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Fokker V.6 (Fokker D.VII)

Triplane Fighter Prototype

Fokker V.6 (Fokker D.VII)

Triplane Fighter Prototype

OVERVIEW
SPECIFICATIONS
ARMAMENT
VARIANTS
HISTORY
MEDIA
OVERVIEW



The Fokker V.6 triplane fighter was an enlarged form of the V.5 prototype developed in parallel and carried a different engine - it was not furthered.
National Flag Graphic
ORIGIN: Imperial Germany
YEAR: 1917
MANUFACTURER(S): Fokker-Flugzeugwerke - Imperial Germany
PRODUCTION: 1
OPERATORS: Imperial Germany (cancelled)
SPECIFICATIONS



Unless otherwise noted the presented statistics below pertain to the Fokker V.6 model. Common measurements, and their respective conversions, are shown when possible.
CREW: 1
LENGTH: 19.72 feet (6.01 meters)
WIDTH: 26.48 feet (8.07 meters)
HEIGHT: 9.88 feet (3.01 meters)
WEIGHT (EMPTY): 959 pounds (435 kilograms)
WEIGHT (MTOW): 1,323 pounds (600 kilograms)
ENGINE: 1 x Mercedes D.II six-cylinder water-cooled engine developing 120 horsepower.
SPEED (MAX): 96 miles-per-hour (155 kilometers-per-hour; 84 knots)
RANGE: 180 miles (290 kilometers; 157 nautical miles)
CEILING: 18,701 feet (5,700 meters; 3.54 miles)
RATE-OF-CLIMB: 900 feet-per-minute (274 meters-per-minute)




ARMAMENT



PROPOSED:
2 x 7.92mm LMG 08/15 machine guns over the nose set to fire through the spinning propeller blades.
VARIANTS



Series Model Variants
• V.6 - Prototype Model Designation; single example completed.


HISTORY



Detailing the development and operational history of the Fokker V.6 (Fokker D.VII) Triplane Fighter Prototype.  Entry last updated on 10/28/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The Fokker V.6 continued the line of triplane prototype fighter begun by Fokker with the V.4 intended for the Austrian-Hungarian air service as a biplane. The line was influenced heavily by the arrival of the Sopwith Triplane unveiled by the Allies in late 1916 and seeing its first actions in early 1917. Its maneuverability, rate-of-climb, and high operating ceiling made it an instant success against the slower, less-maneuverable and heavier-armed Fokker biplanes then in service. This pressed Fokker to develop a competing type which eventually became the classic "Red Baron" Fokker Dr.I Triplane detailed elsewhere on this site.

Like the other V-series triplanes, the Fokker V.6 served as nothing more than a prototype for its service life. Developed in parallel to the earlier V.5 triplane, the V.6 was ordered on July 7th, 1917 and recorded a first flight in 1917 and carried the same basic triple-plane wing arrangement as earlier models - though the fuselage now mated to the more powerful (and heavier) Mercedes D.II six-cylinder water-cooled engine of 120 horsepower. The pilot sat in an open-air cockpit, the engine drove a two-bladed wooden propeller, and the tail unit relied on a single vertical fin with low-mounted horizontal planes. The undercarriage, as expected, was fixed to the fuselage by a series of struts and sported two wheels for ground-running.

Because of the heavier engine in play, the V.6 was a dimensionally larger aircraft design when compared to the V.5 - it saw its wing surfaces enlarged and surface areas increased while the mainplane chord was increased. The longer-wing interplanes were now joined by single solid struts angled forward to meet the staggered arrangement of the triple wings. The changes also caused the cockpit to be pushed further aft (reducing forward visibility all the more) and the fuselage to be deepened.

After a period of testing, it was found that the modified, heavier V.6 prototype added little to the overall initiative as maneuverability proved lacking against the competing V.5 prototype with its rotary engine. As such, the V.5 prototype leaped ahead of the V.6 as the basis for the Dr.I triplane fighter to come.

The V.6 was given up for good in October of 1917. The V.7 appeared for a short time and differed in having a Siemens-Halske Sh.III series engine fitted.

Performance specifications on this page are pure estimates on the part of the author.




MEDIA









Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.

Image of collection of graph types

Relative Maximum Speed Rating
Hi: 100mph
Lo: 50mph
    This entry's maximum listed speed (96mph).

    Graph average of 75 miles-per-hour.
City-to-City Ranges
NYC
 
  LDN
LDN
 
  PAR
PAR
 
  BER
BER
 
  MSK
MSK
 
  TKY
TKY
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Graph showcases the Fokker V.6's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
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Pie graph section
Pie graph section
Pie graph section
Pie graph section
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
1
1

  * Commercial Market High belongs to Cessna 172.

  ** Military Market High belongs to Ilyushin Il-2.


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Supported Roles
A2A
Interception
UAV
Ground Attack
CAS
Training
ASW
Anti-Ship
AEW
MEDEVAC
EW
Maritime/Navy
SAR
Aerial Tanker
Utility/Transport
VIP
Passenger
Business
Recon
SPECOPS
X-Plane/Development
A2A=Air-to-Air; UAV=Unmanned; CAS=Close Support; ASW=Anti-Submarine; AEW=Airborne Early Warning; MEDEVAC=Medical Evac; EW=Electronic Warfare; SAR=Search-Rescue
Supported Arsenal
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