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- Windecker_YE-5 abstract "The Windecker YE-5A was an experimental aircraft evaluated by the U.S. Air Force. It was an all-composite construction aircraft, based on the commercial single-engine, low-wing Windecker Eagle. The YE-5A, delivered in 1973, was used in tests relating to the radar detectability (commonly known as 'stealth') of composite aircraft. A single YE-5A (serial number 73-1653) was built. The YE-5A composite airframe benefited from the U.S. Army project and was shown to be difficult to detect using radar; however other components, including the metal engine, could be seen on radar. The YE-5A was destroyed in a crash during a classified project in 1985, and was replaced by a modified conventional civilian model Windecker Eagle (N4196G), to complete the project. This aircraft is disassembled and in storage in the United States Army Aviation Museum at Fort Rucker, Alabama.".
- Windecker_YE-5 manufacturer Windecker_Industries.
- Windecker_YE-5 numberBuilt "1".
- Windecker_YE-5 predecessor Windecker_Eagle.
- Windecker_YE-5 type Stealth_technology.
- Windecker_YE-5 wikiPageID "3246231".
- Windecker_YE-5 wikiPageRevisionID "559532024".
- Windecker_YE-5 areaAlt "m²".
- Windecker_YE-5 areaMain "ft²".
- Windecker_YE-5 ceilingAlt "5,500 m".
- Windecker_YE-5 ceilingMain "8000.0".
- Windecker_YE-5 climbRateAlt "6.0".
- Windecker_YE-5 climbRateMain "1220.0".
- Windecker_YE-5 crew "one pilot".
- Windecker_YE-5 cruiseSpeedAlt "328.0".
- Windecker_YE-5 cruiseSpeedMain "204".
- Windecker_YE-5 developedFrom Windecker_Eagle.
- Windecker_YE-5 emptyWeightAlt "975.0".
- Windecker_YE-5 emptyWeightMain "2150.0".
- Windecker_YE-5 engine(prop)_ Lycoming_O-540.
- Windecker_YE-5 firstFlight "1973".
- Windecker_YE-5 hasPhotoCollection Windecker_YE-5.
- Windecker_YE-5 heightAlt "2.9 m".
- Windecker_YE-5 heightMain "289.56".
- Windecker_YE-5 jetOrProp%3F_ "prop".
- Windecker_YE-5 lengthAlt "8.7 m".
- Windecker_YE-5 lengthMain "873.7600000000001".
- Windecker_YE-5 loadedWeightAlt "1500.0".
- Windecker_YE-5 loadedWeightMain "3400.0".
- Windecker_YE-5 loadingAlt "kg/m²".
- Windecker_YE-5 loadingMain "19.3".
- Windecker_YE-5 manufacturer Windecker_Industries.
- Windecker_YE-5 maxSpeedAlt "338.0".
- Windecker_YE-5 maxSpeedMain "210".
- Windecker_YE-5 maxTakeoffWeightAlt "kg".
- Windecker_YE-5 maxTakeoffWeightMain "lb".
- Windecker_YE-5 numberBuilt "1".
- Windecker_YE-5 numberOfProps "1".
- Windecker_YE-5 planeOrCopter%3F_ "plane".
- Windecker_YE-5 massAlt "0.14".
- Windecker_YE-5 massMain "0.09".
- Windecker_YE-5 powerAlt "216.0".
- Windecker_YE-5 powerMain "290.0".
- Windecker_YE-5 primaryUser United_States_Air_Force.
- Windecker_YE-5 rangeAlt "1770.0".
- Windecker_YE-5 rangeMain "1100.0".
- Windecker_YE-5 retired "1985".
- Windecker_YE-5 spanAlt "9.8 m".
- Windecker_YE-5 spanMain "32.0".
- Windecker_YE-5 stallSpeedAlt "106.0".
- Windecker_YE-5 stallSpeedMain "66".
- Windecker_YE-5 type "Experimental stealth aircraft".
- Windecker_YE-5 subject Category:Stealth_aircraft.
- Windecker_YE-5 subject Category:United_States_experimental_aircraft_1970–1979.
- Windecker_YE-5 subject Category:Windecker_aircraft.
- Windecker_YE-5 type Aircraft.
- Windecker_YE-5 type MeanOfTransportation.
- Windecker_YE-5 type Product.
- Windecker_YE-5 type DesignedArtifact.
- Windecker_YE-5 comment "The Windecker YE-5A was an experimental aircraft evaluated by the U.S. Air Force. It was an all-composite construction aircraft, based on the commercial single-engine, low-wing Windecker Eagle. The YE-5A, delivered in 1973, was used in tests relating to the radar detectability (commonly known as 'stealth') of composite aircraft. A single YE-5A (serial number 73-1653) was built. The YE-5A composite airframe benefited from the U.S.".
- Windecker_YE-5 label "Windecker YE-5".
- Windecker_YE-5 label "YE-5 (航空機)".
- Windecker_YE-5 sameAs YE-5_(航空機).
- Windecker_YE-5 sameAs m.09102x.
- Windecker_YE-5 sameAs Q8024093.
- Windecker_YE-5 sameAs Q8024093.
- Windecker_YE-5 wasDerivedFrom Windecker_YE-5?oldid=559532024.
- Windecker_YE-5 isPrimaryTopicOf Windecker_YE-5.