- Development
- Variants
- Specifications (DP.IIa)
- References Notes Bibliography
| name=Dietrich DP.II Bussard | image=Bundesarchiv Bild 102-00568, Fritz Heidt.jpg | caption= }}{{Infobox Aircraft Type | type=two-seat training biplane | national origin=Germany | manufacturer=Dietrich-Gobiet Flugzeugwerke | designer=Richard Dietrich | first flight=1920s | introduced= | retired= | status= | primary user= | number built=54 | developed from= | variants with their own articles=
}} |
The Dietrich DP.II Bussard was a 1920s German two-seat training biplane designed by Richard Dietrich and built by the Dietrich-Gobiet Flugzeugwerke as Kassel. DevelopmentThe DP.II was a development of the earlier DP.I with the change to be a cantilever unequal-span biplane. Variants- DP.II
Prototype with a Siemens-Halske Sh 4 radial engine, one built. - DP.IIa
Production variant with a Siemens-Halske Sh 5 radial engine, 53 built. Specifications (DP.IIa){{Aircraft specs
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|prime units?=met
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|crew=2
|capacity=
|length m=5.97
|length ft=
|length in=
|length note=
|span m=7.60
|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=2.43
|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=340
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=560
|max takeoff weight lb=
|max takeoff weight note=
|lift kg=
|lift lb=
|lift note=
|more general=
|eng1 number=1
|eng1 name=Siemens-Halske Sh 5
|eng1 type=seven-cylinder, air-cooled, radial engine
|eng1 kw=
|eng1 hp=55
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
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|eng1 lbf-ab=
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|max speed kmh=145
|max speed mph=
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|max speed mach=
|cruise speed kmh=
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|cruise speed note=
|stall speed kmh=
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|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
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|range km=500
|range miles=
|range nmi=
|range note=
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|ferry range km=
|ferry range miles=
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|endurance=
|ceiling m=3800
|ceiling ft=
|ceiling note=
|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=
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References{{commons category|Dietrich DP.II}}Notes
}}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}} 3 : German civil utility aircraft 1920–1929|Aerobatic aircraft|Biplanes |