请输入您要查询的百科知识:

 

词条 Northrop N-204
释义

  1. Development

  2. Design

  3. Specifications (estimated)

  4. See also

  5. References

name = Northrop N-204image =caption =

}}{{Infobox Aircraft Type

type =High altitude reconnaissance aircraftmanufacturer = Northrop Corporationdesigner =first flight =introduced =retired =status = paper project onlyprimary user = United States Air Force (intended)more users =produced =number built = none completedunit cost =developed from =variants with their own articles =
}}

The Northrop N-204 was a high altitude reconnaissance jet aircraft designed in the United States in the 1950s.

Development

In fall 1957, Northrop submitted a proposal to the United States Air Force for a subsonic high-altitude reconnaissance aircraft, having capitalized on their earlier N-165 design study. The concerns by CIA pilots that the Lockheed U-2 was being tracked by radars on spy missions over the Soviet Union prompted Northrop to make low observable technology a part of the N-204 design, as was later done with the Lockheed A-12.[1]

Although Northrop estimated that the N-204 could go into service in 1960, the N-204 project did not proceed to the hardware stage.[1]

Design

The N-204 was similar to the Lockheed U-2 and Yakovlev Yak-25RV in having long, straight wings like an ordinary sailplane, and a v-tail. However, the engines of the aircraft were not buried in the wing roots or podded under the wings, but instead were buried in the outboard end of the wing center-section.[1]

Specifications (estimated)

{{aircraft specifications
|plane or copter?= plane
|jet or prop?= jet
|ref=[1]
|crew= two, pilot and flight engineer/RSO officer
|capacity=
|length main= 105 ft 8 in
|length alt= 32.2 m
|span main=273 ft 9 in
|span alt= 83.44 m
|height main=
|height alt=
|area main= 5,000 ft²
|area alt= 464.52 m²
|airfoil=
|empty weight main=
|empty weight alt=
|loaded weight main= 34,000 lb
|loaded weight alt= 15,422 kg
|useful load main=
|useful load alt=
|max takeoff weight main= 75,000 lb
|max takeoff weight alt= 34,019 kg
|more general=
|engine (jet)= Westinghouse J54
|type of jet=turbojets
|number of jets=8
|thrust main=6,075 lbf
|thrust alt= 27.02 kN
|thrust original=
|afterburning thrust main=
|afterburning thrust alt=
|max speed main= 480 knots
|max speed alt= 553 mph, 885 km/h
|cruise speed main=
|cruise speed alt=
|never exceed speed main=
|never exceed speed alt=
|stall speed main=
|stall speed alt=
|range main= 3,000 nm
|range alt= 3,452 mi, 5,556 km
|ceiling main= 85,000 ft
|ceiling alt= 25,908 m
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=
|avionics=
}}

See also

{{Portal|United States Air Force}}{{aircontent|
|related=
|similar aircraft=
  • Lockheed U-2
  • Martin RB-57 Canberra
  • Beriev S-13
  • Northrop N-165
  • Yakovlev Yak-25RV

|lists=
|see also=
}}

References

1. ^Chong, Tony, 2016. Flying Wings & Radical Things: Northrop’s Secret Aerospace Projects & Concepts 1939-1994. Forest Lake, Minnesota: Specialty Press.
{{Northrop aircraft}}

2 : Northrop aircraft|United States military reconnaissance aircraft 1950–1959

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/11/13 12:20:01