Google
 

Thursday, February 12, 2009

Samolot mysliwsko-bombowy Su-22

Samolot mysliwsko-bombowy Su-22 Military Papercraft


View full image please click on image

Like the Buccaneer, the SU22 was designed as a high speed, medium range, low level ground attack / recce aircraft. The main design difference between the two being that the SU22 was never intended for carrier operations and from the outset had a limited air-to-air capability. Although its origin can be traced back to the basic SU7 aircraft of the 1950’s, the design was continuously developed emerging as the variable geometry (Swing-wing 30:63) SU17 / 22, the most modern and powerful Warsaw Pact fighter bomber. The NATO code name for the type was “Fitter”.

The design exemplifies two key traits synonymous with Russian military equipment; the twin virtues of Simplicity & Robustness, both in the physical construction of the aircraft as well as its operation. The intent was to have trouble free use under the most demanding operating and environmental conditions combined with ease of maintenance. Both the airframe and the Lyulka AL-21 F-3 engine more than met this challenge!


The SU22M-4 is the final export version of the type and represents the pinnacle in the evolution of the design. It is still widely used in Europe and the Middle East, being broadly compatible to a Tornado GR1 although lacking the latter’s all-weather capability. Like the Tornado it is equipped with a laser range finder designator and terrain following radar and could be equipped with bombs, guided missiles & rockets in addition to the installed twin 30mm canon for the air to surface attack role. Air-to-air threats were countered via rockets, guided missiles and canon in addition to the extensive ECM and chaff / flare systems.

HHA operate one SU22M4, its supersonic capability and ten hardpoints enabling a variety of threat simulation profiles to be flown. Our aircraft is the only one of its type being operated by a civilian company and was acquired from the German Air Force.

Initially delivered on the 26-11-1986 as “629” of the NVA (East German Air Force), it served with 2/ MFG 28 (2nd Squadron, Naval wing 28) at Laage until it was prematurely retired on the 2-10-90 as a result of the collapse of the East German regime.

The German MoD had decided not to keep the SU22 on its inventory, and as a result the East German Squadrons were disbanded and the aircraft was placed in airworthy store under the new squadron code “25+29”. However, the aircraft was still very much a potent strike aircraft in use all over the world, so the German Test and Evaluation Centre (WTD –61) at Manching acquired seven of the type for technological evaluation purposes. Our SU was one of these and became “98+14” with its new owners on 23-9-1991. The aircraft were test flown and maintained by former NVA personnel, with major servicing being undertaken by the Polish aircraft facility WZL-2 at Bydgoszcz. West German pilots and ground crews were rapidly brought up to speed on the type and the evaluation of its systems lasted until September 1998.


After extensive negotiations HHA acquired the aircraft on the 14 January 1999 when it was flown to our maintenance facility at RAF Scampton. When delivered, the aircraft had accrued only 767 flight hours in 743 flights and became the youngest & lowest houred aircraft in our fleet.






Download Paper Model : Click Here

Radziecki czotg tywajacy T-38 M2

Radziecki czotg tywajacy T-38 M2 Military Papercraft



View full image please click on image

M2 Light Tank


Type Light tank
Place of origin United States
Specifications
Weight 11.6 tonnes (25,600 lb)
Length 4.43 m (14.53 ft)
Width 2.47 m (8.1 ft)
Height 2.65 m (8.69 ft)
Crew 4 (Commander/gunner, loader, driver, co-driver)
Armor 6 - 25 mm (0.25 - 1.0 in)
Primary
armament 1x 37 mm Gun M5
103 rounds
Secondary
armament 5x .30-06 Browning M1919A4 machine guns
8,470 rounds
Engine Continental W-670-9A, 7 Cylinder
245/220 hp (183/164 kW)
Power/weight hp/tonne
Suspension Vertical Volute Spring Suspension (VVSS)
Operational
range 320 km (199 mi)
Speed 58 km/h (36 mi/h)

The Light Tank M2 was an American pre-World War II light tank that saw use in early battles of the Pacific War. Although only a few saw combat, it was an important development step in the line of US light tanks of World War II.

Development History

As the Light Tank T2E1, the M2 was developed in 1935 by Rock Island Arsenal for the infantry branch of the U.S. Army. The design coming from the earlier T1 and T2 was somewhat inspired by the famous Vickers 6-ton. Its main weapon was one .50 machine gun, installed in a small one-man turret. After only 10 units were delivered, the Infantry branch decided to switch to a twin turret configuration, with a .30 machine gun in the second turret. These early twin-turret tanks were given the nickname "Mae West" by the troops, after the popular movie star. The twin-turret layout was inefficient, but was a common feature of 1930s light tanks derived from the Vickers, such as the Soviet T-26 and Polish 7TP.

