About: Schweizer X-26 Frigate

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About: Schweizer X-26 Frigate Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The X-26 Frigate is the longest-lived of the X-plane programs. The program included the X-26A Frigate sailplane and the motorized X-26B Quiet Thruster versions: QT-2, QT-2PC, and QT-2PCII. All were based on the Schweizer SGS 2-32 sailplane.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Schweizer X-26 Frigate
rdfs:comment	The X-26 Frigate is the longest-lived of the X-plane programs. The program included the X-26A Frigate sailplane and the motorized X-26B Quiet Thruster versions: QT-2, QT-2PC, and QT-2PCII. All were based on the Schweizer SGS 2-32 sailplane.
sameAs	dbr:Schweizer_X-26_Frigate
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max takeoff weight alt	kg
loaded weight main	1430.0 2500.0
climb rate main	ft/min 200.0
number of props	1(xsd:integer)
length alt	9.33 m 7.92 m
span main	57(xsd:integer)
power/mass alt	0(xsd:double) kW/kg
Status	#1: Unknown. #2 Operational as a glider at Mile High Glider
more performance	Rate of sink: 0.6 m/s Flight endurance: Planned = 4+ hours; demonstrated = 6.7+ hours *Quiet cruise speed: 70 - 80 mph
height alt	2.74 m
Introduced	1967(xsd:integer)
primary user	Tri-Service U.S. Navy Test Pilot School
Type	Experimental Covert Reconnaissance Aircraft Research and training aircraft
type of prop	horizontally opposed 4-cylinder air-cooled engine
loading main	39(xsd:integer) kg/m²
range alt	km
length main	815.34 937.26
power alt	75.0
area main	180.0 185.0
power main	100.0
height main	281.94
span alt	17.37 m
range main	miles
Manufacturer	dbkwik:resource/kximflT_x8Vcn9sj0IfIsQ== dbkwik:resource/xbPKAQd8hyiOtt5kSStvHw==
max speed main	158.0
engine (prop)	Continental O-200
power/mass main	0(xsd:double) hp/lb
climb rate alt	m/s
Quiet Cruise speed main	70(xsd:integer)
ceiling main	13000.0 ft
National Origin	United States
empty weight main	lb 857.0
fuel capacity	20(xsd:integer)
loaded weight alt	650.0 kg
Quiet Cruise alt	km/h
Developed From	dbkwik:resource/Oiu-pnKyjGSDD1pjOikaiA== SGS 2-32
area alt	16.7
First Flight	QT-2: July, 1967, QT-2PC: Dec, 1967
max speed alt	254.0
jet or prop?	prop
loading alt	7(xsd:double) lb/ft²
empty weight alt	kg 389.0
plane or copter?	plane
ceiling alt	m
max takeoff weight main	lb
variants with their own articles	QT-2, QT-2PC and X-26B QT-2, QT-2PC, X-26B
Retired	1969(xsd:integer)
Crew	two
Number Built	2(xsd:integer) 7(xsd:integer)
Designer	2(xsd:integer) dbkwik:resource/p7kKm6F42TfMQq3WBuq_jg== QT-2 and its variants: Stanley Hall
more general	Wing aspect ratio: 18 Propeller: Ole Fahlin four-blade, 8 inch chord, fixed-pitch 100 inch diameter Wing aspect ratio: 18 Fuel Capacity: 20 gallons
abstract	The X-26 Frigate is the longest-lived of the X-plane programs. The program included the X-26A Frigate sailplane and the motorized X-26B Quiet Thruster versions: QT-2, QT-2PC, and QT-2PCII. All were based on the Schweizer SGS 2-32 sailplane.

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