Zlin Z-43 "Military/Ambulance" airplane kit in 1/72 scale - Kovozávody Prostejov model. The Zlín Z-43 "Military/Ambulance" is a military variant of the Czechoslovak Zlín Z-43 light aircraft, originally designed for civilian use and training. In the military it was adapted for liaison, observation and light medical transport tasks. Main features: Role: Liaison/light ambulance aircraft Crew: 1 pilot + 1 or 2 operators/patients Engine: Avia M 337, 6 cylinders, air-cooled Configuration: Low-wing monoplane with fixed tricycle undercarriage Maximum speed: Approximately 250 km/h Uses in the military version: Emergency medical transport (MEDEVAC): can transport a stretchered patient and a medical assistant. Inter-base liaison and communications. Short-range observation and patrolling. This version served mainly in Warsaw Pact countries and some non-aligned states. Although a light aircraft, it proved useful in logistical and support tasks due to its simplicity and reliability.
Zlin Z-43 aircraft kit in 1/72 scale - Kovozávody Prostejov model. The Zlín Z-43 is a Czechoslovak-made light touring and training aircraft developed in the 1960s by Moravan Otrokovice as an evolution of the earlier Zlín Z-42. Main features: Type: Light touring/educational aircraft Seats: 4 (pilot + 3 passengers) Engine: An Avia M 337 piston engine (about 210 horsepower) Top speed: About 250 km/h Autonomy: About 900 km Structure: Low-wing monoplane, fixed tricycle undercarriage Uses: The Z-43 was mainly employed for: Civilian pilot training Aeroclub and sport use Light transport Observation and patrolling Rugged, reliable and easy to fly, it has been widely used in Eastern Europe and other countries for its versatility and low operating costs.
Aircraft kit TG-10D Peregrine / Let L-33 Solo in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The TG-10D Peregrine (U.S. military designation) is the U.S. Air Force's adopted version of the Let L-33 Solo, a single-seat advanced training glider designed and built in the Czech Republic by Let Kunovice in the 1990s. It is intended as an intermediate step between two-seat school gliders, such as the Let L-13 Blaník, and competition models, allowing student pilots to gain experience in solo flight. Main features: Type: Single-seat advanced training glider Structure: Metal (like the Blaník), sturdy and modern design Wingspan: About 15 meters Trolley: Retractable Role: Advanced training in gliding Used at theUSAF Academy, the TG-10D is highly regarded for its stability, handling and ease of maintenance, making it ideal for training in silent flight and perfecting unpowered piloting techniques.
Mikojan-Gurjevic MiG-19S/Shenyang F-6 aircraft kit in 1/72 scale - Kovozávody Prostejov model. The Mikojan-Gurjevic MiG-19S is an advanced version of the MiG-19, the first Soviet fighter capable of exceeding Mach 1 in level flight, which entered service in the mid-1950s. It was equipped with aerodynamic improvements, new avionics systems and an upgraded armament. The Shenyang F-6 is the Chinese license-produced version of the MiG-19, made by the Shenyang Aircraft Corporation. It entered service in the 1960s and was widely exported to many countries, including Pakistan, North Korea, Egypt and Iraq. Common features: Engines: 2 Tumansky RD-9 turbojets (or WP-6 in the Chinese version) Maximum speed: Approximately Mach 1.2 Armament: 3 30 mm cannons, bombs, rockets or air-to-air missiles (in the modified F-6 version) Role: Interceptor and ground attack Main differences: The MiG-19S had more advanced avionics for the time, but was soon outdated. The F-6 was upgraded with more modern systems over time and remained in service until the 2000s in some countries. Both represented an important milestone in the development of supersonic fighters during the Cold War, especially in the Eastern Bloc and China's allied countries.
Mikojan-Gurjevic MiG-19S "Over Eastern Europe" airplane kit in 1/72 scale - Kovozávody Prostejov model. The Mikojan-Gurjevic MiG-19S "Over Eastern Europe" is a variant of the MiG-19, the first Soviet jet fighter capable of flying at supersonic speed in level flight. The "S" (Stryebitel) model was one of the main versions, improved for operational deployments in Warsaw Pact countries and especially widespread in Eastern Europe during the Cold War. Main features: Role: Frontline supersonic fighter Engine: Two Tumansky RD-9B turbojets Maximum Speed: Over Mach 1.2 Armament: 3 NR-30 30 mm cannons Possibility of rockets and light bombs Autonomy: About 2,200 km (with additional tanks) Use: Interception and ground attack Context "Over Eastern Europe: The MiG-19S was widely exported and employed by air forces in countries such as Poland, East Germany, Czechoslovakia, Bulgaria and others. It represented a major evolutionary step from the MiG-15 and MiG-17, introducing the use of two engines and greater firepower, although it was soon superseded by the MiG-21. It was known to be robust, fast, but also difficult to fly, especially at high speed and low altitude. Nevertheless, it was a symbol of Soviet technological supremacy in the mid-1950s.
Let L-33 Solo "Over Europe" airplane kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Let L-33 Solo is a single-seat advanced training glider designed and produced in the Czech Republic by Let Kunovice in the 1990s. It is intended as an intermediate step between two-seater school gliders (such as the Let L-13 Blaník) and competition models. Main features: Type: Single-seat training glider Structure: Metal (similar to Blaník), with a modern and clean design Wingspan: About 15 meters Retractable trolley Role: Advanced training, refinement of unpowered flight It is highly regarded for its stability in flight, ease of piloting and simple maintenance, making it an ideal choice for pilots new to performance gliders.
British BAC 167 Strikemaster Attack Aircraft Kit + Paint Mask and 3D Details in 1/48 scale - Model KOVOZAVODY PROSTEJOV. The BAC 167 Strikemaster is a British light attack and training aircraft developed by the British Aircraft Corporation (BAC) in the 1960s. It is an armed and upgraded version of the Jet Provost T.Mk 5, designed for counter-guerrilla operations, close support and advanced training. Key features: Role: Light attack and training aircraft Crew: 2 (pilot and instructor) Engine: 1 Rolls-Royce Viper turbojet Top speed: About 860 km/h Autonomy: About 1,450 km Armament: 7.62 mm machine guns (generally in wing pods) Unguided rockets and light bombs on subalar pylons Employment: The BAC Strikemaster was widely exported, being used by air forces in countries such as Oman, Saudi Arabia, New Zealand, Ecuador and others. It was valued for ease of maintenance, low cost, and ability to operate even from semi-prepared runways. In combat it was used in several local conflicts, particularly in low-intensity scenarios where total air supremacy was not necessary.
Soptwith Triplane aircraft kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Sopwith Tri plane was a British World War I fighter aircraft designed and built by the Sopwith Aviation Company. Introduced in 1916, it was the first triplane fighter to enter operational service, distinguished by its excellent maneuverability and climb rate. Technical characteristics Type: Single-seat triplane fighter Entry into service: 1916 Length: 5.73 m Wingspan: 8.08 m Height: 3.20 m Empty weight: 499 kg Maximum take-off weight: 698 kg Engine and performance Engine: Clerget 9B (9-cylinder air-cooled radial) Power: 130 hp Top speed: 187 km/h Autonomy: 480 km Operational tangency: 6,250 m Climbing speed: 5,200 m in 10 minutes The triplane design providedexcellent maneuverability and rapid ascent, making it superior to German biplanes of the time. Armament 1 Vickers 7.7 mm machine gun, synchronized with the propeller Although some experimental versions mounted two machine guns, the additional weight reduced performance, so most operational examples retained only one armament. Operational role and use Air superiority fighter: Outperformed Fokkers and Albatros in maneuverability. Escort to scouts: Protected allied observation aircraft. Interceptor: Rapid climb to intercept enemy aircraft at high altitude. Historical impact and famous pilots The Sopwith Triplane was mainly used by the No. 1 Squadron of the Royal Naval Air Service (RNAS). Its agility inspired the Germans to develop the famous Fokker Dr.I, the Red Baron Triplane. Among the best-known pilots: Raymond Collishaw (60 victories), leader of the "Black Flight" Robert Little (47 wins), one of Australia's most decorated aces Conclusion The Sopwith Triplane revolutionized aerial combat because of its extraordinary maneuverability and climb rate. However, it was soon replaced by the more powerful and better armed Sopwith Camel. Despite its short operational career, the Triplane left its mark on aviation history, influencing the development of German triplane fighters.
