With the end of World War 1 (1914-1918) still not a foregone conclusion in early 1918, the French Air Force continued to entertain all-new fighter designs. The B.A.J. ("Boncourt-Audenis-Jacob" of Bron, France) "Type IV" was one of the late-war entries that appeared during this time and comprised a single-engine, tandem twin-seat fighter with biplane wing configuration. However, its arrival towards the end of the war and delays during its development meant that only two prototypes were ever completed. Design of this biplane was attributed to Charles Audenis.
As with other aircraft of this period, the two seat arrangement of the Type IV had the pilot in the forward cockpit with the observer/gunner in the rear (seated back-to-back in close proximity to one another). Armament was a single, fixed, forward-firing 7.7mm Vickers Machine Gun synchronized to fire through the spinning propeller blade by the pilot and twin 7.7mm Lewis Machine Guns on a trainable mounting (T.O.3 series ring) for the rear gunner.
The fuselage was left relatively clean by the standards of the day and even the engine was shrouded over for aerodynamic efficiency. Power was pulled from a single Hispano-Suiza 8Fb 8-cylinder, water-cooled inline piston engine of 300 horsepower, this used to drive a two-bladed, fixed-pitch wooden propeller at the nose.
The biplane configuration utilized a traditional "over-under" wing arrangement of equal span and twin-bay. The interplane support struts were single pieces and cabling was used where necessary. The mainplanes were seated well-forward of midships. The tail unit was given small-area planes itself, a single vertical fin and low-set horizontal planes. The undercarriage was also traditional for the time, made up of a fixed twin-wheeled main unit under center mass and a tailskid at rear.
French authorities though enough of the Type IV design that it contracted for the aircraft on May 1st, 1918. However, the initial prototype was not delivered to Villacoublay for formal evaluations until November of that year due to requested revisions (to be handled by Hanriot) and the official Armistice to end hostilities was signed that November 18th. After a fire broke out at the Bron facility, work on the airplane was not completed until January of 1919. Trials then followed which led to additional repairs seen during the middle part of the year. By this time, a second prototype was being flown for evaluation but the project was more or less a lost cause - the war was over and any additional development of the Type IV was ended with just the two prototypes to show for the effort.
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(OPERATORS list includes past, present, and future operators when applicable)
✓Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
✓Intelligence-Surveillance-Reconnaissance (ISR), Scout
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
✓X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
Length
65.6 ft (20.00 m)
Width/Span
85.3 ft (26.00 m)
Height
26.2 ft (8.00 m)
Empty Wgt
992 lb (450 kg)
MTOW
1,323 lb (600 kg)
Wgt Diff
+331 lb (+150 kg)
(Showcased structural values pertain to the BAJ Type IVC.2 production variant)
Installed:
1 x Hispano-Suiza 8Fb 8-cylinder water-cooled inline piston engine developing 300 horsepower and driving a two-bladed, fixed-pitch wooden propeller at the nose.
(Showcased performance specifications pertain to the BAJ Type IVC.2 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
PROPOSED:
1 x 7.7mm Vickers Machine Gun in fixed, forward-firing mounting.
2 x 7.7mm Lewis Machine Guns in rear, trainable gunner's position.
Supported Types
(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 0
Type IV - Base Series Designation.
Type IVC.2 - Prototype designation; two completed.
General Assessment
Firepower
Performance
Survivability
Versatility
Impact
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
Overall Rating
The overall rating takes into account over 60 individual factors related to this aircraft entry.
46
Rating is out of a possible 100 points.
Relative Maximum Speed
Hi: 150mph
Lo: 75mph
This entry's maximum listed speed (121mph).
Graph average of 113 miles-per-hour.
City-to-City Ranges
NYC
LON
LON
PAR
PAR
BER
BER
MOS
MOS
TOK
TOK
SYD
SYD
LAX
LAX
NYC
BAJ Type IVC.2 operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
Design Balance
The three qualities reflected above are altitude, speed, and range.
Aviation Era Span
Showcasing era cross-over of this aircraft design.
Unit Production (2)
2
36183
44000
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
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Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.
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France (cancelled)
