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Study Guide: Messerschmitt Me 210: Design, Development, and Operational History

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Messerschmitt Me 210: Design, Development, and Operational History Study Guide

Origins and Design Goals

The Messerschmitt Me 210 was primarily designed as a light fighter intended for engaging enemy bombers.

Answer: False

Explanation: The Messerschmitt Me 210 was designed primarily as a heavy fighter and ground-attack aircraft, intended as a successor to the Bf 110, rather than a light fighter for engaging bombers.

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Development of the Me 210 began in 1937, prior to the first flight of its predecessor, the Bf 110.

Answer: True

Explanation: The design phase for the Messerschmitt Me 210 commenced in 1937, preceding the initial flight of its predecessor, the Messerschmitt Bf 110.

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What was the intended primary role of the Messerschmitt Me 210?

Answer: A heavy fighter and ground-attack aircraft.

Explanation: The Messerschmitt Me 210 was conceived and designed primarily to serve as a heavy fighter and ground-attack aircraft, intended to succeed the Bf 110.

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When did the design work for the Me 210, intended as a Bf 110 replacement, commence?

Answer: In 1937, before the Bf 110's first flight.

Explanation: Design work for the Me 210, which was intended as a replacement for the Bf 110, commenced in 1937, prior to the first flight of the Bf 110.

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Which of the following was a key design difference that distinguished the Me 210 from the Bf 110?

Answer: The Me 210 had a redesigned nose section and an internal bomb bay.

Explanation: A key design difference was the Me 210's redesigned nose section and its incorporation of an internal bomb bay, distinguishing it from the Bf 110's external ordnance carriage.

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Development and Prototypes

The second Me 210 prototype (V2) was successfully used for extensive flight testing after initial minor issues were resolved.

Answer: False

Explanation: The second prototype (V2) met a catastrophic end in September 1940 when it was lost due to an unrecoverable spin, underscoring the critical stability issues inherent in the design.

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The initial RLM order for 1,000 Me 210s was placed after the aircraft had successfully completed its initial flight tests.

Answer: False

Explanation: The substantial order for 1,000 Me 210s from the RLM was placed prior to the aircraft's initial flight tests, a decision later recognized as a significant error due to the subsequent discovery of severe design flaws.

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What happened to the second Me 210 prototype (V2) in September 1940?

Answer: It was lost when the pilot could not recover from a spin.

Explanation: In September 1940, the second prototype, Me 210 V2, was lost when its pilot failed to recover from a spin.

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Technical Specifications and Armament

A key design difference between the Me 210 and the Bf 110 was the Me 210's use of external bomb racks for all ordnance.

Answer: False

Explanation: A significant design distinction was the Me 210's incorporation of an internal bomb bay, unlike the Bf 110 which typically carried ordnance externally. This internal bay contributed to reduced drag and a cleaner aerodynamic profile.

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The Me 210 was projected to be significantly slower than the Bf 110, with an expected top speed of around 500 km/h.

Answer: False

Explanation: Contrary to the statement, the Me 210 was projected to be significantly faster than the Bf 110. With its intended Daimler-Benz DB 601F engines, its expected top speed was approximately 620 km/h (390 mph), representing a substantial increase over the Bf 110.

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The Me 210's landing gear retraction system was unique, involving a complex hydraulic system that folded the wheels inward.

Answer: False

Explanation: The Me 210's main landing gear retraction system involved each strut twisting 90 degrees, allowing the wheel to be housed within the wing structure. This mechanism was not unique and was similar to that used on the Junkers Ju 88.

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In its fighter configuration, the Me 210 could be armed with up to four 20 mm cannons housed within its internal bomb bay.

Answer: True

Explanation: In its fighter configuration, the internal bomb bay of the Messerschmitt Me 210 was capable of accommodating up to four 20 mm cannons.

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The defensive armament of the Me 210 consisted of manually operated machine guns mounted in the cockpit.

Answer: False

Explanation: The defensive armament of the Me 210 comprised two 13 mm MG 131 machine guns housed in remotely controlled turrets located on the fuselage sides, not manually operated guns in the cockpit.

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The 44M Lidérc was a Hungarian-developed radar-guided missile intended for use against ground targets with the Me 210.

Answer: False

Explanation: The 44M Lidérc was a Hungarian-developed acoustic proximity-fused air-to-air rocket intended for use against bombers, not a radar-guided missile for ground targets.

