Zeppelin-Staaken VGO.I

{{Short description|German heavy bomber aircraft of World War I }}

{{Use dmy dates |date=August 2024 }}

{{Use British English|date=August 2024 }}

{{Infobox aircraft begin

|name=VGO.I

|image=Zeppelin-Staaken VGO-I.jpg

|caption=

}}{{Infobox aircraft type

|type=Heavy bomber

|national origin=Germany

|manufacturer=Zeppelin-Staaken

|designer=

|first flight=11 April 1915

|introduced=

|retired=

|status=

|primary user=Imperial German Navy

|number built=1

|developed from=

|variants with their own articles=

|developed into=Zeppelin-Staaken VGO.II
Zeppelin-Staaken VGO.III
Zeppelin-Staaken R.IV

}}

The Zeppelin-Staaken VGO.I, redesignated Zeppelin-Staaken RML.1 in naval service, was a heavy bomber built in Germany in 1915 and which saw limited service during World War I.Gray & Thetford 1992, p.582 Although only one example was built, it served as a prototype for further {{lang |de |Riesenflugzeuge}} ("giant aircraft") by Zeppelin-Staaken. Its "VGO" designation was assigned because the aircraft was constructed by Versuchsbau Gotha-Ost, a division of Gothaer Waggonfabrik. At the time of its construction, it was the largest plane in the world.Szigeti 2007, p.12

Design

The VGO.I was a four-bay, equal-span biplane with slightly negative wing stagger.Haddow & Grosz 1988, p.213 Of mostly conventional configuration it diverged most noticeably from the designs of the day not only by its size, but by its biplane horizontal stabilisers, its two fins, and its tricycle undercarriage.Herris 2020, p.15 Its two pilots sat in an open cockpit,Haddow & Grosz 1988, p.212 and the crew also included a mechanic for each of its three engines, and two machine-gunners. One engine was mounted in the nose, driving a tractor propeller, and the other two were mounted in nacelles in the interplane gap and drove pusher propellers. These nacelles were large enough to accommodate a mechanic, who could make his way into them in flight (a requirement of the {{lang |de |Riesenflugzeuge}} specification). The fuselage included a bomb bay large enough to carry a {{convert |1000 |kg |lb |adj=on }} bomb. As defensive armament, the VGO.I carried two machine guns in the fuselage, one firing upward and the other downward. Later, machine guns would also be fitted to the fronts of the engine nacelles.Haddow & Grosz 1988, p.214

The design proved very underpowered, and two more engines were eventually added, one to each nacelle.Haddow & Grosz 1988, p.217 The two engines in each nacelle were geared together to drive a common propeller.Haddow & Grosz 1988, p.218

The structure was a mixture of wood and welded steel tube, covered in canvas. Late in its service life, some of the canvas covering was replaced by cellon to help reduce the aircraft's visibility.

Development

Around the outbreak of World War I, Count Ferdinand von Zeppelin became interested in the potential of a very large aeroplane to overcome the operational limitations of the airships for which he and his company were famous.Haddow & Grosz 1988, p.209Herris 2020, p.12 He was aware of a pre-war project by Hellmuth Hirth and Gustav Klein to build a giant biplane with transatlantic range, and recruited them to work on building an aircraft that could carry a {{convert |1000 |kg |lb |adj=on }} bomb over a range of {{convert |600 |km |mi }}. With Robert Bosch, Zeppelin financed the Versuchsbau Gotha-Ost venture,Haddow & Grosz 1988, p.210–11 and appointed Professor Alexander Baumann to lead the project.Haddow & Grosz 1988, p.210–11 From the outset, this was a private venture,Haddow & Grosz 1988, p.211 but Zeppelin soon secured the interest and support of both the Army and the Navy. At the same time the War Office opposed the project.

Design work began in September 1914 and was complete by December. Construction was delayed in January 1915 because the Maybach HS engines were not yet ready. The aircraft first flew on 11 April 1915 and on 6 June was flown to the Maybach factory in Friedrichshafen for testing by the Imperial German Navy. The HS engine was a new design, and its unreliability proved a constant problem, culminating in a forced landing at Geroldsgrün on 15 December after two of the three engines failed in flight due to failures in their oil supply lines. The heavily damaged aircraft was salvaged and taken back to Gotha.

The VGO.I was rebuilt with many modifications. These included redesigned engine nacelles that incorporated a gunner's position in their fronts, and a redesigned and enlarged tail to improve directional control.Haddow & Grosz 1988, p.215 Both were changes that had already been incorporated into the VGO.II design.Haddow & Grosz 1988, p.214–15 Improved cooling for the still-troublesome HS engines was also provided. In this new form, it flew again on 16 February 1916 and was accepted for naval service by June.

Operational history

The VGO.1 received the designation RML.1, for {{lang |de |Reichs Marine Landflugzeuge}} (Imperial Navy landplane) and a unit, Kommando RLM.1, was established to test it in combat on the Eastern front. The RML.1 was deployed to Auce in June 1916, but due to a series of engine and undercarriage failures that aviation historian Jack Herris called "a tragicomedy of errors", did not reach there until the end of July. In mid August, the RML.1 flew a series of raids.Haddow & Grosz 1988, p.216 On 15 August, it attacked the railway terminal at Sloka. The next day, it attacked the Russian air station at Läbara, and the day after that, the air station at Ruhnu Island and a troop encampment at Kemeri. A second raid on Kemeri was to take place on 24 August but was aborted due to an overheating engine.