Focke-Wulf Fw 190A-4 aircraft kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Focke-Wulf Fw 190A-4 was an improved version of the famous German Fw 190 fighter, which entered service with the Luftwaffe in the fall of 1942. Based on the earlier A-3, it introduced improvements in communication systems and the ability to mount auxiliary tanks or additional armaments, increasing its versatility in combat. Technical characteristics Type: single-engine, propeller-driven fighter Entry into service: Fall 1942 Length: 8.84 m Wingspan: 10.51 m Height: 3.95 m Empty weight: 3,220 kg Maximum takeoff weight: 4,400 kg Engine and performance Engine: BMW 801D-2 (14-cylinder air-cooled radial) Power: 1,677 hp Top speed: 656 km/h at 6,000 m Range: 800 km (up to 1,300 km with additional fuel tank) Operating tangency: 11,000 m Climbing speed: 900 m/min The A-4 retained the BMW 801D-2 engine, but with a methanol-water injection system (MW 50) available on some variants for a short increase in power. Armament The Fw 190A-4 had the same powerful armament as its predecessor: 2 MG 17 7.92 mm machine guns (above engine, 900 rounds total) 2 MG 151/20 20 mm guns (in the wings, 250 rounds each) 2 MG FF/M 20 mm cannons (in the wingtips, 55 rounds each) It could also carry an additional tank or bomb of up to 500 kg under the fuselage, making it effective even in ground attack missions. Operational role and use Air superiority fighter: Excellent performance against the Spitfire Mk V. Bomber interceptor: Due to its heavy armament. Ground attack: Configurations with bombs or rockets for tactical support. Reich defense: Used to counter Allied bombers. Luftwaffe axes and historical impact. The Fw 190A-4 was employed by many experienced Luftwaffe pilots, including: Hermann Graf (212 victories) Walter Nowotny (258 victories) Erich Rudorffer (222 wins) This model maintained superiority in European skies until the appearance of the Spitfire Mk IX and the P-51 Mustang, which forced the Luftwaffe to develop even more advanced versions of the Fw 190. Conclusion The Focke-Wulf Fw 190A-4 represented a major evolution of the A-series, with greater operational flexibility and consistently top-notch performance. It was a major player in the air battles of 1942-43, proving a lethal opponent for Allied fighters and bombers.
Focke-Wulf Fw 190A-3 ''Aces'' aircraft kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Focke-Wulf Fw 190A-3 was one of the first large-scale operational versions of the famous German Fw 190 fighter jet, developed by Focke-Wulf Flugzeugbau AG and employed by the Luftwaffe from the spring of 1942. Compared with earlier versions(A-1 and A-2), theA-3 introduced a more powerful engine and improved structure, quickly becoming one of the most feared fighters of the period. The designation "Aces" refers to the many Luftwaffe aces who used it with great success in the skies over Europe, achieving many aerial victories. Technical characteristics Type: Single-engine, propeller-driven fighter Entry into service: Spring 1942 Length: 8.84 m Wingspan: 10.51 m Height: 3.95 m Empty weight: 3,210 kg Maximum takeoff weight: 4,400 kg Engine and performance Engine: BMW 801D-2 (14-cylinder air-cooled radial) Power: 1,677 hp Top speed: 660 km/h at 6,000 m Range: 800 km (up to 1,300 km with additional fuel tank) Operating tangency: 11,000 m Climbing speed: 900 m/min Adoption of the BMW 801D-2 engine increased power and improved performance at all altitudes, making it a formidable opponent against Allied fighters. Armament The Fw 190A-3 had impressive armament, enabling it to deal effectively with both enemy fighters and bombers: 2 MG 17 7.92 mm machine guns (mounted above the engine, 900 rounds total) 2 MG 151/20 20 mm guns (mounted in the wings, 250 rounds each) 2 MG FF/M 20 mm cannons (mounted in the wingtips, 55 rounds each) Because of this configuration, the fighter had a high capacity to destroy air and ground targets with only a few shots. Operational role and use Air superiority fighter: The Fw 190A-3 proved superior to the RAF's Spitfire Mk V, which struggled to counter it. Bomber interceptor: Its powerful armament enabled it to shoot down American B-17 and B-24 bombers. Ground attack: Some units used it with light bombs for missions to support ground troops. Defense of the Reich: Employed to protect strategic targets from Allied air raids. Luftwaffe axes and historical impact. Many Luftwaffe aces achieved a large number of victories aboard the Fw 190A-3. Among the most famous: Hans Hahn (108 victories) Otto Kittel (267 victories, the fourth most knockdown ace in history) Walter Nowotny (258 wins) The Fw 190A-3 contributed greatly to Luftwaffe supremacy in 1942, prompting the Allies to develop more advanced fighters such as the Spitfire Mk IX and the P-51 Mustang. Conclusion The Focke-Wulf Fw 190A-3 "Aces" was one of the most iconic versions of the German fighter due to its combination of power, speed and firepower. It dominated European skies in 1942, becoming the preferred aircraft of many German aces before Allied fighters evolved to counter it.
Cessna U-17B "Asian users" airplane kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Cessna U-17B is a military version of the famous Cessna 185 Skywagon, used mainly for reconnaissance, light transport and liaison missions. The term " Asian Users" refers to Asian operators who employed this aircraft in their air forces, particularly during the Vietnam War and other regional conflicts. Technical characteristics Type: Liaison and reconnaissance aircraft Entry into service: 1960s Length: 7.92 m Wingspan: 10.92 m Height: 2.36 m Empty weight: 771 kg Maximum takeoff weight: 1,520 kg Engine and performance Engine: Continental IO-520-D (6 cylinders, air-cooled) Power: 300 hp Top speed: 270 km/h Autonomy: 1,300 km Operational tangency: 5,500 m Climbing speed: 5.1 m/s The Cessna U-17B was known for its reliability, ease of maintenance and STOL (Short Takeoff and Landing) capabilities, which made it suitable for operations in improvised runways and harsh environments. Operational role and use Reconnaissance and observation: Territory monitoring and target spotting. Light transport: Movement of personnel and materials in remote areas. COIN (Counter-Insurgency) Missions: Used to support counterinsurgency operations. Medical Evacuation: Transportation of wounded in conflict zones. Key Asian users. The Cessna U-17B was widely used by several Asian air forces, including: South Vietnam (VNAF): Used for reconnaissance and liaison during the Vietnam War. Thailand: Employed for military patrol and transport operations. Philippines: Used by the Air Force for surveillance missions and logistical support. Laos: Deployed for covert missions during the Indochinese conflict. Historical impact The Cessna U-17B played a key role in light air operations in Asia, demonstrating the versatility and robustness typical of Cessna aircraft. Despite its non-offensive nature, it had a significant impact in local wars, especially in Vietnam, where it was often employed to support ground troops and lead air strikes. Conclusion The Cessna U-17B "Asian Users" represents one of the most reliable light military aircraft employed in Asia in the 1960s and 1970s. Its versatility and STOL capability made it ideal for operations in harsh environments, contributing to the mobility and effectiveness of regional air forces.
Avro 504K "Comic" airplane kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. TheAvro 504K "Comic" was a special version of the famous Avro 504, modified for the night fighter role during World War I. Designed to intercept German Zeppelin and Gotha bombers, the "Comic" was distinguished by repositioned armament and increased maneuverability in night combat. Technical characteristics Type: Single-seat night fighter Entry into service: 1917 Length: 8.97 m Wingspan: 10.97 m Height: 3.18 m Empty weight: 558 kg Maximum takeoff weight: 839 kg Engine and performance Engine: rotary Le Rhône 110 hp or Clerget 130 hp Power: 110-130 hp Maximum speed: 155 km/h Autonomy: 400 km Operating tangency: 4,200 m Climbing speed: 3,000 m in 13 minutes Modification to the airframe of theAvro 504K allowed for better control during night flight, with instruments better suited for after-dark missions. Armament 2 Lewis 7.7 mm machine guns, mounted above the upper wing Unlike conventional fighters, the Avro 504K "Comic" had the machine guns decoupled from the propeller and installed above the upper wing to avoid synchronization problems and improve aiming at slower targets such as bombers. Operational role and use Night interceptor: Designed to shoot down Zeppelin and Gotha bombers during raids over London and the UK. Air defense: Used mainly by No. 77 and No. 151 Squadron of the RAF. Advanced trainer: Some examples remained in service as training aircraft. Historical impact and famous aces The Avro 504K "Comic" was a temporary but effective solution to counter German bombers. Despite its modest performance, its agility and innovative armament placement made it a suitable interceptor for night operations. It was replaced in 1918 by more advanced fighters such as the Sopwith Camel "Comic" and the Sopwith Snipe. Conclusion TheAvro 504K "Comic" represented one of the first British night fighter experiments, contributing to the defense of British cities from German raids. Although derived from a training aircraft, it proved effective until the arrival of more modern and specialized aircraft.