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The Stuvi 5B bombsight was located in the rear defensive turret of the Me 210.

Answer: False

Explanation: The Stuvi 5B bombsight was situated in the nose of the Me 210, not in the rear defensive turret, and was designed for shallow-angle dive bombing.

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What was the projected top speed of the Me 210 with its intended Daimler-Benz DB 601F engines?

Answer: Approximately 620 km/h (390 mph)

Explanation: Equipped with the intended Daimler-Benz DB 601F engines, the Me 210 was projected to achieve a maximum speed of approximately 620 km/h (390 mph).

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How did the Me 210's main landing gear retract?

Answer: Each strut twisted 90 degrees, housing the wheel in the wing.

Explanation: The main landing gear struts of the Me 210 retracted by twisting 90 degrees, enabling the wheel to be housed within the wing structure.

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What armament could be fitted inside the Me 210's internal bomb bay in its fighter role?

Answer: Four 20 mm cannons.

Explanation: In its fighter configuration, the internal bomb bay of the Me 210 could be equipped with four 20 mm cannons.

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Describe the defensive armament system of the Me 210.

Answer: Two 13 mm MG 131 machine guns in remotely controlled fuselage turrets.

Explanation: The defensive armament consisted of two 13 mm MG 131 machine guns mounted in remotely controlled fuselage turrets, designed for rearward defense.

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What was the 44M Lidérc project related to the Me 210?

Answer: An acoustic proximity-fused air-to-air rocket.

Explanation: The 44M Lidérc project involved a Hungarian-developed acoustic proximity-fused air-to-air rocket intended for use against bombers.

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What was the purpose of the Stuvi 5B bombsight in the Me 210?

Answer: Aiming for shallow-angle dive bombing.

Explanation: The Stuvi 5B bombsight, installed in the nose of the Me 210, was engineered for precision aiming during shallow-angle dive bombing attacks.

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How did the remotely controlled FDSL 131/1B turrets on the Me 210 allow the gunner to aim?

Answer: Using a handgun-style grip and sight.

Explanation: The remotely controlled FDSL 131/1B turrets on the Me 210 allowed the gunner to aim using a handgun-style grip and sight.

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Flight Characteristics and Design Flaws

The Me 210's development was relatively smooth, with only minor adjustments needed for stability.

Answer: False

Explanation: The development of the Me 210 was marked by significant challenges, particularly concerning its stability and flight characteristics, which required extensive modifications and were not easily resolved.

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To address handling problems, the rear fuselage of the Me 210 was lengthened by approximately one meter in later versions.

Answer: True

Explanation: To mitigate handling deficiencies, a significant modification designated 'lang' involved lengthening the rear fuselage section by approximately 92 cm (36-1/4 inches).

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The primary reason for the Me 210's failure as an operational aircraft was its high fuel consumption.

Answer: False

Explanation: The principal factor contributing to the Me 210's failure as an operational aircraft was its unacceptably poor flight characteristics, stemming from fundamental design flaws, rather than high fuel consumption.

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Which of the following was a major flight characteristic problem encountered during the Me 210's development?

Answer: Poor stability during turns and a tendency to oscillate.

Explanation: A significant problem encountered during the Me 210's development was its poor stability during turns, coupled with a tendency to oscillate even in level flight.

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What modification, designated 'lang', was made to the Me 210 airframe to improve handling?

Answer: Lengthening the rear fuselage section.

Explanation: The modification designated 'lang' involved lengthening the rear fuselage section of the Me 210 airframe by approximately 92 cm (36-1/4 inches) to enhance its handling characteristics.

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What was the primary factor contributing to the Me 210's failure as an operational aircraft?

Answer: Unacceptably poor flight characteristics due to design flaws.

Explanation: The principal factor contributing to the Me 210's failure as an operational aircraft was its unacceptably poor flight characteristics, which were rooted in fundamental design flaws.

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Variants and Production

The Me 210C variant was powered by the older Daimler-Benz DB 601F engines.

Answer: False

Explanation: The Me 210C variant was powered by the more advanced Daimler-Benz DB 605 engines, not the older DB 601F.

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Hungary exclusively produced the Me 210 for its own air force under a license agreement with Germany.

Answer: False

Explanation: While Hungary did produce the Me 210 under license (designated Me 210Ca), the production agreement stipulated that two out of every three aircraft were designated for the German Luftwaffe, not exclusively for the Hungarian Air Force.

