THK-2
The THK-2 was a single-seat, single-engine aerobatic trainer aircraft developed in Turkey in 1944 intended as an advanced trainer. It was a conventional, low-wing cantilever monoplane with an elliptical planform and of wooden construction. The cockpit was enclosed and the main units of the tailwheel undercarriage retracted backwards into the wing.
Wikipage disambiguates
Wikipage redirect
primaryTopic
THK-2
The THK-2 was a single-seat, single-engine aerobatic trainer aircraft developed in Turkey in 1944 intended as an advanced trainer. It was a conventional, low-wing cantilever monoplane with an elliptical planform and of wooden construction. The cockpit was enclosed and the main units of the tailwheel undercarriage retracted backwards into the wing.
has abstract
The THK-2 was a single-seat, s ...... nded role until the mid-1950s.
@en
manufacturer
number built
Link from a Wikipage to an external page
Wikipage page ID
19,963,512
page length (characters) of wiki page
Wikipage revision ID
993,337,519
Link from a Wikipage to another Wikipage
ceiling m
climb rate ftmin
cruise speed kmh
designer
Stanisław Rogalski, Jerzy Teisseyre and Leszek Dulęba
@en
empty weight kg
endurance
eng1 hp
eng1 name
eng1 number
first flight
gross weight kg
height m
length m
manufacturer
max speed kmh
national origin
Turkey
@en
never exceed speed kmh
number built
primary user
primeUnits%3F_
met
@en
range km
ref
Jane's All The World's Aircraft 1951–52
@en
stall speed kmh
type
Aerobatic trainer
@en
wikiPageUsesTemplate
wing area sqm
subject
hypernym
comment
The THK-2 was a single-seat, s ...... acted backwards into the wing.
@en
label
THK-2
@en