Prague E-114 ''Air Baby'' airplane kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Praga E-114 "Air Baby" was a two-seat light touring aircraft designed and built in Czechoslovakia in the 1930s by the Praga Aircraft Company. Known for its light weight and economy in fuel consumption, it was used mainly for training, tourism, and air competitions. Due to its reliability and low operating costs, the Praga E-114 became one of the most popular light aircraft in Europe at the time, also finding use in some countries outside Czechoslovakia. Technical characteristics Type: light touring aircraft Crew: 1 pilot + 1 passenger Length: 6.8 m Wingspan: 11 m Height: 1.85 m Empty weight: 280 kg Maximum take-off weight: 470 kg Engine and performance Engine: Prague B engine(2 opposed cylinders, air-cooled) Power: 28 hp (basic version) Later versions with engines from 40 to 65 hp Maximum speed: 135 km/h Cruising speed: 110 km/h Autonomy: 480 km Maximum tangency: 3,800 m Takeoff and landing: Extremely short and versatile, suitable for small airfields Design and special features Wooden frame with canvas covering, which made it very light. Foldable wings, allowing easy storage even in small spaces. Easy to fly, ideal for flight schools and private pilots. Economicalin fuel consumption, with great efficiency for the time. Operational role and employment Civilian use: Air tourism Pilot training Aviation competitions Military use (limited): Some specimens requisitioned during World War II for transportation and reconnaissance. Its simple construction and low cost made it an affordable aircraft for private pilots and aeroclubs throughout Europe. Historical impact The Praga E-114 was one of the first mass-produced European light aircraft, anticipating the concept of modern ultralights. It was exported to the United Kingdom under the name Hillson Praga. After World War II, some examples continued to fly until the 1950s. Conclusion The Prague E-114 "Air Baby" is an example of an economical and efficient touring aircraft, prized for its ease of piloting and low operating costs. Although it was not a revolutionary aircraft, it played an important role in the spread of private flying in Europe in the 1930s and 1940s.
Focke Wulf Fw 190A-2 aircraft kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Focke-Wulf Fw 190A-2 was the first large-scale operational variant of the famous German Fw 190 fighter, developed by Focke-Wulf Flugzeugbau AG during World War II. After tests on pre-series versions(Fw 190A-0) and the first limited production models(Fw 190A-1), the A-2 variant introduced significant improvements, including a more reliable engine and enhanced armament. It entered Luftwaffe service in 1941, proving superior to the British Spitfire Mk V in aerial combat. Technical characteristics Type: Single-engine, propeller-driven fighter Entry into service: Late 1941 - early 1942 Length: 8.84 m Wingspan: 10.51 m Height: 3.95 m Empty weight: 3,200 kg Maximum takeoff weight: 4,250 kg Engine and performance Engine: BMW 801C-2 (14-cylinder air-cooled radial) Power: 1,600 hp Top speed: 610 km/h at 6,000 m Range: 800 km (up to 1,300 km with auxiliary tank) Operating tangency: 10,400 m Climbing speed: 900 m/min The BMW 801C-2 engine offered greater reliability than the previous BMW 139, improving the fighter's operational life. Armament The Fw 190A-2 was well armed for its time: 2 MG 17 7.92 mm machine guns above the engine (450 rounds each) 2 MG 151/20 20 mm cannons mounted in the wings (250 rounds each) 2 MG FF 20-mm machine guns in the wingtips (60 rounds each) This combination provided great firepower, making it effective against both enemy fighters and heavily armored bombers. Operational role and use Air superiority fighter: The Fw 190A-2 achieved success against the RAF's Mk V Spitfires, proving faster and better armed at medium altitude. Interceptor: Used to counter Allied bombers and protect strategic targets. Ground attack: Some examples were equipped with light bombs for attack missions. Luftwaffe defense: It participated in numerous battles on the Western Front, especially in France and in the skies over the English Channel. Historical impact First real opponent of the Spitfire Mk V, which dominated European skies until then. Basis for later versions of the Fw 190, which continued to improve in power and armament. Decisive contribution to the Luftwaffe in 1942, before the Allies introduced more advanced fighters such as the Spitfire Mk IX and P-51 Mustang. Conclusion The Fw 190A-2 marked the beginning of Focke-Wulf supremacy in European skies. With its powerful engine, superior armament and robustness, it proved to be one of the best German fighters of the first phase of the war. Its superiority forced the RAF to quickly develop new versions of the Spitfire to compete.
Focke Wulf Fw 190A-0 aircraft kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Focke-Wulf Fw 190A-0 was the first pre-series version of the famous German Fw 190 fighter, developed by Focke-Wulf Flugzeugbau AG in the late 1930s and tested in the early 1940s. This variant was intended for operational evaluation before mass production and served as the basis for later versions of the Fw 190A series, which became one of the Luftwaffe's best fighters in World War II. Technical characteristics Type: Single-engine, propeller-driven fighter First flight: June 1, 1939 Entry into service: 1940 (operational tests) Length: 8.84 m Wingspan: 10.51 m Height: 3.95 m Empty weight: 2,980 kg Maximum takeoff weight: 3,950 kg Engine and performance Engine: BMW 139 (14-cylinder air-cooled radial) Power: 1,550 hp Top speed: 595 km/h Autonomy: 850 km Operational tangency: 10,000 m Climbing speed: 900 m/min The BMW 139 engine was soon replaced in later versions with the more reliable and powerful BMW 801. Armament (pre-series with variations between models) 2 MG 17 7.92 mm machine guns (mounted above the engine) 2 MG 17 7.92 mm machine guns (mounted in the wings, later replaced by cannons in later versions) The armament of the Fw 190A-0 was less powerful than later operational models, which integrated 20-mm cannons to improve offensive capability. Operational role Test and evaluation: The Fw 190A-0 was assigned to Luftwaffe experimental units to test performance under real-world conditions. Development of later versions: It served as the basis for the Fw 190A-1, which went into production and fought starting in 1941. Comparison with the Bf 109: The aircraft was designed as an alternative and complement to the Messerschmitt Bf 109, with a more robust radial engine and greater ability to absorb damage in combat. Historical impact Starting point of the Fw 190A series: The design proved promising and led to the mass production of the Fw 190A-1 and subsequent versions, which became key to the Luftwaffe. Overcoming technical problems: The BMW 139 engine proved problematic, leading to the choice of the BMW 801 in production versions. Contribution to the evolution of German fighters: Robust design and high performance made the Fw 190 an excellent fighter in air superiority, interception and ground attack roles. Conclusion The Fw 190A-0 was a crucial phase in the development of one of the best German fighters of World War II. Although limited to experimentation, testing enabled the design to be refined and the Fw 190A-1, which became a mainstay of the Luftwaffe, to mass production.
DSF Kranich II aircraft kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The DFS Kranich II was an advanced training and performance glider designed and built in Germany in the 1930s by the Deutsche Forschungsanstalt für Segelflug (DFS), the German Institute for Gliding Research. This model was an evolution of the DFS Kranich I, improved to offer better aerodynamic performance. It was widely used in gliding schools, competitions and, during World War II, as a trainer for military transport glider pilots. Technical Characteristics. Type: two-seat, high-performance glider Crew: 2 people (instructor and student or pilot and passenger) Length: 8.36 m Wingspan: 17 m Empty weight: 265 kg Maximum takeoff weight: 400 kg Glide ratio: about 25:1 Flight speed: Maximum: 170 km/h Minimum: 50 km/h Design and special features Wooden frame with canvas covering, typical of gliders of the period. High cantilevered wing, without external struts, to reduce aerodynamic drag. Retractable undercarriage, to improve aerodynamics during flight. Excellent soaring capabilities, allowing long duration flights by taking advantage of updrafts. Operational role and use Gliding school: Used to train glider pilots, both civilian and military. Gliding competitions: Due to its performance, the Kranich II participated in several aviation competitions in the 1930s and 1940s. Military use (World War II): Employed by the Luftwaffe for training pilots of transport gliders such as the DFS 230, used in airborne operations. Historical impact One of the most popular and widespread two-seater gliders before and during World War II. Used to train an entire generation of glider pilots for both sport and military purposes. After the war, many examples were rebuilt and used in flight schools in different countries. Conclusion The DFS Kranich II was an advanced glider for its time, prized for its handling and performance. Its historical importance is related to both the development of gliding in Germany and its use in Luftwaffe pilot training.
