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词条 Lockheed L-193
释义

  1. Design and development

  2. Specifications (L-193)

  3. References

  4. External links

{{refimprove|date=October 2011}}
name= L-193 Constellation II image= L-193 Constellation II (top view).gif caption=

}}{{Infobox Aircraft Type

type= Jet airliner
Aerial refuelling tanker
national origin= United States manufacturer= Lockheed designer= first flight= introduced= retired= status= Canceled primary user= more users= produced= number built= 0 program cost= unit cost= developed from= variants with their own articles=
}}

The Lockheed L-193 Constellation II was a jet airliner design concept, designed between 1949 and 1953 with a swept wing and engines mounted at the tail. An airliner and tanker version were developed. The latter, in an aerial refueling competition initiated by the United States Air Force (USAF), won and was preferred over the Boeing KC-135 Stratotanker. Since the competing Boeing aircraft was ready to fly first, examples were ordered as an interim measure. They performed well enough that the L-193 was never ordered as a tanker, and airliner plans were dropped soon after.

Design and development

The Lockheed L-193 jet was designed between 1949 and 1953. By comparison, Boeing started producing the prototype for the Boeing 707 after the design was completed in 1952. Lockheed sought input from Trans World Airlines for the airliner's requirements[1] and several sub-variants were developed. It was a swept wing with the engines mounted at the tail. The same arrangement was later used by the Lockheed JetStar (1957), Vickers VC-10 (1962), and Ilyushin Il-62 (1963). It was designed to be slightly smaller than the Boeing 707 and Douglas DC-8 of the time.[2][3] Lockheed used features seen in its previous designs, including tip tanks similar to the Lockheed Constellation and a double-deck fuselage similar to the Lockheed Constitution.[4] The engines were also flush mounted to the fuselage, a feature dropped from most current jet designs.

In the wake of the Korean War, a competition was held in 1954 for a USAF aerial refueling tanker. A modified L-193 was chosen in 1955 to supplement the interim KC-135 tanker. The aircraft was designated "KCX-LO", and the first prototype would have been the XK-1.{{Citation needed|date=June 2010}} A prototype was ordered in February 1955. Air Force Secretary Harold E. Talbott ordered 250 KC-135 interim tankers while the selection winner was manufactured. The KC-135 was able to be delivered two years earlier than the Lockheed, and was able to be put into squadron service four years earlier. The orders for the Lockheed tanker were eventually dropped so the USAF would not have to support two separate tanker designs.[5]

Lockheed never produced its jet airliner, instead producing the modestly-successful propjet-powered Electra. Lockheed also produced the C-141 Starlifter jet cargo transport and an SST design, but did not produce a jet airliner until the L-1011 wide-body trijet. By contrast, Boeing had beat Lockheed by producing its prototype first, at its own expense, rather than waiting for the military contract, and would eventually dominate the market with a family of airliners based on the 707 and KC-135.

Specifications (L-193)

{{Aircraft specs
|ref=[6][7]
|prime units?=kts


|genhide=
|crew=5
|capacity=48 - 64
|length m=
|length ft=112
|length in=2
|length note=
|span m=
|span ft=104
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=
|height ft=36
|height in=8
|height note=
|wing area sqm=
|wing area sqft=1615
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=148000
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=


|eng1 number=4
|eng1 name=
|eng1 type=
|eng1 kw=
|eng1 hp=
|eng1 kn=
|eng1 lbf=12,200
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
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|eng2 number=
|eng2 name=
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|eng3 number=
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|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=
|max speed mph=618
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=600
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=500 to 2500 depending on configuration
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=5500
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|power/mass=
|thrust/weight=
|more performance=


|armament=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|other armament=
|avionics=
}}

References

Notes
1. ^{{cite book|title=Howard Hughes and TWA, Volume 87|author=Robert W. Rummel}}
2. ^{{cite news |title=Here Is U-2's Father|newspaper=Chicago Tribune |date=December 22, 1963}}
3. ^{{cite web|title=THE HEARTBREAK MARKET: AIRLINERS|url=http://www.generalatomic.com/jetmakers/chapter7.html|accessdate=9 October 2010}}
4. ^{{cite book|title=L-1011 TriStar and the Lockheed story|author=Douglas J. Ingells}}
5. ^"Boeing KC-135 Stratotanker -- More than just a Tanker" Robert S. Hopkins III
6. ^Of men and stars: a history of Lockheed Aircraft Corporation, 1913-1957
7. ^Flight International, Volume 59
Bibliography
{{refbegin}}
  • Air Enthusiast 126 & Secret Projects - Postwar Secret Projects
  • USAF AIRCRAFT 1947-1956 by James C. Fahey
{{refend}}

External links

  • "75 Years of In-Flight Refueling"
{{Lockheed aircraft}}

5 : Lockheed aircraft|Cancelled military aircraft projects of the United States|Quadjets|Low-wing aircraft|Air refueling

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