Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Lockheed_CL-1200> ?p ?o. }
Showing items 1 to 86 of
86
with 100 items per page.
- Lockheed_CL-1200 abstract "The Lockheed CL-1200 Lancer was a late 1960s company-funded proposal for a new and improved F-104 Starfighter. It was intended for the export market and was in direct competition with the Northrop F-5E Tiger II, Dassault Mirage F1, Northrop YF-17 and the McDonnell Douglas F-4F Phantom. Lockheed hoped to capitalize on its F-104 production experience through commonality of parts and systems, and minimize expenses by reusing tooling, jigs and existing factory facilities. Lockheed was also experienced in consortium production and further hoped to continue this arrangement with the CL-1200. It was projected that CL-1200 deliveries could begin in 1972.Borrowing heavily from the F-104 design the new type featured a new high-mounted, increased span wing and low-mounted, enlarged tailplanes. Both features were incorporated to improve flight handling characteristics and short-field performance. The CL1200-1 was to have used an uprated version of the F-104 engine, the General Electric J79 with a later variant known as the CL1200-2 to be powered by a Pratt and Whitney TF-30 turbofan.The CL-1200-1 was entered in the International Fighter Aircraft competition, but since the Northrop F-5 was named as the winner in November 1970, the primary market for the Lancer was lost, and the project was terminated with no examples completed.The X-27 was an experimental designation assigned by the USAF to a proposed high-performance research aircraft derived from the CL-1200 Lancer project. The X-27 was to have tested advanced technology high-performance engines and equipment. Again, the X-27 project did not proceed beyond the mock-up stage.The CL-1200-2 (sometimes referred to as the CL-1600) was a proposed development of the X-27 for entry into the Lightweight Fighter Competition in 1972. The CL-1200-2 was not proceeded with when General Dynamics and Northrop designs were given contracts for the YF-16 and YF-17. The design was similar to the X-27 but had round intakes with shock cones and a different fin.A further variant proposed for the United States Navy was designated the CL-1400 or CL-1400N. It was based on the forward fuselage, intake and wing of the CL-1200-2 with the rear fuselage of the X-27.".
- Lockheed_CL-1200 designer Kelly_Johnson_(engineer).
- Lockheed_CL-1200 manufacturer Lockheed_Corporation.
- Lockheed_CL-1200 wikiPageExternalLink getimage.htm?id=11903.
- Lockheed_CL-1200 wikiPageExternalLink monograph31.pdf.
- Lockheed_CL-1200 wikiPageExternalLink x-27-side.jpg.
- Lockheed_CL-1200 wikiPageExternalLink x-27.jpg.
- Lockheed_CL-1200 wikiPageID "1665791".
- Lockheed_CL-1200 wikiPageRevisionID "582079327".
- Lockheed_CL-1200 afterburningThrustAlt "111.2 kN".
- Lockheed_CL-1200 afterburningThrustMain "25000".
- Lockheed_CL-1200 airfoil "Bi-convex".
- Lockheed_CL-1200 areaAlt "28.0".
- Lockheed_CL-1200 areaMain "300.0".
- Lockheed_CL-1200 armament "CL-1200-2 only: * 1 × 20 mm General Electric M61 Vulcan cannon with 725 rounds, or * 1 × 30 mm DEFA cannon with 400 rounds * Up to ordnance".
- Lockheed_CL-1200 ceilingAlt "1098000.0".
- Lockheed_CL-1200 ceilingMain "In excess of 60,000 ft".
- Lockheed_CL-1200 climbRateAlt "300.0".
- Lockheed_CL-1200 climbRateMain "60000.0".
- Lockheed_CL-1200 crew "One".
- Lockheed_CL-1200 designer Kelly_Johnson_(engineer).
- Lockheed_CL-1200 emptyWeightAlt "8112".
- Lockheed_CL-1200 emptyWeightMain "17885".
- Lockheed_CL-1200 engine(jet)_ "Pratt & Whitney TF30-P-100".
- Lockheed_CL-1200 hasPhotoCollection Lockheed_CL-1200.
- Lockheed_CL-1200 heightAlt "294.0".
- Lockheed_CL-1200 heightMain "17".
- Lockheed_CL-1200 jetOrProp%3F_ "jet".
- Lockheed_CL-1200 lengthAlt "972.0".
- Lockheed_CL-1200 lengthMain "57".
- Lockheed_CL-1200 lists "* List of experimental aircraft * List of Lockheed aircraft".