Sopwith Swallow aircraft kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Sopwith Swallow was a prototype single-seat fighter plane developed in the United Kingdom during World War I by the Sopwith Aviation Company. It was designed as an evolution of the famous Sopwith fighters, particularly the Sopwith Camel, with the aim of testing new aerodynamic configurations and improving performance. Key features Design: Monoplane, an unusual configuration for the era when biplanes dominated military aircraft design. Cantilever (cantilever) wings, with no struts or tie-rods, an innovative feature for the time. Fuselage derived from the Sopwith Camel, with a compact, aerodynamic profile. Engine: Equipped with a Clerget 9B rotary engine, capable of generating about 130 hp, the same engine used by the Sopwith Camel. Performance: Top speed: About 200 km/h. Operating radius and altitude similar to the Sopwith Camel, but never fully documented due to the experimental nature of the design. Armament: Equipped with a synchronized Vickers machine gun mounted on the muzzle. Purpose and use The Sopwith Swallow was conceived to explore the advantages of a monoplane design over traditional biplanes. The idea was to reduce weight and drag to improve performance in terms of speed and maneuverability. However: It never passed the experimental stage. The monoplane configuration of the time was considered too fragile compared to sturdy biplanes, and the design was scrapped. The technology available at the time was not yet mature to fully support the benefits of the monoplane design. Legacy Although the Sopwith Swallow did not have a direct impact on the conflict, it represented an important step in aviation development, contributing to the understanding of monoplane configurations. The design influenced designers' thinking for the postwar period, when monoplanes became the standard for military and civil aviation. Today the Sopwith Swallow is remembered as an interesting experiment and a precursor to future technological developments in aviation.
P-51D-5 Mustang "Aces" airplane kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The P-51D-5 Mustang "Aces" is a variant of the famous North American P-51 Mustang fighter aircraft, widely used during World War II and the Korean War. The term "Aces" refers to the pilots who, flying this model, achieved "ace" status, that is, they shot down at least five enemy aircraft in combat. Key features of the P-51D-5 Design: Low-wing monoplane with all-metal structure. The cockpit of the P-51D-5 featured a teardrop dome ("bubble canopy"), which significantly improved visibility compared to previous versions. The plane had clean aerodynamic lines designed to optimize speed and maneuverability. Engine: Equipped with a Rolls-Royce Merlin V-1650-7 engine, manufactured under license in the United States by Packard, capable of developing about 1,490 hp. This engine provided outstanding performance, especially at high altitudes. Performance: Top speed: About 700 km/h. Operating radius: About 1,650 km with internal tanks, extendable with additional tanks. Maximum altitude: Up to 12,800 meters. Armament: Six Browning M2 12.7-mm machine guns mounted in the wings. Ability to carry bombs (up to 450 kg total) or rockets for tactical support missions. Operational role Air superiority fighter: Used to dominate the skies, shooting down enemy aircraft in air combat. Bomber escort: Due to its long range, the P-51D was one of the few fighters capable of accompanying Allied bombers during missions deep into enemy territory. Ground attack: Equipped with bomb and rocket capabilities, the Mustang was also used for attacks against ground targets. The P-51D-5 and the "Aces" This variant of the Mustang was one of the most produced and used during the war. Many of the American and Allied pilots who achieved "ace" status did so at the controls of a P-51D. Its main opponents were German fighters such as the Messerschmitt Bf 109 and the Focke-Wulf Fw 190, against which the Mustang proved more than equal to the task. Legacy The P-51D-5 Mustang is now considered one of the best piston fighters ever built, thanks to its balance of speed, maneuverability, firepower and range. It remained in operational service in some air forces until the 1960s and is still highly valued by aviation enthusiasts. Many surviving examples are preserved in museums or used for demonstration flights and air races. The P-51D is a symbol of Allied aviation during World War II and a testament to the technological innovation of the time.
US X-3 "Stiletto" experimental aircraft kit + Paint Mask and 3D Details in 1/72 scale - Model KOVOZAVODY PROSTEJOV. TheX-3 "Stiletto" is a U.S. experimental aircraft developed by the Douglas Aircraft Company in the 1950s to study flight at high supersonic speeds. Featuring a sleek, streamlined design with short, thin wings, the X-3 aimed to explore the aerodynamic and structural issues of flight at extreme speeds. Although it did not achieve all its goals, it provided crucial data for the development of future supersonic aircraft. Key features Design: Long, thin fuselage that resembled a "stiletto" (hence the name). Extremely short and thin wings designed to reduce drag at supersonic speeds. Retractable, sturdy landing gear to handle stresses on the ground. Engines: Equipped with two Westinghouse J34-WE-17 turbojets. The engines were not powerful enough, limiting the aircraft's performance compared to the initial designs. Performance: Top speed: Approximately 1,050 km/h (well below the expected Mach 2). Operational altitude: Up to about 11,000 meters. Limitations due to low engine thrust and aircraft weight. Role and use Main purpose: The X-3 was designed to collect data on aerodynamics, structural materials, and the behavior of an aircraft at high speeds and under sustained supersonic flight conditions. Tests and results: Made its first flight on October 20, 1952. It failed to achieve supersonic speeds in level flight due to engine and design limitations. However, it was extremely useful in the study of thin and short wings, influencing later designs such as the Lockheed F-104 Starfighter. Legacy Although the Douglas X-3 "Stiletto" was not as successful as hoped as an experimental aircraft, the data collected during testing contributed significantly to our understanding of the challenges of supersonic flight. The innovative design and short wings became the basis for many supersonic fighters developed in later years. The only example built is currently on display at the National Museum of the United States Air Force in Dayton, Ohio. In summary, the X-3 represents an important milestone in the history of experimental aviation, despite its technical limitations.
Pilatus PC-9M aircraft kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Pilatus PC-9M is an advanced variant of the Pilatus PC-9 military training aircraft, produced by the Swiss company Pilatus Aircraft. This aircraft is designed for training military pilots in both basic and advanced stages and is valued for its reliability, maneuverability and versatility. Key features Role: Training and light support aircraft. Crew: Two people (instructor and student, in tandem configuration). Engine: 950-shp Pratt & Whitney Canada PT6A-62 turbopropeller. Top speed: Approximately 593 km/h. Autonomy: Up to 1,300 km. Maximum operational altitude: Approximately 11,580 meters. Distinctive features of the PC-9M The PC-9M version features significant improvements over the original model, including: Updated avionics: More advanced navigation and communication systems compatible with modern standards. Ergonomic cockpit: Designed to simulate fighter jet flight environments. Improved performance: Reinforced structure for increased operational loads and ability to withstand a wide range of maneuvers. Operational flexibility: Configurable for carrying light weapons or surveillance pods, usable for light attack roles. Use The Pilatus PC-9M is used by numerous air forces around the world to train pilots destined for more complex fighters and aircraft. User countries include: Switzerland: (Original manufacturer and operator). Slovenia, Croatia, Australia, and other countries that require reliable trainers for their military programs. Differences from other trainers The PC-9M is known for its balance between high performance and low operating cost. Despite the introduction of jet trainers such as the Pilatus PC-21, the PC-9M remains a viable choice for many air forces because of its ability to prepare pilots for real-world operational environments without the economic burden of an advanced jet.
Pilatus PC-9 Part.2 aircraft kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Pilatus PC-9 is an advanced military training aircraft designed and manufactured by the Swiss company Pilatus Aircraft. This aircraft, developed in the 1980s, was designed to provide comprehensive training for military pilots, including both basic and advanced training phases. Key features Role: Light training and support aircraft. Crew: Two people in tandem configuration (instructor and student). Engine: Pratt & Whitney Canada PT6A-62 turbopropeller of about 950 shp. Top speed: Approximately 593 km/h. Autonomy: Up to 1,300 km. Maximum operational altitude: 11,580 meters. Design and configuration The Pilatus PC-9 has a robust and aerodynamic structure that enables it to operate in demanding conditions. Some highlights include: Modern cockpit: Equipped with advanced instrumentation to simulate the flight environment of a fighter jet, enabling realistic training. Ejection system: Includes ejection seats to ensure crew safety. Maneuverability: Can withstand loads from -3g to +7g, making it suitable for advanced maneuvering. Usage The Pilatus PC-9 has been adopted by many air forces worldwide as the primary platform for training pilots destined for more complex fighters and aircraft. Major users include: Australia Ireland Slovenia Croatia Saudi Arabia Variants PC-9/A: Version for the Royal Australian Air Force (RAAF). PC-9M: Updated variant with modern avionics and reinforced structure for improved performance and operational flexibility. Beechcraft T-6 Texan II: Based on the PC-9 design, produced in the United States with significant modifications. Strengths. Cost-effectiveness: Operating a PC-9 is significantly less expensive than operating a trainer jet. Versatility: Suitable for both basic and advanced training, and in some cases used for light support roles. Reliability: The combination of Pratt & Whitney engine and Swiss design ensures high performance and easy maintenance. The PC-9 has been replaced in some countries by the more advanced Pilatus PC-21, but it remains in service in many air forces because of its effectiveness as a training platform.
