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About: dbkwik:resource/GiY8PHplYcJJe3Y0nKGApA==

PropertyValue
rdf:type
rdfs:label
  • Yakovlev Yak-32
rdfs:comment
  • The Yakovlev Yak-32 (NATO reporting name Mantis) was a single-seat version of the Yakovlev Yak-30 (1960), and was claimed by the OKB to be the world's first sporting aircraft with an ejection seat. This version was designated as Yak-104PS. Neither the Yak-30 or the Yak-32 entered production.
owl:sameAs
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
loaded weight main
  • 1930.0
climb rate main
  • 18.0
length alt
  • 33
span main
  • 9.38 m
more performance
  • 34380.0
thrust alt
  • 2363
height alt
  • 11.1
primary user
Type
range alt
  • 600.0
length main
  • 10.14 m
useful load main
  • 991.0
area main
  • 14.3
height main
  • 3.4 m
span alt
  • 30
range main
  • 965.0
Manufacturer
max speed main
  • 755.0
thrust/weight
  • 0.360000
climb rate alt
  • 3540.0
ceiling main
  • 11,500 m
empty weight main
  • 1435.0
type of jet
  • turbofan
loaded weight alt
  • 4255.0
area alt
  • 153.7
First Flight
  • 1960
engine (jet)
  • Tumansky RU19-300
max speed alt
  • 469.0
jet or prop?
  • jet
empty weight alt
  • 3164.0
thrust main
  • 1070
number of jets
  • 1
plane or copter?
  • plane
ceiling alt
  • 37730.0
variants with their own articles
Crew
  • 1
Armament
  • Various
Number Built
  • 3
useful load alt
  • 2185.0
more general
  • * Basic fuel capacity: 500 kg * Maximum fuel capacity: 805 kg * Max wing loading: 154 kg/m² * Max power loading: 0.41 kg/kgp
abstract
  • The Yakovlev Yak-32 (NATO reporting name Mantis) was a single-seat version of the Yakovlev Yak-30 (1960), and was claimed by the OKB to be the world's first sporting aircraft with an ejection seat. This version was designated as Yak-104PS. Neither the Yak-30 or the Yak-32 entered production.
is variants with their own articles of