Following the Spanish Civil War, the U.S. Army understood it needed better arms and better armored vehicles. The Cavalry branch had already opted for a single, larger turret on its nearly identical M1 Combat Car. By 1940 the twin machine gun turrets were replaced by one larger turret with a 37 mm gun, and armor reached 25 mm. Other upgrades included improved suspension, improved transmission, and better engine cooling.

The Battle of France gave momentum to the US tank program, and in July 1940 work began on a new light tank based on the M2 series. By adding heavier armor and a slightly longer hull, the M3 was created. The early M3 closely resembled the M2A4 and indeed the two types occasionally served in the same units; the easiest recognition feature is the idler wheel. On the M2A4, the idler is raised; on the M3 it trails on the ground, increasing the flotation of the heavier vehicle. In March 1941 light tank production switched to the M3 series.

The M2's importance lies in the sound basis it provided for US M3-series light tanks early in WW2. The M3's high speed and mechanical reliability were legacies of the M2 program.[citation needed]


Employment

By December 1941, the M2A1, M2A2 and M2A3 were used for training only. A few M2A4 saw some combat in the Battle of Guadalcanal with the U.S. Marine Corps and remained in service in some areas of Pacific until 1943.

Britain ordered 100 M2A4s in early 1941. After 36 of them were delivered, the order was canceled in favor of an improved Light Tank M3.

M2A2 "Mae West" on display at Patton Cavalry and Armor Museum, Fort Knox, KY
  • M2A1 (1935).
    • .50 MG in a single turret. 10 units were produced.
  • M2A2 (1935).
    • Twin turrets. Dubbed "Mae West". 239 units produced.
  • M2A3 (1938).
    • Twin turrets, Thicker armor, improved suspension. 72 units produced.
  • M2A4 (1940).
    • Single turret with 37mm gun. Thicker armor. 375 units produced.


Download Paper Model : Click Here

Tuesday, February 10, 2009

SAMOLOT TOWARZYSZACY LUBLIN R-XIII D

SAMOLOT TOWARZYSZACY LUBLIN R-XIII D


View full image please click on image

The Lublin R-XIII was the Polish army-cooperation plane (observation and liaison plane), designed in the early-1930s in the Plage i Laśkiewicz factory in Lublin. It was the main army cooperation plane in the Invasion of Poland. Its variant Lublin R-XIV was a military trainer aircraft.



Design and development

In 1927, the Polish aviation authorities announced a contest for an army-cooperation plane (in Polish: samolot towarzyszący, literally: acompanying plane. In Polish doctrine it was a close reconnaissance, observation and liaison aircraft, operating from casual airfields, providing big Army land units with information about the enemy). The PZL state factory proposed the PZL Ł-2, built in a series of 25 aircraft, while private factory Plage i Laśkiewicz in Lublin proposed the Lublin R-X, designed by Jerzy Rudlicki. It was flown on February 1, 1929. Five aircraft were built for the Air Force as R-Xa, and one was built as a long-distance sports plane. The third competitor was the PWS-5t2.

The contest was won by the R-Xa, having the shortest take-off and landing, and good performance, but the factory was ordered to develop design further. At that time, Rudlicki was working upon an unarmed trainer aircraft R-XIV and an observation aircraft R-XV. Both were new designs, basing upon the R-X construction (a trivia is, that number XIII was initially omitted in designations as "unlucky"). In February 1930, the Polish Air Force ordered 15 of R-XIV. The first serial plane was built in June 1930, without an earlier prototype, and all were delivered by July 1931. The R-XIV was a two-seater, parasol wing aircraft, with a 220hp radial engine and fixed landing gear. The crewman sat in open cabs in tandem. The R-XV was not ordered, but the Air Force demanded instead, that two R-XIV should be armed with an observer's machine gun, for testing. Such armed R-XIV, fitted also with other minor modifications, most notably a changed shape of a tail fin, became the first prototype of the army-cooperation plane, that received a designation Lublin R-XIII.