- Lockheed_CL-1200 loadedWeightAlt "11061".
- Lockheed_CL-1200 loadedWeightMain "24385".
- Lockheed_CL-1200 manufacturer Lockheed_Corporation.
- Lockheed_CL-1200 maxSpeedAlt "1700".
- Lockheed_CL-1200 maxSpeedMain "1477".
- Lockheed_CL-1200 maxTakeoffWeightAlt "15900.0".
- Lockheed_CL-1200 maxTakeoffWeightMain "35000.0".
- Lockheed_CL-1200 morePerformance "* Takeoff run: 1,450 ft * Landing run: 2,060 ft".
- Lockheed_CL-1200 nationalOrigin "United States".
- Lockheed_CL-1200 numberOfJets "1".
- Lockheed_CL-1200 planeOrCopter%3F_ "plane".
- Lockheed_CL-1200 rangeAlt "420".
- Lockheed_CL-1200 rangeMain "367".
- Lockheed_CL-1200 ref "NB: These are estimated figures given by Lockheed as neither type flew.".
- Lockheed_CL-1200 related "* F-104 Starfighter".
- Lockheed_CL-1200 similarAircraft "* Dassault Mirage F1".
- Lockheed_CL-1200 spanAlt "522.0".
- Lockheed_CL-1200 spanMain "29".
- Lockheed_CL-1200 status "Cancelled at mock-up stage".
- Lockheed_CL-1200 thrustAlt "66.7 kN".
- Lockheed_CL-1200 thrustMain "15000".
- Lockheed_CL-1200 type "Interceptor".
- Lockheed_CL-1200 typeOfJet Turbofan.
- Lockheed_CL-1200 unitCost "US$ Estimated 2.4 million".
- Lockheed_CL-1200 subject Category:Abandoned_military_aircraft_projects_of_the_United_States.
- Lockheed_CL-1200 subject Category:High-wing_aircraft.
- Lockheed_CL-1200 subject Category:Lockheed_F-104_Starfighter.
- Lockheed_CL-1200 subject Category:Lockheed_aircraft.
- Lockheed_CL-1200 subject Category:Single-engined_jet_aircraft.
- Lockheed_CL-1200 type Aircraft.
- Lockheed_CL-1200 type MeanOfTransportation.
- Lockheed_CL-1200 type Product.
- Lockheed_CL-1200 type Model_airplane.
- Lockheed_CL-1200 type TransportationDevice_Vehicle.
- Lockheed_CL-1200 type DesignedArtifact.
- Lockheed_CL-1200 comment "The Lockheed CL-1200 Lancer was a late 1960s company-funded proposal for a new and improved F-104 Starfighter. It was intended for the export market and was in direct competition with the Northrop F-5E Tiger II, Dassault Mirage F1, Northrop YF-17 and the McDonnell Douglas F-4F Phantom. Lockheed hoped to capitalize on its F-104 production experience through commonality of parts and systems, and minimize expenses by reusing tooling, jigs and existing factory facilities.".
- Lockheed_CL-1200 label "Lockheed CL-1200 Lancer".
- Lockheed_CL-1200 label "Lockheed CL-1200".
- Lockheed_CL-1200 label "Lockheed CL-1200".
- Lockheed_CL-1200 label "Lockheed X-27".
- Lockheed_CL-1200 label "Lockheed X-27".
- Lockheed_CL-1200 label "X-27 (航空機)".
- Lockheed_CL-1200 label "X-27试验机".
- Lockheed_CL-1200 label "لوكهيد سي إل-1200".
- Lockheed_CL-1200 sameAs Lockheed_X-27.
- Lockheed_CL-1200 sameAs Lockheed_CL-1200_Lancer.
- Lockheed_CL-1200 sameAs Lockheed_CL-1200.
- Lockheed_CL-1200 sameAs Lockheed_X-27.
- Lockheed_CL-1200 sameAs X-27_(航空機).
- Lockheed_CL-1200 sameAs Lockheed_CL-1200.
- Lockheed_CL-1200 sameAs m.05lvdm.
- Lockheed_CL-1200 sameAs Q1432376.
- Lockheed_CL-1200 sameAs Q1432376.
- Lockheed_CL-1200 wasDerivedFrom Lockheed_CL-1200?oldid=582079327.
- Lockheed_CL-1200 isPrimaryTopicOf Lockheed_CL-1200.