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  • Messerschmitt Me 163 Komet (Comet) Single-Seat Rocket-Powered Interceptor Aircraft

    The explosive - literally and figuratively - Messerschmitt Me 163 Komet was the first operational combat aircraft design to incorporate swept wings.

     Updated: 5/18/2016; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com

    The German Messerschmitt Me 163 "Komet" was perhaps the most unique frontline, operational-level fighter design of World War 2. German engineers, seemingly always on the cutting edge of evolving war technology, developed the rocket-powered aircraft based on early testing completed with an engine-less glider. The resulting research produced the single-seat, swept-wing fighter that was equally dangerous to both enemy bomber crews and the Me 163 pilot alike. The Me 163 first flew on September 1st, 1941 and was formally introduced in the Luftwaffe inventory in 1944. Despite its impressive performance statistics, the Me 163 was something of a tactical failure and more or less a technological dead end with the rise of jet-powered flight soon to come. The idea of fast interceptors also soon gave way to ground-based homing/guided missile technologies.

    The Me 163 was born from the mind of Dr. Alexander Lippisch who pioneered a great deal of data research of tailless glider designs dating back to the 1920s prior to joining the Messerschmitt concern in 1939. Work began on such a tailless design through the DFS 194 glider outfitted with a Walter rocket motor. The motor relied on a volatile, though potent combination, known as "C-Stoff" and "T-Stoff". The new Messerschmitt design would utilize the chemical explosion to power the small fighter at break-neck speeds - able to outfly any bomber formation escort fighters with ease. More importantly, the design could be aloft in seconds in response to incoming waves of Allied bombers appearing through both day and night campaigns, wreaking havoc on German industry and supply lines. By 1944, the German initiative that was once held early in the war was all but lost and it began to fight more a defensive war for its very survival.

    Testing occurred at the covert Peenemunde facility in June of 1940 to help prove the concept sound. Despite the motor failing to impress due to reliability issues, the airframe itself handled well in the hands of test pilot Heini Dittmar. Serial production of several prototype forms was ordered under the "Me 163" designation in the early part of 1941. At least five "V" based prototypes emerged beginning with V1. Some eight preproduction forms then followed in the Me 163 "A-0" format. Early prototypes managed to reach an impressive 340 miles per hour in recorded test flights.

    The diminutive Me 163 was piloted by a single crewman housed under a wide clear canopy. The design was given the then-revolutionary concept of swept-back wings mounted along each fuselage side. The fuselage was a stout, portly design intended to house the cockpit and necessary fuel stores. The empennage was capped by a simple vertical tail fin lacking any horizontal planes. Take-off for the Me 163 was achieved by way of a wheeled, unsprung "dolly" assembly with the rocket motor at full thrust. The dolly was then jettisoned immediately after take-off for it proved an unnecessary counter-aerodynamic element. The interceptor then climbed to the required attack altitude to meet the incoming enemy bomber formation, most likely expending all of its fuel supply by this time. From its lofty perch, the accepted tactic for the Me 163 became a high-speed swoop down into the bomber formation, engaging targets with cannon for as long as momentum allowed - usually two or three dives though each swipe at the target was managed through a quick three-second-or-less window of opportunity. Once spent of both fuel and ammunition, the Komet was then glided to the ground under basic physics, landing on a relatively smooth patch of earth atop the provided spring-loaded centerline skid.

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    Messerschmitt Me163 B01a Komet (Comet) Technical Specifications

    Service Year: 1944
    Type: Single-Seat Rocket-Powered Interceptor Aircraft
    National Origin: Nazi Germany
    Manufacturer(s): Messerschmitt - Germany
    Production Total: 370

    Structural (Crew Space, Dimensions and Weights)

    Operating Crew: 1
    Length: 19.62 feet (5.98 meters)
    Width: 30.61 feet (9.33 meters)
    Height: 9.02 feet (2.75 meters)

    Weight (Empty): 4,189 lb (1,900 kg)
    Weight (MTOW): 9,480 lb (4,300 kg)

    Installed Power and Standard Day Performance

    Engine(s): 1 x Walter 109-509A-2 liquid-fueled rocket motor generating 3,800 lb of thrust for 7.5 minutes of powered flight.

    Maximum Speed: 659 mph (1,060 kph; 572 knots)
    Maximum Range: 25 miles (40 km)
    Service Ceiling: 39,698 feet (12,100 meters; 7.52 miles)
    Rate-of-Climb: 31,500 feet-per-minute (9,601 m/min)

    Armament / Mission Payload

    2 x 20mm cannons OR 2 x 30mm cannons in wing roots.

    Global Operators / Customers

    Nazi Germany; Japan (Mitsubishi J8M)

    Model Variants (Including Prototypes)

    DFS 194 - Tailless research glider of which the Me 163 is based on.

    Me 163 - Base series designation

    Me 163 V1 - Initial Prototype Model

    Me 163 V2 - Prototype

    Me 163 V3 - Prototype

    Me 163 V4 - Prototype

    Me 163 V5 - Prototype

    Me 163A - Initial prototype of which five were produced.

    Me 163A-0 - Eight pre-production examples based on the Me 163 prototype.

    Me 163B - Streamlined mass-production model; featuring improved rocket motor.

    Me 163B-0 - Pre-production models; fitted with 2 x 20mm MG 151/20 cannons in wing roots.

    Me 163B-1 - Production-quality airframes fitted with 2 x 30mm cannons in wing roots.

    Me 163B-1a

    Me 163S - Proposed dual-seat conversion trainer from modified Me 163B airframes.

    Mitsubishi J8M "Shusui" - Japanese variant based on acquired Me 163 manufacturing rights in 1943.