Low Observable UCAV VLO Structure/Design Radar cross section reduction design Radar Absorbing Structure Radar

generation Unmanned Combat Air Vehicle Length 10 m Max.

6 Next generation stealth Unmanned Combat Aerial Vehicle KUS-X UCAV conceptual model Very Low Observable UCAV VLO Structure/Design Radar cross section reduction design Radar Absorbing Structure Radar Absorbing Material Flight Control System Tailless aircraft flight control system Advanced autonomous flight & mission control system Overview Technical Specification Conceptual model for next generation Unmanned Combat Air Vehicle Length 10 m Max. Speed Features Employees high level of autonomous flight and mission control system Application of radar signature reduction aircraft design and materials Internal payload bay for guided bombs and missiles Width Height Engine MTOW 16 m 3 m Turbo-jet 0,000 kg Cruise Speed Ceiling Range Endurance 30,000 ft 000 km 6 hrs Usage Close air support, suppression of enemy air defenses & penetration ISR

7 중고도급다목적무인항공기 KUS-15 다목적중고도무인항공기개념모델 임무다양성및상호운용성보장 다양한임무수행 감시정찰, 정밀공격 통신중계 / 전자전 신호정찰 플랫폼공동활용 비행체형상개발 지상통제장비등공동운용 개요 제원 / 성능 군 / 민수다목적용중고도급파생형무인항공기개념모델 전장 13 m 최대속도 특징 전폭 25 m 순항속도 정찰 / 감시외다양한임무수행 ( 공격, 통신중계, 전자전등 ) 공통플랫폼 (Common Platform) 활용비행체형상개발 지상또는위성중계사용 전고최대이륙중량엔진 3 m 0,000 kg 1,200 마력급 최대고도운용반경운용시간 45,000 ft 000 km 24 h 이상 용도 군사용 : 감시정찰, 정밀공격, 통신중계, 전자전, 신호정보등 민간용 : 광대역해상감시, 국경 / 환경감시등

Multi-mission Medium Altitude Long Endurance UAV KUS-15 Multi-mission MALE UAS conceptual model Mission diversity & interoperability Versatile UAS ISR, Precision Attack Communication Relay Electronic

Features Length Width Height 13 m 25 m 3 m Max.

8 Multi-mission Medium Altitude Long Endurance UAV KUS-15 Multi-mission MALE UAS conceptual model Mission diversity & interoperability Versatile UAS ISR, Precision Attack Communication Relay Electronic Warfare C2(Command & Control) SIGINT Common Platform Modular aircraft structure Universal GCS Overview Technical Specification Conceptual model for Multi-mission Medium Altitude Long Endurance UAV Features Length Width Height 13 m 25 m 3 m Max. Speed Cruise Speed Ceiling 45,000 ft Provides multi-mission capability (ISR, Attack, Communication relay and Electronic Warfare) Employees LOS and/or SATCOM datalink to enhance its operation range MTOW 0,000 kg Engine 1,200 HP Range Endurance 000 km 24 + hrs Usage Military : ISR, Precision attack, Communication relay, EW & SIGINT, C2 Civil : Maritime, Border, Environment and scientific surveillance & monitoring

Republic of Korea Airworthiness Certification of Unmanned Aerial System

Republic of Korea Airworthiness Certification of Unmanned Aerial System Name : Maj. Na, Kyeong-min(ROK), Hwang, Ki-Lyong(KAL) E-mail : kminn@korea.kr, klhwang@koreanair.com Contents PART I Introduction