In July 21, 1931, 50 aircraft R-XIII were ordered. The first series of 30 were designated R-XIIIA, the next 20 were R-XIIIB. Both variants differed mostly in a type of a machine gun ring mounting. The first serial R-XIII was built on June 7, 1932. By March 11, 1933, all were given to the Air Force.

In 1932, next 170 aircraft were ordered. 48 were built in R-XIIIC variant with minor modifications, then 95 were built in a most numerous R-XIIID variant. It introduced visible changes, like a Townend ring on a radial engine, and a new engine cowling. It also had new type of a machine gun ring mounting. The first R-XIIID was tested in February, 1933. All aircraft were given to the Air Force by March 2, 1935. During repairs, older models A, B and C were modified to R-XIIID standard as well.

In 1933, Jerzy Rudlicki proposed a new design R-XXI, for a new contest for R-XIII successor, but it was not accepted (the contest was won by the RWD-14 Czapla). However, some of R-XXI features, like higher and rounded in cross-section fuselage and changed shape of a tail fin, were found in latest R-XIII variants. Single prototype of the R-XIIIE was built in 1934, fitted with a stronger 360hp engine Gnome-Rhone 7K Titan, but it was not produced. Another variant R-XIIIF introduced new, Polish-designed 340hp engine Skoda G-1620A Mors-I. It had no Townend ring on cylinders of the radial engine. After one prototype (no. 56.101), a series of 50 R-XIIIF were ordered in 1934. After 7 aircraft had been delivered, the Polish aviation authorities refused to buy nearly-completed further 18 aircraft, planning to nationalize all aviation industry in Poland. As a result, Plage i Laśkiewicz factory went bankrupt in late 1935, and it was next nationalized under a name LWS (Lubelska Wytwórnia Samolotów - Lublin Aircraft Works). Then, 18 R-XIIIF, bought by scrap price, were completed, and next series of 32 was built. All R-XIIIF were delivered to the Air Force by 1938. However, only 26 of them were completed with Mors engines (and mostly used for training or staff liaison), while 32 had standard 220hp Wright engines, lowering their performance to R-XIIID level.

In 1931, one R-XIV was tested on floats, as a seaplane. Since tests came out well, the Polish Navy designated it R-XIII bis/hydro and ordered the next three (nos. 700-703). In 1933, the Navy ordered 10 R-XIII ter/hydro, which was a seaplane variant of R-XIIID (nos. 704-713). Finally, in 1934 the Navy bought 6 R-XIIIG seaplanes, differing in details from a previous variant - among others, a metal propeller (nos. 714-720). They were delivered by April 1935. All variants could also be easily converted to wheeled landing gear.

In 1933, one R-XIIIB was converted to a long-distance sport plane R-XIIIDr, named Błękitny Ptak (the Blue Bird), meant for a flight to Australia, however it was crashed in 1935 in Siam by Stanisław Karpiński. Several aircraft were converted to civilian sport ones, used in aeroclubs.

12 R-XIII's were converted to blind flying trainers R-XIIIt in 1934, with higher closed trainee cab. Some were converted to simple liaison aircraft, removig armament and mounting a windscreen in the second cab. Several R-XIII were used to tow gliders, using a special frame with a hook, attached to a fuselage.

The R-XIII prototype was converted in 1932 to an experimental variant R-XIX, with V-tail of Rudlicki's design, but it was not accepted by the authorities, despite it had better field of machine gun fire.

In total, 15 R-XIV and 273 R-XIII were built, including 20 seaplanes.

Combat use

In the early 1930s the R-XIII was quite a successful plane for its purpose. It had a very short take-off (68 m for R-XIIIA) and landing, enabling it to operate from fields and meadows. However, only some of R-XIIIs were equipped with a radio and a camera, what lowered their usefulness. In 1932-1936 they were used in three-aircraft liaison platoons, being a basic Polish army-cooperation plane. In 1937 they were formed into army-cooperation escadres (eskadra towarzysząca), in 1939 reformed into observation escadres (eskadra obserwacyjna). Only in 1939, part of R-XIII were replaced by the RWD-14b Czapla, which was not much more modern. A planned replacement was a modern LWS-3 Mewa, but it was not introduced due to war outbreak.

In the Invasion of Poland in 1939, the Polish Air Force had about 150 R-XIII. Of them, 49 were in combat units, 30 in reserve, about 30 in training units and about 40 in repairs. In combat units, R-XIII were used in 7 observation escadres (out of 12): numbers 16, 26, 36, 43, 46, 56 and 66. Each escadre had 7 aircraft. The 16th Escadre was in C-in-C reserve, while the others were distributed among the field Armies. The R-XIII was no match for any of Luftwaffe fighters, bombers or even reconnaissance aircraft, being much slower, and armed with only one machine gun, but they were actively used for close reconnaissance and liaison tasks.