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A total of 108 Hungarian-built Me 210 Ca-1 aircraft were supplied to the German Luftwaffe.

Answer: True

Explanation: The German Luftwaffe received a total of 108 Hungarian-built Me 210 Ca-1 aircraft, as part of the overall production of 267 Me 210C variants.

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The initial production variants of the Me 210 were designated A-0 and A-1, serving as fighter-bombers.

Answer: False

Explanation: The initial production variants were designated Me 210 A-1 (fighter-bomber/heavy fighter) and Me 210 A-2 (dive bomber/heavy fighter). The A-0 designation referred to pre-production aircraft.

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The Me 210 Ca-1 variant was distinguished by its use of Daimler-Benz DB 601 engines and a standard airframe.

Answer: False

Explanation: The Me 210 Ca-1 variant was distinguished by its use of Daimler-Benz DB 605B engines and an improved airframe, not the older DB 601 engines.

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Some Hungarian Me 210 Ca-1 aircraft were modified to carry a 40 mm Bofors cannon in the lower fuselage for anti-bomber roles.

Answer: True

Explanation: Certain Hungarian Me 210 Ca-1 aircraft were indeed modified to incorporate a 40 mm Bofors autocannon in the lower fuselage, specifically intended for the role of destroying Allied bombers.

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The Me 210D was a successful variant that entered mass production and saw service with the Luftwaffe.

Answer: False

Explanation: The Me 210D variant was planned but never progressed beyond the project stage and was not built or put into production.

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Which engines powered the improved Me 210C variant?

Answer: Daimler-Benz DB 605

Explanation: The improved Me 210C variant was powered by Daimler-Benz DB 605 engines.

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Under the production agreement for the Me 210Ca in Hungary, what proportion of aircraft were designated for the German Luftwaffe?

Answer: Two out of every three aircraft.

Explanation: The production agreement for the Hungarian-licensed Me 210Ca stipulated that two-thirds of the aircraft produced were to be supplied to the German Luftwaffe.

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What was the initial production outcome for the Me 210 in Germany in 1942?

Answer: Production was halted after only 90 aircraft were delivered.

Explanation: In 1942, German production of the Me 210 was halted after only 90 aircraft had been delivered, significantly limiting its operational deployment.

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What was the total production number for the Me 210C variants, and how many were supplied to the Luftwaffe?

Answer: 267 built, 108 to Luftwaffe.

Explanation: A total of 267 Me 210C variants were produced, with 108 of these aircraft being supplied to the German Luftwaffe.

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What were the designations for the initial production variants of the Me 210?

Answer: Me 210 A-1 and Me 210 A-2

Explanation: The initial production variants of the Me 210 were designated Me 210 A-1 and Me 210 A-2, following the pre-production A-0 models.

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What engines powered the Hungarian-licensed Me 210 Ca-1 variant?

Answer: Daimler-Benz DB 605B

Explanation: The Hungarian-licensed Me 210 Ca-1 variant was powered by two Daimler-Benz DB 605B engines.

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For what purpose were some Hungarian Me 210 Ca-1 aircraft modified with a 40 mm Bofors cannon?

Answer: Destroying Allied bombers.

Explanation: Some Hungarian Me 210 Ca-1 aircraft were modified to carry a 40 mm Bofors cannon in the lower fuselage, specifically for the purpose of destroying Allied bombers.

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What became of the planned Me 210D variant?

Answer: It remained only a project and was never built.

Explanation: The planned Me 210D variant remained solely a project and was never constructed or put into production.

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How many Hungarian-built Me 210 Ca-1 aircraft were operated by the Royal Hungarian Air Force?

Answer: 179

Explanation: The Royal Hungarian Air Force operated a total of 179 Hungarian-built Me 210 Ca-1 aircraft.

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Operational Service and Deployment

The Me 210 entered widespread service with the Luftwaffe in 1942, with thousands of units delivered.

Answer: False

Explanation: The Me 210 entered limited service with the Luftwaffe in 1942, but production was halted early, with only 90 aircraft delivered, far short of widespread service or thousands of units.

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Both the Luftwaffe and the Royal Hungarian Air Force found the Hungarian-built Me 210Ca-1 aircraft to be unsatisfactory.