Pilatus PC-9 aircraft kit in 1/72 scale - KOVOZAVODY PROSTEJOV model. The Pilatus PC-9 is an advanced military training aircraft designed and manufactured by the Swiss company Pilatus Aircraft. This aircraft, developed in the 1980s, was designed to provide comprehensive training for military pilots, including both basic and advanced training phases. Key features Role: Light training and support aircraft. Crew: Two people in tandem configuration (instructor and student). Engine: Pratt & Whitney Canada PT6A-62 turbopropeller of about 950 shp. Top speed: Approximately 593 km/h. Autonomy: Up to 1,300 km. Maximum operational altitude: 11,580 meters. Design and configuration The Pilatus PC-9 has a robust and aerodynamic structure that enables it to operate in demanding conditions. Some highlights include: Modern cockpit: Equipped with advanced instrumentation to simulate the flight environment of a fighter jet, enabling realistic training. Ejection system: Includes ejection seats to ensure crew safety. Maneuverability: Can withstand loads from -3g to +7g, making it suitable for advanced maneuvering. Usage The Pilatus PC-9 has been adopted by many air forces worldwide as the primary platform for training pilots destined for more complex fighters and aircraft. Major users include: Australia Ireland Slovenia Croatia Saudi Arabia Variants PC-9/A: Version for the Royal Australian Air Force (RAAF). PC-9M: Updated variant with modern avionics and reinforced structure for improved performance and operational flexibility. Beechcraft T-6 Texan II: Based on the PC-9 design, produced in the United States with significant modifications. Strengths. Cost-effectiveness: Operating a PC-9 is significantly less expensive than operating a trainer jet. Versatility: Suitable for both basic and advanced training, and in some cases used for light support roles. Reliability: The combination of Pratt & Whitney engine and Swiss design ensures high performance and easy maintenance. The PC-9 has been replaced in some countries by the more advanced Pilatus PC-21, but it remains in service in many air forces because of its effectiveness as a training platform.
Messerschmitt Bf 108 "Taifun" airplane kit in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Messerschmitt Bf 108 is a single-engine light touring and liaison aircraft developed by the German company Bayerische Flugzeugwerke, better known as Messerschmitt. Designed in the 1930s, the Bf 108 became a versatile and innovative aircraft for its time, used in both civilian and military applications. Key features Role: Touring, light transport and liaison aircraft. Crew: 1-2 people (pilot and passenger) with the possibility of carrying up to 4 occupants. Engine: Argus As 10C piston engine, an air-cooled V8 of about 240 hp. Top speed: Approximately 190 mph (305 km/h). Autonomy: Up to 1,000 km. Structure: Low-wing monoplane with retractable undercarriage. Development and use. The Bf 108 was initially designed as a sport aircraft for competition and advanced tourism. It made its debut in 1934 during the Challenge International de Tourisme, an international air competition, where it stood out for its speed and modern design. Later, the aircraft was also adapted for military use, notably as: Liaison aircraft for officers and personnel during World War II. Pilottrainer. Distinctive features Technological innovations: For its time, the Bf 108 was extremely advanced, with features such as retractable undercarriage and an aerodynamic metal fuselage. Performance: High speed and maneuverability made it suitable for long distances and landings in tight spaces. Reliability: It was appreciated for its robustness and ease of maintenance. Variants Bf 108 A: The early version, produced in a small number and used for air competitions. Bf 108 B: The main version, with aerodynamic improvements and a more powerful engine. Nord 1000 Pingouin: A version produced under license in France after the war. Historical use The Bf 108 was used by the Luftwaffe as a liaison aircraft during World War II and by numerous civilian and military customers worldwide. After the conflict, some variants were built under license in France and remained in use for decades. Trivia The design of the Bf 108 influenced the development of the later Messerschmitt Bf 109, one of the most famous fighters of World War II. It is also known by the nickname "Taifun" (Typhoon), given by the famous German pilot Elly Beinhorn, who used it in numerous record flights. The Messerschmitt Bf 108 remains an aviation icon of the 1930s because of its innovative design and versatility.
Russian Ilyushin Il-10/B-33 "Beast" attack aircraft kit + Paint Mask and 3D Details in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Ilyushin Il-10, also known as the B-33 in its variant produced under license in Czechoslovakia, is a Soviet-originated ground attack aircraft designed by Sergei Vladimirovic Il'jušin during World War II. This aircraft was developed as a successor to the Ilyushin Il-2 Sturmovik, famous for its role in supporting ground troops on the Eastern Front. Key features Role: Ground attack aircraft. Crew: Two people (pilot and rear gunner). Engine: A Mikulin AM-42 piston engine. Maximum speed: Approximately 550 km/h. Armament: 23-mm ShVAK or VYa-23 cannons mounted in the wings. Rear machine guns for defense (usually a 12.7-mm UBT). Bomb and rocket carrying capability for attacks against ground targets. Operational history Introduction: Introduced toward the end of World War II, it entered service in 1944. Wartime use: It participated in the last skirmishes of the war and the Korean War (1950-1953) where it was employed by North Korean forces. Variants: The B-33 was the version built under license in Czechoslovakia with some minor modifications. Production About 6,000 were produced, including those built in Czechoslovakia. It was in service in various Warsaw Pact countries and other nations allied with the Soviet Union. This aircraft was prized for its ruggedness and offensive capability, but with the evolution of jet aircraft, it was phased out in the 1950s.
Russian Avia B-33/Il-10 "Beast" attack aircraft kit + Paint Mask and 3D Details in 1/72 scale - Model KOVOZAVODY PROSTEJOV. TheAvia B-33/Il-10 "Beast" is a license-produced version of the famous Soviet Ilyushin Il-10 attack aircraft, built in Czechoslovakia by Avia after World War II. The Il-10 itself was the direct successor to the iconic Ilyushin Il-2 "Sturmovik," earning the nickname "Beast" for its power and endurance on the battlefield. Key features Design: Single or two-seater monoplane with all-metal structure. Heavy armor around cabin and vital components, designed to resist anti-aircraft fire. Equipped with medium-low configuration wings for greater stability during low-level flight. Engine: Equipped with a Mikulin AM-42 radial engine, about 2,000 hp, which provided good speed and load capacity. Performance: Top speed: About 550 km/h. Operating radius: 800 km, optimal for close support missions. Warload capability: Bombs, rockets and heavy machine guns. Armament: Cannons: Two 23-mm automatic cannons in the wings. Machine guns: One rear machine gun for the defensive gunner. Munitions: Light bombs and air-to-ground rockets for attacks against ground targets. Operational role Designed as a ground attack aircraft, the Il-10 and its variant Avia B-33 were used to support ground troops with attacks against enemy tanks, vehicles and infantry. The Avia B-33 was produced in large quantities in Czechoslovakia starting in 1951 to equip the national air force and some allied countries of the Soviet bloc. Wartime employment: Participated in numerous local and regional conflicts during the Cold War. Its robustness and ability to survive enemy fire made it an aircraft feared by its adversaries. Legacy TheAvia B-33/Il-10 "Beast" is considered one of the last great piston attack aircraft before the advent of jets. It was a symbol of air power for many Eastern Bloc armed forces until the 1960s, when it began to be replaced by more modern jets. Its combination of firepower, protection and low-flying capability made it a worthy successor to the Il-2 "Sturmovik." Today, some surviving examples are displayed in aviation museums, where they continue to tell the story of the transition between the piston and jet aircraft eras.
Martin Baker MB5 "British Prototype" 1944 British fighter jet Martin Baker Prototype kit + Paint Mask and 3D Details in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Martin-Baker MB5 was a British fighter prototype developed during World War II by the Martin-Baker Aircraft Company in 1944. Although it never went into production, it is considered one of the most advanced and promising fighter designs of its time, combining excellent performance, innovative engineering and a design that would rival the best aircraft of the time. Key features Structure: All-metal monoplane with clean lines and a modular design that facilitated maintenance and repairs. Cockpit: Spacious and well-organized cabin with exceptional visibility due to the bubble dome. Engine: Equipped with a Rolls-Royce Griffon 83 engine, a liquid-cooled V12 with about 2,340 hp, coupled with a five-blade counter-rotating Rotol propeller. Performance: Top speed: Over 700 km/h, making it competitive with the most advanced piston fighters of the time. Range: About 1,600 km, suitable for medium-range missions. Excellent climb rate and maneuverability due to powerful engine and aerodynamic configuration. Armament: Designed to carry four 20 mm Hispano guns mounted in the wings, offering devastating firepower. Innovative design The Martin-Baker MB5 was distinguished by its modular design, which allowed for faster maintenance than other fighters of the time. The cockpit configuration was ergonomic, offering pilots intuitive instrument control, a significant change from previous aircraft. Role and use The MB5 was intended as a multi-role fighter for the Royal Air Force (RAF), with both interception and ground attack capabilities. However, it was never officially adopted for several reasons: Development late in the war (1944) meant that jets were rapidly becoming the priority for the air force. Production of proven fighters such as the Supermarine Spitfire and Hawker Tempest was already in full swing. The emergence of jet aircraft, such as the Gloster Meteor, made piston-powered fighters obsolete. Legacy Despite its potential, the Martin-Baker MB5 remained a prototype and was never mass-produced. However, the design contributed to the prestige of the Martin-Baker Aircraft Company, which later specialized in the design and production of ejection systems for military aircraft, an area in which the company still leads the world. The MB5 is remembered as one of the best piston fighters ever built, a symbol of British aviation innovation and capability in World War II.
