아라바 202 | |
|---|---|
| 국가 | 이스라엘 |
| 역할 | 경량 STOL 수송 항공기 |
| 첫 비행 | 1969년 11월 27일 4 |
| 내장 | 103 |
항공기 아라바 202 Israel Aerospace Industries (IAI)에서 설계 및 제조 한 단거리 이륙 및 착륙 (STOL) 유틸리티 수송 항공기입니다.
소스: 위키의 Arava 202
| Arava 202 Walk Around | |
|---|---|
| 사진 작가 | 아이작 거쉬먼 |
| 로컬라이제이션 | Unknow |
| 사진 | 51 |
Arava 202 01
Arava 202 02
Arava 202 03
Arava 202 04
Arava 202 05
Arava 202 06
Arava 202 07
Arava 202 08
Arava 202 09
잠깐, 당신을 위해 Arava 202 사진 검색 ...
커피 사줘
참고 항목:
General Characteristics
The IAI Arava is a twin-engine, high-wing, short takeoff and landing (STOL) utility transport aircraft, and was Israel Aircraft Industries’ (IAI) first major indigenous aircraft design to enter production. The Arava 202 is an improved version, featuring a slightly longer fuselage and distinctive Whitcomb winglets for better aerodynamic efficiency.
| Property | Typical Value (IAI-201/202 Variant) |
|---|---|
| 역할 | STOL Utility / Military Transport |
| 제조업체 | Israel Aircraft Industries (IAI) |
| First Flight (Arava Series) | November 27, 1969 |
| 승무원 | 2 pilots |
| Capacity (Troops) | 24 fully equipped troops or 16 paratroopers |
| 윙스 팬 | 20.96 m (68 ft 9 in) |
| 길이 | 13.03 m (42 ft 9 in) (202 is slightly longer than 201) |
| Max Takeoff Weight | 6,804 kg (15,000 lb) |
| Units Built (Total) | ~103 (Production ended 1988) |
Design and Powerplant
- Engines: Two Pratt & Whitney Canada PT6A-34 turboprop engines (or PT6A-36 on the 202 prototype).
- Power Output: 559 kW (750 shp) each.
- Fuselage Design: Features a unique, short, barrel-like fuselage with a high wing and twin tail booms extending from the engine nacelles.
- Loading Access: The entire rear section of the fuselage is hinged and swings open to the side, allowing for easy and rapid loading/unloading of bulky cargo or vehicles.
- Landing Gear: Fixed tricycle landing gear, chosen to save weight and complexity, ideal for rough-field operations.
- 202 Specifics: The IAI-202 variant featured a longer fuselage, modified wings, and distinctive Whitcomb winglets at the wingtips for reduced drag.
Performance and Capability
- Max Cruise Speed: 319 km/h (176 knots, 198 mph) at 3,050 m (10,000 ft).
- Maximum Range: Approximately 1,056 km (570 nautical miles) with max fuel.
- Payload Capacity: 2,351 kg (5,184 lb) of cargo.
- STOL Takeoff Distance: Approximately 463 m (1,520 ft) to clear a 50 ft obstacle.
- Service Ceiling: 7,620 m (25,000 ft).
- Military Roles: Besides transport, military Aravas could be fitted with side-firing machine guns and rocket pods for counter-insurgency/gunship roles.
전망 : 862