Answer: False

Explanation: Contrary to the statement, both the Luftwaffe and the Royal Hungarian Air Force reportedly found the Hungarian-built Me 210Ca-1 aircraft to be satisfactory and relatively successful.

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The Luftwaffe's Me 210 units saw extensive combat service primarily on the Eastern Front.

Answer: False

Explanation: The Luftwaffe's operational deployment of Me 210 units was primarily concentrated in North Africa, specifically Tunisia and Sardinia, rather than the Eastern Front.

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Besides Germany and Hungary, the Me 210 was also operated operationally by the Japanese Imperial Army.

Answer: False

Explanation: While Japan received a single Me 210 aircraft, it was solely for testing purposes and not for operational service with the Japanese Imperial Army.

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The Luftwaffe operated a total of 198 Me 210 aircraft, combining German-built and Hungarian-built models.

Answer: True

Explanation: The Luftwaffe's operational fleet comprised a total of 198 Me 210 aircraft, consisting of 90 German-built units (primarily A-series) and 108 Hungarian-built Me 210 Ca-1 models.

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The Royal Hungarian Air Force operated fewer Me 210 Ca-1 aircraft than the German Luftwaffe.

Answer: False

Explanation: The Royal Hungarian Air Force operated 179 Me 210 Ca-1 aircraft, which is more than the 108 Hungarian-built units supplied to the German Luftwaffe.

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The last Hungarian Me 210s were retired due to obsolescence at the end of World War II.

Answer: False

Explanation: The final Hungarian Me 210s were destroyed by their crews in March 1945 due to a critical lack of fuel and spare parts, rather than being retired due to obsolescence at the war's end.

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How were the Hungarian-built Me 210s received by their operators?

Answer: Both the Luftwaffe and the Royal Hungarian Air Force were reportedly satisfied.

Explanation: Reports indicate that both the German Luftwaffe and the Royal Hungarian Air Force were satisfied with the performance and reliability of the Hungarian-built Me 210 aircraft.

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In which theaters did the Luftwaffe primarily deploy its Me 210 units?

Answer: North Africa (Tunisia and Sardinia).

Explanation: The Luftwaffe primarily deployed its Me 210 units for combat operations in the North African theaters, specifically Tunisia and Sardinia.

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Which nation, besides Germany and Hungary, received a single Me 210 for testing purposes?

Answer: Japan

Explanation: Japan received a single Messerschmitt Me 210 aircraft for testing purposes, in addition to Germany and Hungary.

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Why were the last Hungarian Me 210s destroyed in March 1945?

Answer: Because of a lack of fuel and spare parts.

Explanation: The final Hungarian Me 210s were destroyed by their crews in March 1945 due to a critical shortage of fuel and essential spare parts.

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Programmatic Outcomes and Legacy

The failure of the Me 210 program forced the Luftwaffe to continue using the outdated Bf 110, leading to increased losses.

Answer: True

Explanation: The unsuccessful development and limited deployment of the Me 210 compelled the Luftwaffe to continue relying on the increasingly outdated Bf 110, which resulted in elevated losses for its heavy fighter units.

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The Messerschmitt Me 310 was the direct successor that replaced the Me 210 in Luftwaffe service.

Answer: False

Explanation: The Messerschmitt Me 410 Hornisse, a further development of the Me 210, served as its successor and eventually replaced it in Luftwaffe service, not the Me 310.

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The failure of the Me 210 program had what significant consequence for the Luftwaffe's heavy fighter units?

Answer: They were forced to continue operating the outdated Bf 110, leading to higher losses.

Explanation: The failure of the Me 210 program necessitated the continued operation of the outdated Bf 110 by Luftwaffe heavy fighter units, resulting in increased combat losses.

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Which aircraft, a further development of the Me 210, eventually replaced it in Luftwaffe service?

Answer: Messerschmitt Me 410 Hornisse

Explanation: The Messerschmitt Me 410 Hornisse, which represented a further development of the Me 210, ultimately succeeded and replaced it in Luftwaffe service.

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The RLM's decision to order 1,000 Me 210s before the prototype flew is described as a major error primarily because:

Answer: The aircraft suffered from severe design flaws and poor flight characteristics.

Explanation: The RLM's decision to order 1,000 Me 210s prior to its prototype flight was a major error primarily due to the aircraft subsequently exhibiting severe design flaws and poor flight characteristics.

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