On 1 September, two engines failed in quick succession while the RML.1 was outbound on a night raid. The pilots guided it to a forced landing in a pine forest. The fuselage was salvaged and sent back to Staaken, but Kommando RML.1 was disestablished, and its personnel reassigned. The aircraft itself was rebuilt again, with new wings and engines. This time, five Maybach Mb.IVa engines were installed, each with a similar power output to the original HS engines. One engine was installed in the nose, as before, but the other four were installed two to each nacelle, geared together to drive a common propeller.Haddow & Grosz 1988, p.217–18 During this rebuild, some of the fuselage covering was replaced with cellon, as part of a {{lang |de |Unsichtbare Flugzeug}} (invisible aircraft) test, intended to reduce the visibility of large aircraft. A completely new tail was built, mounted higher on the fuselage, and this was also covered in cellon.

The newly rebuilt VGO.I flew on 10 March 1917, but suffered an engine failure in the port nacelle after an explosion. As its pilots brought it back to the airfield, they needed to use hard rudder to balance the asymmetrical thrust. Unfortunately, a problem with the rudder pedals jamming at high deflections that had been noted in ground tests had not yet been corrected. As a result, once on the ground and with its rudders jammed, the VGO.I could not be steered, and collided with the side of a hangar. One pilot was killed instantly, and the other died a few hours later. The VGO.I was not rebuilt again.

Operators

;Imperial German Navy

:Kommando RML.1

Specifications (after first rebuild)

{{Aircraft specs

|ref=Kroschel & Stützer 1994, p.133, and as noted

|prime units?=met

|genhide=

|crew=Six

|capacity=

|length m=24

|length ft=

|length in=

|length note=

|span m=42.2

|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=6.6

|height ft=

|height in=

|height note=

|wing area sqm=332

|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=6520

|empty weight lb=

|empty weight note=

|gross weight kg=9520

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=

|lift kg=

|lift lb=

|lift note=

|more general=

|eng1 number=3

|eng1 name=Maybach HS

|eng1 type=six-cylinder, water-cooled, inline piston engine

|eng1 kw=177

|eng1 hp=

|eng1 shp=

|eng1 kn=

|eng1 lbf=

|eng1 note=(240 PS each)

|power original=

|thrust original=

|eng1 kn-ab=

|eng1 lbf-ab=

|eng2 number=

|eng2 name=

|eng2 type=

|eng2 kw=

|eng2 hp=

|eng2 shp=

|eng2 kn=

|eng2 lbf=

|eng2 note=

|eng2 kn-ab=

|eng2 lbf-ab=

|eng3 number=

|eng3 name=

|eng3 type=

|eng3 kw=

|eng3 hp=

|eng3 shp=

|eng3 kn=

|eng3 lbf=

|eng3 note=

|eng3 kn-ab=

|eng3 lbf-ab=

|more power=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|rot number=

|rot dia m=

|rot dia ft=

|rot dia in=

|rot area sqm=

|rot area sqft=

|rot area note=

|perfhide=

|max speed kmh=110

|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=

|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=

|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=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude={{convert |2000 |m |ft}} in 39 minutes
{{convert |3000 |m |ft}} in 79 minutes

|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=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|thrust/weight=

|more performance=

|guns= 4 × {{convert |7.92 |mm |in |adj=on }} Parabellum MG 14Cooksley 2000, p.42 machine guns

|bombs= {{convert |1000 |kg |lb}} bombs

|rockets=

|missiles=

|hardpoints=

|hardpoint capacity=

|hardpoint rockets=

|hardpoint missiles=

|hardpoint bombs=

|hardpoint other=

|avionics=

}}

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

Notes

=References=

{{reflist}}

=Bibliography=

  • {{cite book |last=Cooksley |first=Peter |title=German Bombers of WWI in Action |year=2000 |publisher=Squadron/Signal |location=Carrollton, Texas }}
  • {{cite book |last1=Gray |first1=Peter |last2=Thetford |first2=Owen |title=German Aircraft of the First World War |year=1992 |publisher=Putnam |location=London }}
  • {{cite book |last1=Haddow |first1=George William |last2=Grosz |first2=Peter M. |title=The German giants: the story of the R-Planes 1914–1919 |year=1988 |publisher=Putnam |location=London }}
  • {{cite book |last=Herris |first=Jack |title=Zeppelin-Staaken Aircraft of WWI: Volume 1: VGO.1 – R.VI R.29/16 |year=2020 |publisher=Aeronaut |location=Reno, Nevada }}
  • {{cite book |last1=Kroschel |first1=Günter |last2=Stützer |first2=Helmut |title=Die deutschen Militärflugzeuge 1910–1918 |language=de |trans-title=German military aircraft 1910–1918 |year=1994 |publisher=E. S. Mittler & Sohn |location=Augsburg }}
  • {{cite magazine |last=Szigeti |first=Martin |title=Geburtsstunde der Giganten |language=de |trans-title=Birth of the Giants |magazine=Klassiker der Luftfahrt |number=4/07 |year=2007 |publisher=Motor Presse Stuttgart |location=Stuttgart |pages=10–17 }}

{{Zeppelin aircraft}}

Category:1910s German bomber aircraft

Category:Zeppelin-Staaken

Category:Biplanes

Category:Twin-tail aircraft

Category:Three-engined push-pull aircraft

Category:Five-engined push-pull aircraft

Category:Aircraft with fixed tricycle landing gear

Category:Aircraft first flown in 1915