About: EM-10 Bielik   Sponge Permalink

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

The EM-10 Bielik () is low cost Polish military training aircraft prototype, built by Margański & Mysłowski and first flown on 4 June 2003. The single engine aircraft had a composite (mostly carbon fibre) fuselage with a light alloy aft section. The pressurized cockpit had ejection seats.

AttributesValues
rdf:type
rdfs:label
  • EM-10 Bielik
rdfs:comment
  • The EM-10 Bielik () is low cost Polish military training aircraft prototype, built by Margański & Mysłowski and first flown on 4 June 2003. The single engine aircraft had a composite (mostly carbon fibre) fuselage with a light alloy aft section. The pressurized cockpit had ejection seats.
empty weight kg
  • 1700(xsd:integer)
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
range km
  • 2500(xsd:integer)
stall speed kmh
  • 155(xsd:integer)
Status
  • prototype
eng1 type
Type
  • Training aircraft
height m
  • 2(xsd:double)
span m
  • 6(xsd:double)
climb rate ms
  • 75(xsd:integer)
Manufacturer
  • Margański & Mysłowski
max speed kmh
  • 1000(xsd:integer)
eng1 kn
  • 13(xsd:double)
length m
  • 9(xsd:integer)
National Origin
  • Poland
First Flight
  • 2003-06-04(xsd:date)
max takeoff weight kg
  • 2500(xsd:integer)
wing area sqm
  • 11(xsd:double)
prime units?
  • met
Crew
  • 2(xsd:integer)
Number Built
  • 1(xsd:integer)
eng1 name
  • Single-shaft turbojet
Designer
  • Edward Margański
eng1 number
  • 1(xsd:integer)
abstract
  • The EM-10 Bielik () is low cost Polish military training aircraft prototype, built by Margański & Mysłowski and first flown on 4 June 2003. The single engine aircraft had a composite (mostly carbon fibre) fuselage with a light alloy aft section. The pressurized cockpit had ejection seats.
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