STATUS: Retired, Out-of-Service
MANUFACTURER(S): Heinkel - Germany
LENGTH: 54.79 feet (16.7 meters)
WIDTH: 115.49 feet (35.2 meters)
HEIGHT: 13.12 feet (4 meters)
WEIGHT (EMPTY): 47,399 pounds (21,500 kilograms)
WEIGHT (MTOW): 62,556 pounds (28,375 kilograms)
ENGINE: 5 x Junkers Jumo 211F-2 inverted V-12 liquid-cooled engines developing 1,300 horsepower each.
SPEED (MAX): 296 miles-per-hour (477 kilometers-per-hour; 258 knots)
RANGE: 1,174 miles (1,890 kilometers; 1,021 nautical miles)
CEILING: 16,010 feet (4,880 meters; 3.03 miles)
Detailing the development and operational history of the Heinkel He 111Z (Zwilling) Utility Transport Aircraft.
Entry last updated on 6/16/2018.
Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The He 111 Z (or "Zwilling") was a relatively successful joining of two He 111 medium-class bombers (detailed elsewhere on this site) to bring together an existing airframe designs suitable to transport the massive Messerschmitt Me 321 cargo glider. The He 111 Z became a possible solution with the intent that a large wing area with five installed powerplants would prove sufficient. Externally, the creation appeared as nothing more than two He 111 airframes joined at a common wing section with an extra (fifth) engine fitted to the joining structure.
A pair of twin-engine He 111 H-6's served as base conversion models for the new Heinkel Zwilling design. Two He 111 Z prototypes were then constructed with the He 111 H-6's joined by a center wing chord structure containing the fifth engine. The design was sound on the whole when evaluated by pilots at Rechlin and this resulted in ten production He 111 Z's ordered. The portside fuselage accommodated the pilot, primary mechanic, dedicated gunner and a radio operator/navigator while the starboard fuselage held the co-pilot, secondary mechanic and another gunner bringing the total crew count to seven (the co-pilot could double as a navigator if the situation pressed). The pilot was afforded full instrumentation while the co-pilot was given only a limited instrument panel. As such there was no real redundancy to the system as one might expect in such a design arrangement. The pilot was afforded five throttle levers for complete control over the five engine installations. Control for the radiator flaps was divided between the port and starboard cockpits with each man having control of the radiator flaps to his own side. Undercarriage control could be handled by either cockpit. Self-defense was managed through a variety of machine gun arrangements mostly centering on 7.7mm MG and/or 13mm MG machine guns as well as 20mm cannons. Armament varied, however, and was primarily dependent on what the "donor" He 111 H-6 airframe selected for conversion.
The engine configuration was made up of 5 x Junkers Jumo 211F 12-cylinder, liquid-cooled, inverted Vee engines of up to 1,340 horsepower each. These engines were fitted across five individual nacelles along the wing leading edge, three found at the center wing chord and two held outboard to either side of their respective fuselage in the usual way. Despite this multi-engined layout, the He 111 Z was still somewhat underpowered when attempting to pull a fully-loaded Me 321 glider. This was rectified through the utilization of rockets for additional thrust (RATO - "Rocket Assisted Take-Off") - not a wholly uncommon sight found at the beginning of the jet age. The Zwilling could, however, maintain flight if any or all of the three central wing cord engines failed - certainly showcasing the importance of the outboard engines. Range could be augmented by up to four external drop tanks which supplied the design its needed endurance.
By the end of the war, only four He 111 Zwillings were known to exist in operational condition despite some 12 total ultimately produced. The unaccounted for Zwillings were reportedly lost to Allied action while either in the air or still grounded. In any case, the Zwilling proved a (limited) success for it was quite capable of ferrying dozens of injured while being able to supply the massive Messerschmitt Me 321 gliders with a much-needed glider tug.
Several production marks of the He 111 Z were planned though only the original He 111 Z-1 ever saw any level of quantitative manufacture while the proposed Z-2 long-range bomber and Z-3 long-range reconnaissance platform never came to fruition. Both variants would have been based on the work already completed through the Z-1 production initiative.
Where applicable, the appearance of U.S. Department of Defense (DoD), Russian Ministry of Defense, Chinese Ministry of Defense or British Ministry of Defence visual information does not imply or constitute endorsement of this website (www.MilitaryFactory.com). Images marked with "www.MilitaryFactory.com" or featuring the Military Factory logo are copyrighted works exclusive to this site and not for reuse in any form.
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.
Relative Maximum Speed Rating
This entry's maximum listed speed (296mph).
Graph average of 225 miles-per-hour.
Graph showcases the Heinkel He 111Z (Zwilling)'s operational range (on internal fuel) when compared to distances between major cities.
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