- Specifications (A.24)
- See also
{{Unreferenced|date=April 2010}} name = A.24 | image = Aero A.24.jpg | caption = | alt = }}{{Infobox aircraft type | type = Bomber | national origin = Czecho-Slovakia | manufacturer = Aero | design group = | designer = | builder = | first flight = | introduction = | introduced = | retired = | status = | primary user = | more users = | produced = | number built = 1 | program cost = | unit cost = | developed from = | variants with their own articles = | developed into = }} |
The Aero A.24 was a twin-engined biplane bomber aircraft of the 1920s. Flight tests showed it to be severely underpowered, making it useless as a combat aircraft. Only a single prototype was built. Aero proposed a variant designated the A.27 that was to have overcome the A.24's shortcomings by re-engining the design with Bristol Jupiters, but the Czech Air Force was not interested in pursuing this option, and all development ceased. Specifications (A.24){{Aircraft specs |ref= |prime units?=met |genhide= |crew=3/4 |capacity= |length m=13.7 |length ft= |length in= |length note= |span m=22.2 |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |lower span m= |lower span ft= |lower span in= |lower span note= |height m= |height ft= |height in= |height note= |wing area sqm=106 |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg=2960 |empty weight lb= |empty weight note= |gross weight kg=4511 |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general=
|eng1 number=2 |eng1 name=Maybach Mb.IV |eng1 type=6-cyl. water-cooled in-line piston engines |eng1 kw= |eng1 hp=240 |eng1 shp= |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note=
|perfhide= |max speed kmh=155 |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km=600 |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m=3600 |ceiling ft= |ceiling note= |g limits= |roll rate= |climb rate ms= |climb rate ftmin=267 |climb rate note= |time to altitude= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |more performance=
|guns= |bombs= up to {{convert|1000|kg|abbr=on}} of bombs |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |avionics= }}
See also{{commons category-inline}}{{aircontent |related= |similar aircraft= |lists= |see also= }}{{Aero Vodochody aircraft}} 3 : Aero Vodochody aircraft|Cancelled military aircraft projects|Czechoslovakian bomber aircraft 1920–1929 |