USS 노스 캐롤라이나 BB-55

USS North Carolina (BB-55)

국가미국
수업노스캐롤라이나급 전함
시작1940년 6월 13일
해제1947년 6월 27일

USS 노스캐롤라이나 (BB-55)는 노스 캐롤라이나급 전함의 주함이며 미국 해군의 네 번째 군함으로, 노스캐롤라이나 주의 이름을 따서 명명되었다. 그것은 제 2 차 세계 대전 중에 서비스에 들어간 최초의 새로 건설 된 미국 전함이었으며 태평양 작전 극장의 모든 주요 해군 공세에 참여했습니다. 그것의 15 전투 별은 그녀를 차 세계 대전의 가장 장식 된 미국 전함으로 만들었습니다.

소스: USS 노스 캐롤라이나 위키 백과에

USS North Carolina BB-55 Walk Around
PhotographerVladimir Yakubov
LocalisationWilmington, NC
Photos517
잠깐, 당신을 위해 USS 노스 캐롤라이나 검색 ...

참고 항목:

World War II: The Definitive Visual History from Blitzkrieg to the Atom Bomb(DK Definitive Visual Histories) - 아마존 지도별 제2차 세계 대전 지도(DK History Map by Map) - 아마존

USS 노스 캐롤라이나 (BB-55) : 제 2 차 세계 대전 전투에서 박물관 선박까지 (Legends of Warfare: Naval, 4) - 아마존


General Characteristics and Role

The Boeing X-36 Tailless Fighter Agility Research Aircraft was an experimental subscale jet developed by McDonnell Douglas (later Boeing) for NASA and the US Air Force in the mid-1990s. Its primary role was to test the feasibility of a fighter aircraft design that lacked the traditional vertical and horizontal tail surfaces. The X-36 was intended to explore how a tailless configuration could enhance stealth (by reducing radar cross-section) and improve maneuverability, particularly at high angles of attack, compared to conventional fighter jets. It was flown remotely by a pilot in a ground station due to its small size and lack of a cockpit.

Property Typical Value (X-36)
역할 Experimental Aircraft (Agility and Stealth Research)
National Origin 미국
제조업체 McDonnell Douglas / Boeing
First Flight 17 May 1996
Pilot/Control Unmanned, remotely controlled from a ground cockpit.
길이 5.77 m (18 ft 11 in)
윙스 팬 3.17 m (10 ft 5 in)
높이 0.95 m (3 ft 1 in)
Max Takeoff Weight 567 kg (1,250 lb)

Powerplant and Flight Controls

  • Engine: 1 x Williams International F112 turbofan engine.
  • Thrust: Approx. 3.1 kN (700 lbf).
  • Top Speed: Estimated at 370 km/h (230 mph).
  • Flight Control System: Required a highly advanced Digital Fly-By-Wire (DFBW) system to maintain stability, as the aircraft was inherently unstable without tail surfaces.
  • Control Surfaces: Yaw and pitch control were achieved using canards (foreplanes) and a combination of split ailerons (flaperons) and a **thrust-vectoring nozzle** on the engine.

Program Outcome and Legacy

  • Test Program: The X-36 completed a highly successful test program, demonstrating excellent maneuverability with its tailless design. It achieved a total of 31 flights, logging 15 hours of air time.
  • Success Metric: The program demonstrated that a tailless fighter design could achieve up to a 40% increase in cruising lift and a significant improvement in agility over conventional designs.
  • Influence: Although the X-36 never led directly to a production aircraft, its successful demonstration of control and stability heavily influenced subsequent low-observable (stealth) aircraft design and DFBW control systems, including possible future unmanned combat air vehicles (UCAVs).
  • Preservation: Both X-36 prototypes are now preserved: one is at the National Museum of the United States Air Force in Ohio, and the other is at the NASA Dryden Flight Research Center (now Armstrong) in California.

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