Dutch Fokker C.X "Pegasus engine" reconnaissance aircraft kit + Paint Mask and 3D Details in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Fokker C.X "Pegasus engine" is a variant of the Fokker C.X reconnaissance and light bombing biplane, equipped with a Bristol Pegasus engine, a 9-cylinder air-cooled radial. This model was an alternative solution to the Rolls-Royce Kestrel engine version, offering a different balance of performance, reliability, and ease of maintenance. Key features Design: The Fokker C.X is a classic biplane with wood and metal construction, canvas-covered wings and an open cockpit for two crew members (pilot and gunner/observer). Engine: The Bristol Pegasus delivered between 600 and 700 hp (depending on version), offering a combination of ruggedness and ease of operation. Top speed: About 300-320 km/h, slightly lower than the Kestrel-engined variant. Range: Up to about 1,000 km, making it suitable for medium-range missions. Armament: Machine guns: One or two fixed ones in front and one brandishing one for the observer. Carrying capacity: Light bombs for tactical bombing missions. Operational role. Reconnaissance and bombing: Employed for tactical observations and light strikes against ground targets. International use: In the Netherlands, it was mainly used for patrol and training tasks. In Finland, it played a significant role during the Winter War (1939-1940), due to its ability to operate in difficult conditions and on improvised tracks. It was also employed in other countries, including Spain during the Spanish Civil War. Legacy Although the Fokker C.X "Pegasus engine" was obsolete in the face of modern monoplanes of the 1940s, it remained in service because of its versatility and robustness. It is now considered an example of the transition between traditional biplanes and modern combat aircraft. Some examples have been restored for museums and historical exhibitions.
Dutch Fokker C.X "Kestrel engine" reconnaissance airplane kit + Paint Mask and 3D Details in 1/72 scale - Model KOVOZAVODY PROSTEJOV. The Fokker C.X "Kestrel engine" is a biplane reconnaissance and light bombing aircraft designed by the Dutch Fokker company in the 1930s. It is a variant of the basic Fokker C.X model, equipped with a high-performance Rolls-Royce Kestrel engine, which made it more powerful than other versions equipped with less advanced engines. Key features Design: Traditional biplane with mixed wood and metal structure, with canvas-covered surfaces. Engine: The Kestrel, a liquid-cooled V12 engine, provided about 600-700 hp (depending on version), ensuring better performance than radial engines used in other configurations. Top speed: About 330 km/h (330 mph), higher than the average biplane reconnaissance aircraft of the time. Crew: Two members, one pilot and one observer/miter. Armament: Generally equipped with one or two fixed machine guns for the pilot and one wieldable machine gun for the observer, plus a load of light bombs. Operational Role. Designed primarily as a reconnaissance and light bomber aircraft. Used by the air forces of countries such as the Netherlands, Finland and Spain (during the Spanish Civil War). In Finland, the Fokker C.X was particularly effective during the Winter War (1939-1940) against the Soviet Union due to its reliability and ability to operate from improvised runways. Legacy Despite being surpassed by the emerging monoplane aircraft of the 1940s, the Fokker C.X "Kestrel engine" proved robust and versatile, earning a good reputation in combat. Today it is remembered as one of the last biplanes effectively employed in an operational military role.
Kit aereo Supermarine Spitfire HF Mk.VII 'Grey Camo' in scala 1/72 - Modello Kovozávody Prostejov. Il Supermarine Spitfire HF Mk.VII 'Grey Camo' è una variante del celebre caccia britannico Spitfire HF Mk.VII, caratterizzata da una mimetica grigia pensata per operazioni ad alta quota. Questa livrea particolare era progettata per ridurre la visibilità dell'aereo rispetto al cielo, migliorando la sua capacità di passare inosservato durante missioni di intercettazione e ricognizione ad alta quota. Caratteristiche principali del modello 'Grey Camo' Livrea grigia: Il camuffamento grigio era composto da diverse tonalità, come il Medium Sea Grey e il Ocean Grey, per armonizzarsi con il cielo e ridurre il contrasto con l'ambiente circostante. Questo schema di mimetizzazione era comune per aerei operanti in Europa occidentale, dove la minaccia di intercettazione visiva ad alta quota era elevata. Motore e prestazioni: Equipaggiato con il motore Rolls-Royce Merlin 71, ottimizzato per quote elevate. Velocità massima: 660 km/h a circa 12.000 metri. Tetto operativo: fino a 13.100 metri. Cabina pressurizzata: Una delle prime varianti dello Spitfire con una cabina pressurizzata, permettendo missioni più lunghe e sicure a grandi altitudini. Armamento: 2 cannoni Hispano Mk.II da 20 mm. 4 mitragliatrici Browning da 7,7 mm, montate nelle ali. Ruolo operativo Intercettazione ad alta quota: Destinato a combattere contro bombardieri nemici e velivoli da ricognizione tedeschi, come il Junkers Ju 86P. Ricognizione: La mimetica grigia era particolarmente utile per missioni di ricognizione dove l'invisibilità era essenziale. Scorta ad alta quota: Scortava i bombardieri alleati, proteggendoli dagli attacchi di caccia nemici. Contesto storico Il 'Grey Camo' riflette l'adattamento dell'aviazione britannica alle esigenze della guerra aerea, in particolare sopra l'Europa occidentale, dove l'intercettazione di bombardieri e ricognitori ad alta quota era essenziale. Prodotto in numero limitato, il Mk.VII con livrea grigia era parte della strategia della RAF per ottenere la supremazia ad alta quota. Il Supermarine Spitfire HF Mk.VII 'Grey Camo' dimostra la versatilità del design dello Spitfire, adattato per soddisfare le sfide specifiche del teatro operativo della Seconda Guerra Mondiale. La sua combinazione di prestazioni avanzate e mimetizzazione lo rese uno strumento efficace nel repertorio alleato.
Kit aereo Supermarine Spitfire HF Mk.VII in scala 1/72 - Modello Kovozávody Prostejov. Il Supermarine Spitfire HF Mk.VII è una variante specializzata del celebre caccia britannico Spitfire, sviluppato durante la Seconda Guerra Mondiale per operazioni ad alta quota. La sigla HF sta per High Flying (alta quota), indicando il suo adattamento specifico per combattere a grandi altitudini, spesso contro bombardieri nemici e caccia di scorta. Caratteristiche principali Motore: Equipaggiato con il motore Rolls-Royce Merlin 71, ottimizzato per operazioni ad alta quota grazie a un sistema di compressore migliorato. Potenza: circa 1.710 cavalli. Ala: Dotato della configurazione ad ala "corta" di tipo C per un migliore equilibrio tra velocità e manovrabilità. Cabina pressurizzata: Il Mk.VII fu uno dei primi Spitfire a essere equipaggiato con una cabina pressurizzata, essenziale per missioni a quote elevate (oltre 10.000 metri). Questo miglioramento garantiva un maggiore comfort e sicurezza per il pilota, riducendo gli effetti negativi dell'ipossia. Prestazioni: Velocità massima: 660 km/h a circa 12.000 metri. Autonomia: circa 1.700 km con serbatoi aggiuntivi. Tetto di servizio: 13.100 metri, che lo rendeva uno dei caccia alleati più capaci ad alta quota. Armamento: Configurazione standard: 2 cannoni Hispano Mk.II da 20 mm, montati sulle ali. 4 mitragliatrici Browning da 7,7 mm, montate nelle ali. Caratteristiche strutturali: Fuseliera rinforzata per gestire le pressioni a quote elevate. Prua più lunga rispetto ad altre varianti per accogliere i nuovi sistemi di compressione del motore. Ruolo operativo Missioni ad alta quota: Progettato per intercettare bombardieri nemici, in particolare i Junkers Ju 86P tedeschi, che operavano a quote molto elevate. Utilizzato per contrastare incursioni di ricognitori nemici ad alta quota. Scorta a lunga distanza: Grazie alla sua autonomia migliorata, era impiegato anche per missioni di scorta a bombardieri alleati. Riconoscimento tattico: Alcuni esemplari furono adattati per missioni di ricognizione ad alta quota, grazie alle sue eccellenti prestazioni in aria rarefatta. Produzione e impiego Prodotto in numero relativamente limitato rispetto ad altre varianti del Spitfire, il Mk.VII era riservato a compiti specializzati. Entrò in servizio operativo a partire dal 1943, utilizzato principalmente dalla Royal Air Force (RAF). Operò in Europa e nel Mediterraneo, dove la necessità di intercettori ad alta quota era più sentita. Importanza storica Il Spitfire HF Mk.VII rappresenta un passo significativo nell'evoluzione dei caccia della Seconda Guerra Mondiale, mostrando come la tecnologia e il design aeronautico britannico sapessero rispondere rapidamente alle sfide operative del conflitto. Pur non essendo prodotto in grandi quantità, fu un aereo cruciale nelle operazioni ad alta quota e dimostrò la versatilità del progetto di base dello Spitfire.
