Zeppelin-Staaken E-4/20
{{Infobox aircraft begin
| name=Zeppelin-Staaken E-4/20 | image=Staaken E.4 20.jpg | caption= }}{{Infobox aircraft type | type= Airliner | national origin= Germany | manufacturer=Zeppelin-Staaken (Zeppelin-Werke G.m.b.H., Staaken, Berlin) | designer=Adolf Rohrbach | introduced= | retired= | status= | primary user= | more users= | produced= | number built=1 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Zeppelin-Staaken E-4/20 was a revolutionary four-engine all-metal passenger monoplane designed in 1917 by Adolf Rohrbach and completed in 1919 at the Zeppelin-Staaken works outside Berlin, Germany. The E-4/20 was the first four-engine, all-metal stressed skin heavier-than-air airliner built.
Design and development
At a time when most aircraft were small, single-engine biplanes made of wood and canvas, the E-4 was a large (102-foot wingspan), all-metal, four-engine, stress-skinned, semi-monocoque, cantilevered-wing monoplane, with an enclosed cockpit, and accommodation for 18 passengers plus a crew of five, including two pilots, a radio operator, an engineer and a steward, as well as radio-telegraph communications, a toilet, a galley and separate baggage and mail storage. With a maximum speed of 143 mph, cruising speed of {{convert|131|mph|abbr=on|disp=flip}}, a range of about {{convert|750|mi|km|abbr=on|disp=flip}}, and a fully loaded weight of {{convert|18739|lb|abbr=on|disp=flip}}, it outperformed most other airliners of its day.
The E-4 included numerous innovations, including its all-metal monocoque construction, onboard facilities such as lavatory, kitchen and radio communications, and its notable and sturdy monoplane load-bearing box-girder wing constructed of dural metal which formed both the wing's main girder and the structure of the wing itself. Skinned with thin sheets of dural metal to give the aerofoil shape necessary for a wing, the girder section wing had fabric covered leading and trailing edges attached to it. This superb and innovative wing was robust and self-supporting.
The E-4 was completed in 1919 and test flown between 30 September 1920 and 1922 when it was broken up on the orders of the Inter-Allied Commission.
Background
The Zeppelin-Staaken E-4/20 was a product of the innovative Zeppelin Airship company. Count Ferdinand von Zeppelin, founder of the Luftschiffbau Zeppelin GmbH (Zeppelin Airship Construction Co.) was himself a major aeronautical innovator, creator of the groundbreaking giant aluminium alloy framed Zeppelin lighter than air dirigible airships and later developer of a series of R-Planes.
Zeppelin was one of the first aeronautical pioneers to apply stringent scientific principles to the design of aircraft, focusing on issues like power-to-weight ratios of engines and using the then new metal alloy aluminium for structural components. Zeppelin heard of the success in Russia of Igor Sikorsky's pioneering 4-engined Le Grand and Ilya Muromets aircraft. From the outbreak of war in 1914 the 4-engined Ilya Muromets class of aircraft were used as heavy bombers. The German government saw the potential for large strategic bombers and issued a design standard which was used by several manufacturers to produce Riesenflugzeuge ("Giant Aircraft") or R-Planes. The most successful design and manufacturing company of R-Planes was Zeppelin which was also the only company to manufacture them in series production, the R-VI.
Legacy
Adolf Rohrbach went on to found his own aircraft company, Rohrbach Metall-Flugzeugbau where he designed and built a number of innovative civil all-metal airliners, such as the Ro-VIII trimotor as well as some groundbreaking flying boats.
The Smithsonian Institution's "Airspace Magazine" suggested that Rohrbach could have been Germany's Boeing or Douglas but that the Inter-Allied Commission deemed the E-4/20 too much of a threat as a potential bomber to be allowed to go into serial production and ordered its destruction, even declining offers to sell it to allied countries.
The 1932 Armstrong Whitworth Atalanta used a very similar configuration, differing in construction details and more powerful engines.{{cite book|last1=Tapper|first1=Oliver|title=Armstrong Whitworth Aircraft since 1913|url=https://archive.org/details/armstrongwhitwor1913tapp_412|url-access=limited|date=1973|publisher=Putnam & Company Limited|location=London|isbn=9780370100043|pages=[https://archive.org/details/armstrongwhitwor1913tapp_412/page/n112 219]-235}}
Specifications
File:Zeppelin-Staaken_E-4_20_3-view_Le_Génie_Civil_August_20,1921.png
{{Aircraft specs
|ref={{cite book |last=Haddow |first=G.W. |author2=Peter M. Grosz |title=The German Giants - The German R-Planes 1914-1918 |publisher=Putnam |location=London |year=1988 |edition=3rd |isbn=0-85177-812-7|pages=289–293}}{{cite web|title=Zeppelin-Staaken E.4/20|url=http://www.all-aero.com/index.php/home2/12129-zeppelin-staaken-e420|website=all-aero|access-date=30 January 2017}}{{cite journal|title=THE ZEPPELIN-STAAKEN ALL-METAL MONOPLANE: And a New Smaller Edition|journal=Flight|date=17 March 1921|pages=185–186|url=http://www.flightglobal.com/pdfarchive/view/1921/1921%20-%200185.html|access-date=30 January 2017}}
|prime units?=met
|genhide=
|crew=3-5
|capacity=12-18 pax
|length m=16.6
|span m=31
|height m=4.5
|height note=approx.
|wing area sqm=106
|aspect ratio=
|airfoil=
|empty weight kg=6072
|gross weight kg=8500
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=4
|eng1 name=Maybach Mb.IVa
|eng1 type=6-cyl water-cooled in-line piston engines
|eng1 hp=245
|prop blade number=2
|prop name=fixed pitch wooden propellers
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|max speed kmh=225
|cruise speed kmh=200
|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=1200
|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=5-6 hours
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|wing loading kg/m2=80
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=0.09 kW/kg (0.055 hp/lb)
|more performance=
}}
References
{{Reflist}}
External links
{{commons category|Zeppelin-Staaken E-4/20}}
- [http://www.airwar.ru/enc/cw1/zse420.html]
- [http://www.airspacemag.com/multimedia/photos/?c=y&articleID=18766954&page=6 Smithsonian photo]
- Popular Mechanics, January 1921 [https://books.google.com/books?id=5z8EAAAAMBAJ&pg=RA1-PA36 photos]
{{Zeppelin aircraft}}
{{Idflieg R-class designations}}
{{DEFAULTSORT:Zeppelin-Staaken E-4 20}}
Category:1910s German airliners
Category:Four-engined tractor aircraft