- Development
- Specifications
- References Notes Bibliography
{{Orphan|date=June 2015}} name=Dietrich DP.III | image= | caption= }}{{Infobox Aircraft Type | type=Light passenger transport monoplane | national origin=Germany | manufacturer=Dietrich-Gobiet Flugzeugwerke | designer=Richard Dietrich | first flight=1920s | introduced= | retired= | status=Not flown | primary user= | number built= | developed from= | variants with their own articles= }} |
The Dietrich DP.III was a design for a 1920s German light passenger transport monoplane for six passengers designed by Richard Dietrich and was to be built by the Dietrich-Gobiet Flugzeugwerke as Kassel. Due to the financial problems of the company it is believed that the DP.III was not completed. DevelopmentThe DP.III was a high-wing cantilever monoplane with a conventional tail unit and a fixed tailskid landing gear. It was to be powered by an inline piston engine in the 172 to 194 kW (230-260 hp) range possibly a Benz Bz IV or Rolls-Royce Falcon. It had a crew of two in a semi-open cockpit and accommodation for six passengers in an enclosed cabin. Specifications{{Aircraft specs |ref= |prime units?=met |genhide= |crew=2 |capacity=6 passengers |length m=12.50 |length ft= |length in= |length note= |span m=17.00 |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m=3.60 |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg=1300 |empty weight lb= |empty weight note=estimated |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg=2200 |max takeoff weight lb= |max takeoff weight note=estimated |lift kg= |lift lb= |lift note= |more general=
|eng1 number=1 |eng1 name=Rolls-Royce Falcon |eng1 type=inline piston engine |eng1 kw= |eng1 hp=230 |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 note=
|perfhide= |max speed kmh=150 |max speed mph= |max speed kts= |max speed note=estimated |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= |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=950 |range miles= |range nmi= |range note=estimated |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=3000 |ceiling ft= |ceiling note=estimated |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2 |disk loading lb/sqft= |disk loading note= |power/mass met= |power/mass imp= |power/mass note= |thrust/weight= |thrust/weight note= |more performance= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
ReferencesNotes }}Bibliography{{refbegin}}- {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
{{refend}} 1 : German airliners 1920–1929 |