Kit aereo Grumman J4F-2/OA-14 'Widgeon' in scala 1/72 - Modello Kovozávody Prostejov. Il Grumman J4F-2/OA-14 "Widgeon" è una variante dell'idrovolante anfibio Grumman Widgeon, progettato per scopi militari e civili negli anni '40. Sviluppato come versione migliorata del J4F-1, il J4F-2 e la sua designazione nell'aviazione dell'esercito statunitense, OA-14, furono impiegati principalmente per missioni di pattugliamento costiero, ricerca e soccorso, e trasporto leggero durante la Seconda Guerra Mondiale. Caratteristiche principali Ruolo: Pattugliamento marittimo. Operazioni di ricerca e salvataggio (SAR). Trasporto leggero. Struttura: Idrovolante anfibio bimotore con carrello retrattile per operazioni su terra e acqua. Ali alte con galleggianti alle estremità per la stabilità durante il decollo e l'atterraggio in acqua. Dimensioni: Lunghezza: 9,47 metri. Apertura alare: 11,8 metri. Altezza: 3,7 metri. Motori: Due motori radiali Ranger L-440-5 a 6 cilindri raffreddati ad aria, con una potenza di circa 200 cavalli ciascuno. Velocità massima: circa 255 km/h. Autonomia: circa 1.400 km. Equipaggio e carico: Equipaggio: 2 piloti. Capacità: fino a 3 passeggeri o carico leggero. Armamento: Una mitragliatrice calibro .30 (7,62 mm), tipicamente montata in una postazione ventrale. Poteva trasportare cariche di profondità o bombe leggere per missioni antisommergibile. Impiego operativo J4F-2 (U.S. Navy e U.S. Coast Guard): Utilizzato prevalentemente dalla U.S. Navy e dalla Guardia Costiera degli Stati Uniti per missioni costiere di pattugliamento e SAR. In alcune operazioni, fu usato per identificare e attaccare sottomarini nemici. Un J4F-2 è noto per aver affondato un sottomarino tedesco, l'U-166, nel Golfo del Messico nel luglio 1942. OA-14 (U.S. Army Air Forces): La designazione OA-14 fu usata dall'esercito americano per missioni di salvataggio aereo e marittimo, nonché per il trasporto di personale e materiali in aree remote. Forze Alleate: Vari esemplari furono utilizzati da altre forze alleate, tra cui il Canada, la Gran Bretagna, e l'Australia, in ruoli simili. Impiego civile e postbellico Dopo la guerra, il J4F-2/OA-14 fu adattato per uso civile. Divenne popolare per il trasporto privato e commerciale, specialmente in aree costiere o isole remote. Grazie alla sua versatilità anfibia, venne utilizzato per turismo, pesca sportiva e trasporto merci leggere. Importanza storica Il Grumman J4F-2/OA-14 "Widgeon" è un esempio di velivolo anfibio versatile, capace di svolgere una varietà di ruoli in guerra e pace. Sebbene non avesse la potenza e l'armamento di altri aerei militari dell'epoca, eccelleva in operazioni di supporto, rendendolo una risorsa indispensabile per le forze armate e per gli operatori civili dopo il conflitto.
Kit aereo Grumman J4F-1 'Widgeon' in scala 1/72 - Modello Kovozávody Prostejov. Il Grumman J4F-1 "Widgeon" è un idrovolante anfibio bimotore progettato e prodotto dalla Grumman Aircraft Corporation negli Stati Uniti durante la Seconda Guerra Mondiale. Derivato dal precedente Grumman Goose, il Widgeon è più piccolo e progettato principalmente per operazioni militari, ma ha trovato ampio impiego anche nel settore civile. Caratteristiche principali Ruolo: Idrovolante da pattugliamento marittimo, trasporto leggero e missioni di ricerca e soccorso. Struttura: Design compatto e leggero. Ali alte con galleggianti alle estremità per stabilità sull'acqua. Carrello d'atterraggio retrattile per operazioni anfibie (su acqua e terra). Dimensioni: Lunghezza: 9,47 metri. Apertura alare: 11,8 metri. Altezza: 3,7 metri. Motori: Due motori radiali Ranger L-440-5, ciascuno con una potenza di circa 200 cavalli. Velocità massima: circa 255 km/h. Autonomia: circa 1.400 km. Equipaggio e passeggeri: Equipaggio: 2 piloti. Capacità: fino a 3 passeggeri o un carico utile leggero. Armamento: In configurazione militare, era armato con una mitragliatrice calibro .30 e poteva trasportare cariche di profondità o bombe leggere, rendendolo utile per missioni antisommergibile. Utilizzo militare U.S. Navy e U.S. Coast Guard: Utilizzato per pattugliamento costiero, ricerca e salvataggio, e missioni antisommergibile durante la Seconda Guerra Mondiale. Royal Navy e altre forze alleate: Operò in ruoli simili, specialmente in regioni insulari o costiere. Era apprezzato per la sua versatilità, specialmente in scenari dove erano richieste capacità anfibie. Impiego nel Dopoguerra Dopo la guerra, molti Widgeon furono acquistati da operatori civili e convertiti per uso privato o commerciale, come trasporto leggero e turismo in aree costiere e insulari. La loro capacità anfibia li rese popolari tra compagnie che operavano in regioni remote o difficili da raggiungere. Importanza storica Il Grumman J4F-1 Widgeon è ricordato come uno dei più piccoli e versatili anfibi della Grumman. Sebbene non avesse la capacità offensiva o la robustezza di altri velivoli della stessa epoca, eccelse in ruoli di supporto e pattugliamento, contribuendo significativamente alle operazioni costiere alleate.
Kit aereo Grumman Gosling Mk.I in scala 1/72 - Modello Kovozávody Prostejov. Il Grumman Gosling Mk.I è la designazione britannica per il Grumman G-21 Goose, un idrovolante bimotore anfibio progettato e costruito dalla Grumman Aircraft Engineering Corporation negli Stati Uniti. Fu sviluppato negli anni '30 come velivolo di trasporto privato di lusso, ma divenne ampiamente utilizzato durante la Seconda Guerra Mondiale per ruoli militari come trasporto leggero, ricognizione e missioni di ricerca e soccorso. Caratteristiche principali del Grumman Gosling Mk.I Ruolo: Aereo anfibio da trasporto leggero e ricognizione. Utilizzato principalmente dalla Royal Navy e dalla Royal Air Force (RAF). Struttura: Fusoliera in metallo robusto, progettata per operazioni sia su acqua che su piste terrestri. Ali montate sulla parte alta della fusoliera, con galleggianti sotto le estremità alari per la stabilità sull'acqua. Dimensioni: Lunghezza: 11,5 metri. Apertura alare: 14 metri. Altezza: 4 metri. Motori: Alimentato da due motori radiali Pratt & Whitney R-985 Wasp Junior, ciascuno con una potenza di circa 450 cavalli. Capacità di raggiungere una velocità massima di circa 300 km/h. Equipaggio e passeggeri: Equipaggio: 2 piloti. Capacità di trasporto: fino a 6 passeggeri o un carico utile di circa 680 kg. Armamento (versioni militari): Nessun armamento offensivo standard, ma alcune varianti potevano essere equipaggiate con mitragliatrici leggere o bombe per missioni antisommergibili e di pattugliamento costiero. Impiego operativo Royal Air Force (RAF) e Royal Navy utilizzarono il Grumman Gosling Mk.I durante la Seconda Guerra Mondiale per compiti di: Trasporto di personale e materiali. Pattugliamento marittimo e costiero. Missioni di evacuazione medica. Ricerca e soccorso, specialmente in scenari isolati e difficili da raggiungere. Importanza storica Il Gosling Mk.I rappresenta un adattamento militare efficace di un progetto civile, dimostrando grande versatilità durante la Seconda Guerra Mondiale. Sebbene non fosse destinato al combattimento diretto, il suo contributo nelle operazioni logistiche e di supporto fu significativo, specialmente in ambienti marittimi o isolati. Dopo la guerra, molti esemplari tornarono a un uso civile o furono venduti a compagnie aeree regionali.
