Team # 강준홍 김상민 박창연 이재형 전중수

Part 5 : Performance Part 4 : Electric Part 3 : Sub - System Part 2 : Air vehicle Part 1 : System Project Overview 조원소개, Project 목적

Chief engineer & Performance engineer 김상민 Air vehicle engineer 이재형 Sub system engineer 전중수 Electric engineer 박창연 Weight engineer 강준홍 RQ-7 A/B Shadow 200

우리는 왜 term project 를 하는가 ? 우리는 왜 term project 를 하는가 ? 습득된 이론적 지식 Project 실제 UAV 적용 미래 공학도로서의 자질 향상

 Army Shadow 200 UAV  Developed 1999  Used in Iraq  Remove pilots from danger  Carries high-resolution video camera  Flies via GPS (Global Positioning System)  Automatic take-off and landing

Length 11.17ftMax. Speed 118 knots Wingspan 14 ftCruise Speed 90 knots Max. Gross Wt. 375 lbs.Loiter Speed 60 knots Payload Wt lbs. *Max. Altitude 15,000-19,000 ft * Data Link Range 125 kmEndurance 6-7 hrs * (options for 200 Km range)Engine 38 bhp (UEL741)

RQ-7ARQ-7B Length11.2ft (3.4m) Wingspan12.9ft14ft Height3ft Weightmax:328lb, empty:165lb max:375lb, empty:165lb Speedmax:110kts, loiter:70kts max:105kts, loiter:60kts Cruise Speed82~90kts Ceiling14000ft15000ft Range67nm Endurance5h7h PropulsionUEL AR-741 rotary engine ; 38hp Fuel capacity40liter50liter

Boom-mounted Inverted V tailLaunch and Recovery

Strong Points 레이더반사면적 (Radar Cross Section) 감소로 생존 가능성 증가 표면적 감소로 인한 항력 감소 엔진을 보호 Weak Points 단일동체보다 무거움 소음이 크다 구조가 복잡하다

Airfram e Max Speed Cruis e Speed Min. Endurance SpanEngineDry Weight Payload T-16XL Pioneer Shadow Scan Eagle Viking ~ Blue Horizon

Features Range : 30 KM Weight : 60 lbs Ruggedized Workstation GCS Compatible AV Control/Status, Map & Video on One Screen

Boom-mounted Inverted V tailLaunch and Recovery

Launch Hydraulic Rail Launch ( 유압레일발사체 ) Launch on road, runway and flat surface Recovery Auto recovery on flat terrain with arresting cables Emergency recovery with parachute