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    Horten Ho IX / Horten Ho 229 Jet-Powered Flying Wing / Fighter-Bomber (1945)

    Horten Ho IX / Horten Ho 229 Jet-Powered Flying Wing / Fighter-Bomber (1945)

    The Ho 229 brought about many firsts - advanced swept-back wings, a jet-powered flying wing design and radar absorbing stealth technology.





    Authored By Dan Alex  (Updated: 4/21/2016):

    The Horten Ho IX (or "Horten Ho 229" - sometimes wrongly designated the "Gotha Go 229") maintains a certain level of celebrity status in the world of military aviation, essentially becoming the first production-worthy form of any aircraft categorized as a true "flying wing" - that is an aircraft not relying on any sort of vertical tail surfaces to achieve flight and maneuverability. Additionally, the Ho IX/Ho 229 was the first to incorporate radar absorbing "stealth" technologies into its frame work - quite the accomplishment in forward thinking for 1944 - and made heavy use of swept-back wings before they became the norm of the jet age. In these ways alone, the Ho IX/Ho 229 was truly a marvel attempt in every way imaginable that a handful of prototypes were constructed to iron out the design. Though a production order was in the works by 1945 though the end of World War 2 saw to it that this machine never contributed to the German war effort in any respect, thus leaving the reader to his/her imagination as to the impact the system would have had in the skies over Europe.

    Flying Wings

    Flying wing designs had been the focus of man-a-aircraft engineer for some time leading up to World War 2. American Jack Northrop himself was one of the big name pioneers in the realm, working on his own flying wing designs, while the Horten brothers - Reimar and Walter Horten - had been studying the capabilities and possibilities for some time now primarily in the field of unpowered glider flight (a third brother, Wolfram, would later die when his bomber was downed over Dunkirk).

    Flying wings featuring a lack of vertical implements theoretically offered some inherent advantages by the deletion of such surfaces thus reducing drag to an extent. The Hortens strongly believed that such structures aboard a planform offered more drawbacks than additions. In a flying wing design, the fuselage was generally integrated into the wing roots for a very streamlined approach adding to effective aerodynamic principles. A larger wing surface area also promoted a better rate-of-climb, a larger fuel load (essentially increasing range) and a larger bomb load. However, the lack of vertical flying surfaces also brought about challenges in controlling such an aircraft - an issue that Northrop dealt with to a high degree in his XB-35 flying wing strategic bomber (finally realized in the modern Northrop B-2 Spirit stealth bomber). Northrop's attempt was in fact a commissioned effort to develop a wing-only design based on pictures received of the Horten early 1930's glider attempts. Such wing-only flight would not be realized until the advent of powerful computers in the modern age that could aid the pilot in flight, keeping the aircraft from entering irrecoverable actions.

    Horten Roots

    With restrictions set forth by the Treaty of Versailles following World War 1, the German manufacturing capacity for waging war was severely restricted by the victors. As such, government funding that may have been intended for the production of tanks, guns, planes and the like were instead funneled to other "peacetime" ventures within the country. One such venture proved to be the various glider clubs forming across Germany. These clubs allowed Reimar and Walter the chance to forge some tail-less glider design concepts into practice. Essentially, the glider club was another German attempt to skirt the rules of the Versailles Treaty and train young pilots while testing out aircraft designs under a certain level of secrecy. Though never formally trained in aeronautics, the Hortens maintained a love affair with flight and grew into experienced pilots in their own right, this occurring in their critical early years and helping to pave a legacy now forthcoming. Even as teenagers, their first flyable glider was completed in 1933.

    The brothers took to developing models in the beginning and then culminated this process with the production of the Ho I sailplane in 1934. The Ho I was a tail-less system with straight wings that, by all accounts, flew quite well. The pilot sat in a prone position within the apex of wing assembly while elevons were utilized for pitch and roll control while brake flaps were integrated to account for yaw. These brake flaps were affixed to the upper and lower sections of the wing leading edge.

    Despite this early success, the Horten brothers were destined to get more out of their concept and put forth a newer design approach. They destroying their original Ho I and took to building a more efficient design. The second attempt was appropriately designated as Ho II and featured swept-back leading and trailing edge wings, a prone glazed-over cockpit and instantly set itself apart from the preceding design attempt. Four Ho II prototypes were produced to test out further flying wing concepts and while at least one of these was powered through a single Hirth-brand 80 horsepower engine mounted to the rear of the main body in a "pusher" arrangement. The Ho IIs were tested sometime in 1938, with one such flight occurring at Darmstadt in the capable hands of renowned female test pilot Hanna Reitsch.



     SPECIFICATIONS 


    Horten Ho 229 A-0
    Type: Jet-Powered Flying Wing / Fighter-Bomber
    National Origin: Nazi Germany [ VIEW ]
    Manufacturer(s): Gothaer Waggonfabrik / Horten - Germany [ VIEW ]
    Introduction: 1945
    Production Total: 2 [ VIEW ]

     GLOBAL OPERATORS 


    Nazi Germany


     CHARACTERISTICS 


    Crew: 1
    Length: 24.51 feet (7.47 meters)
    Width: 54.99 feet (16.76 meters)
    Height: 9.19 feet (2.80 meters)
    Weight (Empty): 10,141 lb (4,600 kg)
    Weight (MTOW): 17,857 lb (8,100 kg)


     STANDARD DAY PERFORMANCE 


    Maximum Speed: 607 mph (977 kmh; 528 knots)
    Maximum Range: 1,181 miles (1,900 km)
    Service Ceiling: 52,493 feet (16,000 meters; 9.9 miles)
    Rate-of-Climb: 4,330 feet-per-minute (1,320 m/min)


     INSTALLED POWER 


    Powerplant: 2 x Junkers Jumo 109-004C turbojet engines developing 2,205 lb of thrust each.


     ARMAMENT / MISSION PAYLOAD 


    Hardpoints: 2
    Armament / Mission Payload:
    ORIGINALLY PROPOSED:
    2 x 30mm MK 108 cannons
    2 x 1,100lb bombs

    Go 229 A-0:
    4 x 30mm MK 103 cannons
    2 x 2,205lb bombs

    Other possible armament could have included:

    24 x R4M air-to-air/air-to-surface rockets
    2 x 30mm underwing cannon pods
    2 x 30mm underwing cannon pod


     VARIANTS 


    Ho IX V1 - Initial Prototype; powerless glider; single example

    Ho IX V2 - Rebuilt airframe to accommodate Junkers 109-004B-1 engines; single example; lost to accident from engine failure.

    Ho IX V3 (Gotha 229 V3) - Two Junkers Jumo 109-004C turbojets of 2,205 thrust; revised engine intakes; repositioned engines forward in fuselage.

    Go 229 V4 - Two-seat All-Weather/Nightfighter Variant; never produced.

    Go 229 V5 - Two-Seat All-Weather/Nightfighter Variant; never produced.

    Go 229 V6 - Armament Test Prototype; fitting 4 x MK 103 cannons

    Ho 229 V6 (IXb) -Two-Seat Trainer; never produced.

    Ho 229 V7 (IXb) - Two-Seat Nightfighter; never produced.

    Go 229A-0 - Production Model Designation; based on Go 220 V6 prototype; fitting 4 x MK 103 cannons; provision for 2 x 2,205lb bombs; 20 examples on order; never produced.


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