Kit aereo Grumman G-44 'Widgeon' in scala 1/72 - Modello Kovozávody Prostejov. Il Grumman G-44 "Widgeon" è un idrovolante anfibio leggero, progettato e costruito negli anni '40 dall'azienda americana Grumman Aircraft Engineering Corporation. Era destinato principalmente all'uso civile, ma venne successivamente adattato per impieghi militari durante la Seconda Guerra Mondiale, trovando un ruolo importante in missioni di pattugliamento, ricerca e soccorso, e trasporto leggero. Caratteristiche principali Ruolo: Aereo da trasporto leggero. Operazioni di ricerca e salvataggio (SAR). Pattugliamento costiero. Struttura: Idrovolante anfibio con fusoliera idrodinamica per decolli e atterraggi in acqua e carrello retrattile per operazioni terrestri. Ali alte e galleggianti alle estremità per stabilità in acqua. Dimensioni: Lunghezza: 9,47 metri. Apertura alare: 11,6 metri. Altezza: 3,4 metri. Motorizzazione: Due motori radiali Ranger L-440 raffreddati ad aria, ciascuno con una potenza di circa 200 cavalli. Velocità massima: 255 km/h. Autonomia: circa 1.300 km. Altitudine massima operativa: 4.600 metri. Capacità: Equipaggio: 2 piloti. Capacità di trasporto: fino a 3 passeggeri o un carico leggero. Impiego civile Il G-44 "Widgeon" fu originariamente concepito come un idrovolante per il mercato privato, pensato per trasportare passeggeri su brevi distanze, soprattutto in regioni costiere o isole. Grazie alla sua capacità anfibia, si dimostrò ideale per collegamenti rapidi tra località difficilmente accessibili via terra. Impiego militare Durante la Seconda Guerra Mondiale, il "Widgeon" venne adattato per scopi militari, in particolare per la U.S. Navy, la Guardia Costiera, e la U.S. Army Air Forces. Fu impiegato in vari ruoli: Pattugliamento costiero: Sorveglianza di aree costiere e individuazione di sommergibili nemici. È celebre un episodio in cui un "Widgeon" della Guardia Costiera americana affondò il sottomarino tedesco U-166 nel Golfo del Messico. Ricerca e soccorso: Operazioni di recupero in mare grazie alla sua capacità anfibia. Trasporto leggero: Trasporto di ufficiali, equipaggiamenti o piccoli carichi in teatri di guerra. Designazioni militari: U.S. Navy e Guardia Costiera: J4F-1 e J4F-2. U.S. Army Air Forces: OA-14. Utilizzo postbellico Dopo la guerra, molti esemplari del G-44 "Widgeon" vennero venduti a privati e operatori commerciali. Grazie alla sua versatilità, il "Widgeon" divenne popolare per: Operazioni turistiche. Pesca sportiva. Servizi di trasporto merci in regioni remote. Importanza storica Il Grumman G-44 "Widgeon" è un esempio di aereo multifunzione che ha saputo rispondere efficacemente sia alle esigenze civili che militari. Sebbene meno famoso di altri velivoli Grumman, come il Goose, il "Widgeon" si è distinto per le sue prestazioni affidabili e la sua versatilità, rimanendo in uso per decenni dopo la sua introduzione.
Kit aereo AGO C.IV 'Special Markings' in scala 1/72 - Modello Kovozávody Prostejov. L'AGO C.IV 'Special Markings' è una variante del AGO C.IV, un velivolo da ricognizione biposto tedesco utilizzato durante la Prima Guerra Mondiale. Il termine 'Special Markings' fa riferimento a una versione del modello con livree o segni distintivi particolari, spesso usati per personalizzare gli aerei di squadroni o piloti specifici, o per distinguersi in missioni particolari. AGO C.IV: Caratteristiche generali Ruolo: Aereo da ricognizione e osservazione armata, tipico della classe C della Germania Imperiale. Design: Biplano con fusoliera centrale e motore montato in configurazione spingente. Progettato dalla compagnia AGO Flugzeugwerke, conosciuta per i suoi velivoli innovativi. Motore: Equipaggiato con un motore Mercedes D.IV da 220 cavalli, che offriva una velocità massima di circa 160 km/h. Armamento: Una mitragliatrice Parabellum per l'osservatore (posteriore). Alcuni modelli potevano essere equipaggiati con un armamento offensivo per il pilota. Equipaggio: Pilota e osservatore, con quest'ultimo responsabile della ricognizione e della gestione delle armi difensive. Special Markings Questa dicitura si riferisce a livree distintive, spesso utilizzate per identificare unità specifiche o aerei assegnati a ufficiali di alto rango. Caratteristiche comuni delle marcature speciali: Colori unici o motivi decorativi come emblemi, stemmi o motivi geometrici. Contrassegni per missioni celebrative, commemorative o propagandistiche. Ruolo operativo Ricognizione tattica e strategica: Usato per osservare le linee nemiche, identificare movimenti di truppe e dirigere il fuoco dell'artiglieria. Missioni di bombardamento leggero: Equipaggiato occasionalmente con piccole bombe per colpire bersagli tattici. Intercettazioni armate: Nonostante fosse principalmente un ricognitore, poteva difendersi contro caccia nemici. Importanza storica L'AGO C.IV rappresentava un'evoluzione significativa nel design aeronautico tedesco durante la Prima Guerra Mondiale. Sebbene non sia stato prodotto in grandi quantità rispetto ad altri velivoli tedeschi, si distinse per il suo design unico e le sue capacità operative versatili. Le versioni con special markings aggiungono un elemento storico interessante, riflettendo l'individualità e l'identità delle unità che lo utilizzavano.
Kit aereo Zlin Z-50M in scala 1/48 - Modello KOVOZAVODY PROSTEJOV. Lo Zlin Z-50M è un aereo da addestramento e acrobazia leggera, progettato e prodotto dalla Moravan Otrokovice (Repubblica Ceca). Fa parte della famiglia di velivoli Zlin Z-50, conosciuti per le loro eccellenti prestazioni nel volo acrobatico competitivo e per l'addestramento di piloti in manovre avanzate. Caratteristiche principali Ruolo: Aereo da addestramento e acrobazia. Costruttore: Moravan Otrokovice. Motore: Versione equipaggiata con un motore Walter M-137AZ, un'opzione più economica rispetto al motore più potente delle altre varianti Z-50. Primo volo: Fine anni '70 (versione originale Z-50), con la versione Z-50M introdotta come variante successiva. Equipaggio: 1 pilota. Velocità massima: Circa 310 km/h. Apertura alare: Circa 8,4 metri. Peso massimo al decollo: Circa 750 kg. Caratteristiche distintive Design ottimizzato per acrobazie: La struttura leggera e resistente, combinata con una configurazione aerodinamica avanzata, rende lo Z-50M ideale per eseguire manovre acrobatiche complesse. Motore meno potente: Rispetto alle versioni più performanti della famiglia Z-50, lo Z-50M utilizza un motore meno potente per ridurre i costi operativi, rendendolo adatto all'addestramento iniziale. Eccellente manovrabilità: Progettato per rispondere rapidamente ai comandi del pilota, una caratteristica essenziale per il volo acrobatico. Robustezza strutturale: Capace di sostenere elevate forze di g, necessarie per le acrobazie. Utilizzo Addestramento: Utilizzato principalmente per addestrare piloti acrobatici, in particolare nelle scuole di volo. Competizioni acrobatiche: Partecipazione a competizioni nazionali e internazionali di volo acrobatico, anche se meno comune rispetto alle versioni più potenti della famiglia Z-50. Uso civile: Popolare tra gli appassionati di volo acrobatico per il suo costo relativamente basso e la semplicità di manutenzione. Conclusione Lo Zlin Z-50M rappresenta una versione più accessibile e versatile della famiglia Z-50, mantenendo gran parte delle caratteristiche che hanno reso questi aerei celebri nel mondo del volo acrobatico. È apprezzato per il suo design robusto e le capacità manovrabili, pur offrendo un'opzione economica per l'addestramento e l'uso ricreativo.