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The X-26 is a sailplane and is the longest-lived of the X-plane programs.
Development
The X-26A was used by the U.S. Navy (USN) to train test pilots in the condition of yaw/roll coupling. Since jet trainers were known to be dangerous in this condition, the X-26 was based on the Schweizer Aircraft CorporationSchweizer Aircraft CorporationSchweizer SGS 2-32|SGS 2-32 sailplane. Sailplanes react much slower and are easier to control than jet aircraft, making the X-26 a much safer training platform. Four aircraft were originally ordered. Three of the original planes crashed. The USN purchased a replacement for each of the crashed units.
Operational History
The X-26B were X-26As modified with a ContinentalContinental O-200 engine and Continental O-200 engine and propeller._These aircraft were designed to test stealth observation techniques for aircraft during the Vietnam War. Two of the X-26As were modified for the program. They were tested in Vietnam successfully. The LockheedYO-3 Quiet Star|YO-3A Quiet Star program continued the research begun by the X-26B. After the completion of their part of the program, the X-26Bs were de-modified and returned to the USN.
The USN continues to use the X-26A in the training program at the U.S. Naval Test Pilot School.
Specifications (X-26A Frigate)
{{airtemp|
|plane or copter?=plane
|jet or prop?=prop
|crew=two
|length main=26 ft 9 in
|length alt=7.92 m
|span main=57 ft 1.5 in
|span alt=17.37 m
|height main=9 ft 3 in
|height alt=2.74 m
|area main=180 ft²
|area alt=16.7 m²)
Aspect ratio: 18:1
|empty weight main=857 lb
|empty weight alt=389 kg
|loaded weight main=1430 lb
|loaded weight alt=650 kg
|max takeoff weight main= lb
|max takeoff weight alt= kg
|engine (prop)= Continental O-200
|type of prop= horizontally opposed 4-cylinder engine
|number of props= 1
|power main= 100 hp
|power alt= 75 kW
|max speed main=158 mph
|max speed alt=254 km/h)
Rate of sink: 0.6 m/s (120 ft/min)
|range main= miles
|range alt= km
|ceiling main= ft
|ceiling alt= m
|climb rate main= ft/min
|climb rate alt= m/s
|loading main=39 kg/m²
|loading alt=7.9 lb/ft²
|power/mass main= 0.07 hp/lb
|power/mass alt= 0.12 kW/kg
}}
References
[http://history.nasa.gov/monograph31.pdf American X-Vehicles] (.pdf)
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