- Design and development
- Operational history
- Specifications
- See also
- References Notes Bibliography
name=900 Acrobat | image= | caption= }}{{Infobox Aircraft Type | type=Single-seat aerobatic monoplane | national origin=Russia | manufacturer=Aviatika | designer= | first flight=22 February 1993 | introduced= | retired= | status= | produced= | primary user= | number built=1 | developed from= | variants with their own articles= | developed into= }} |
The Aviatika-900 Acrobat is a 1990s Russian single-seat aerobatic monoplane designed and built by Aviatika Joint Stock Company. The aircraft is sometimes referred to as the MAI-900 Acrobat, the Moscow Aviation Institute being one of the constitute organisations when the company was formed in 1993. Design and developmentThe Acrobat is an all-metal monoplane with cantilever wings and a strut-braced tailplane. It has a fixed landing gear with a steerable tailwheel and is powered by a {{convert|360|hp|kW|0|abbr=on}} AOOT M-14P radial piston engine. Operational historyThe aircraft set five FAI-accredited records. The aircraft was sold to Lithuanian aerobatic pilot Jurgis Kairys. Specifications{{Aircraft specs |ref= |prime units?=met |genhide= |crew=1 |capacity= |length m=5.7 |length ft= |length in= |length note= |span m=7.15 |span ft= |span in= |span note= |height m=3.0 |height ft= |height in= |height note= |wing area sqm=10 |wing area sqft= |wing area note= |aspect ratio=5:11 |airfoil=Symmetrical |empty weight kg=590 |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg=715 |max takeoff weight lb= |max takeoff weight note= |more general=
|eng1 number=1 |eng1 name=AOOT M-14P |eng1 type=radial piston engine |eng1 kw= |eng1 hp=360 |eng1 kn= |eng1 lbf= |eng1 note= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop note=
|perfhide= |max speed kmh=375 |max speed mph= |max speed kts= |max speed note= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh=107 |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits=±11 |roll rate= |climb rate ms= |climb rate ftmin=4530 |climb rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= }}
See also{{aircontent |see also= |related= |similar aircraft=- Sukhoi Su-29
- Yakovlev Yak-54
|lists= }}ReferencesNotesBibliography{{refbegin}}- {{cite book |last=Taylor |first= Michael J. H.|authorlink= |coauthors= |title= Brassey's World Aircraft & Systems Directory|year=1996 |publisher= Brassey's|location= London, England |isbn=978-1-85753-198-5|pages=}}
{{refend}}{{aerobatics}}{{Aero-1990s-stub}} 4 : Soviet and Russian sport aircraft 1990–1999|Single-engined tractor aircraft|Aerobatic aircraft|Aircraft first flown in 1993 |