About: SITAR GY-110 Sher Khan   Sponge Permalink

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

The SITAR GY-110 Sher Khan was a light aircraft designed in France in the late 1960s as a larger and more powerful version of designer Yves Gardan's Bagheera. Like the Bagheera, it was to be conventional low-wing, cantilever monoplane with a fully enclosed cabin. However, although the Bagheera had seating for up to four people in 2+2 configuration, the Sher Khan was to have a stretched fuselage with full seating for four people. The wings were also to be enlarged in span, and unlike the Bagheera, whose tricycle undercarriage was fixed, the Sher Khan's was to be retractable.

AttributesValues
rdf:type
rdfs:label
  • SITAR GY-110 Sher Khan
rdfs:comment
  • The SITAR GY-110 Sher Khan was a light aircraft designed in France in the late 1960s as a larger and more powerful version of designer Yves Gardan's Bagheera. Like the Bagheera, it was to be conventional low-wing, cantilever monoplane with a fully enclosed cabin. However, although the Bagheera had seating for up to four people in 2+2 configuration, the Sher Khan was to have a stretched fuselage with full seating for four people. The wings were also to be enlarged in span, and unlike the Bagheera, whose tricycle undercarriage was fixed, the Sher Khan's was to be retractable.
sameAs
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
met or eng?
  • met
eng1 type
  • piston engine
Type
  • civil utility aircraft
eng1 kW
  • 150(xsd:integer)
perfhide
  • Y
Manufacturer
Capacity
  • 3(xsd:integer)
National Origin
  • France
Crew
  • 1(xsd:integer)
eng1 hp
  • 200(xsd:integer)
Designer
ref
  • Taylor 1971, p.78
eng1 number
  • 1(xsd:integer)
abstract
  • The SITAR GY-110 Sher Khan was a light aircraft designed in France in the late 1960s as a larger and more powerful version of designer Yves Gardan's Bagheera. Like the Bagheera, it was to be conventional low-wing, cantilever monoplane with a fully enclosed cabin. However, although the Bagheera had seating for up to four people in 2+2 configuration, the Sher Khan was to have a stretched fuselage with full seating for four people. The wings were also to be enlarged in span, and unlike the Bagheera, whose tricycle undercarriage was fixed, the Sher Khan's was to be retractable. Power was to be supplied by engines in the 150-kW to 240-kW (200-hp to 300-hp) range.
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