About 40 R-XIII of combat units were destroyed during the campaign, but only part of them were shot down by the German aircraft or flak. During the campaign, 9 aircraft were given to observation escadres as replenishment. Some planes were also used in a wartime improvised units in air bases. About 10 combat aircraft and 7 from other units were withdrawn to Romania. A number of aircraft were bombed by the Germans in air bases or burned by withdrawing Poles. None have survived to today.

In the Naval Air Squadron, 11 R-XIIIter and R-XIIIG floatplanes were used in 1939. One of them made a night bombing raid on Danzig on September 7, searching in vain for Schleswig-Holstein. On September 8 all planes were bombed, while stationed on the sea near Hel on Hel Peninsula.

Variants

  • R-XIII prototype (conversion of R-XIV, no. 56.1)
  • R-XIIIA - army cooperation aircraft, 30 produced from 1931 (nos 56.2-56.31)
  • R-XIIIB - army cooperation aircraft, 20 produced from 1932 (nos 56.32-56.51)
  • R-XIIIC - army cooperation aircraft, 48 produced from 1933 (nos. 56.52-56.99)
  • R-XIIID - standard variant of army cooperation aircraft, 95 produced from 1933 (nos 56.102-56.196)
  • R-XIIIE - one prototype of 1934 with 360hp Gnome-Rhone 7K Titan engine (no. 56.100)
  • R-XIIIF - army cooperation aircraft with modified fuselage, part with 340hp Skoda G-1620A Mors-I engine, 58 produced from 1934 (nos. 56.101, 58.01-58.57)
  • R-XIII bis/hydro - seaplane, 4 produced from 1931 (nos. 700-703)
  • R-XIII ter/hydro - seaplane, 10 produced from 1934 (nos. 704-713)
  • R-XIIIG - seaplane, 6 produced from 1934 (nos. 714-720)
  • R-XIIIDr - long-distance sport conversion, 1 made (no. 56.51)
  • R-XIIIt - trainer conversion, at least 12 made
  • R-XIV - trainer, 15 produced from 1930 (nos. 54.1-54.15)
  • R-XV - army cooperation variant of R-XIV, not built
  • R-XIX - one prototype with V-tail of 1932 (no. 56.1)
  • R-XXIII - This was the original designation of the R-XIIIDr.

Description

Mixed construction (steel and wood) plane, conventional in layout, with braced high-wings, canvas and plywood covered (front part of a fuselage was metal covered). Conventional fixed landing gear, with a rear skid. Crew of two, sitting in tandem in an open cockpit, with twin controls. The observer had a 7.7 mm Vickers K or Lewis machine gun on a ring mounting (rarely 2 machine guns). The aircraft could be fitted with racks for small bombs 12–25 kg. A 9 cylinder air-cooled radial engine Wright Whirlwind J-5 (produced in Poland) with 162 kW (220 hp) nominal power and 176 kW (240 hp) take-off power (on 22 aircraft R-XIIIF, 250 kW (340 hp) engine Skoda G-1620A Mors-I). Two-blade wooden or metal propeller. Fuel tank 200 liters in the fuselage, could be dropped in case of fire emergency (R-XIV - 135 liter tank).

Operators

Specifications (R-XIIID)

General characteristics

  • Crew: 2 - Pilot and observer
  • Length: 8.5m ()
  • Wingspan: 13.2m ()
  • Height: 2.8m ()
  • Wing area: 24.50m2 ()
  • Empty weight: 956kg (2,108lb)
  • Loaded weight: 1332kg (2,930lb)
  • Powerplant:Wright Whirlwind J-5 9-cylinder radial engine, 162kW (220hp)

Performance



Download Paper Model : Click Here

Monday, February 9, 2009

Historyczny zaglowiec Mayflower

Historyczny zaglowiec Mayflower


View full image please click on image

The Mayflower was the famous ship that transported the English Separatists, better known as the Pilgrims, from Southampton, England, to Plymouth, Massachusetts (which would become the capital of Plymouth Colony), in 1620.[1]

The vessel left England on September 6 (Old Style)/September 16 (New Style),[2] and after a gruelling 66-day journey marked by disease, which claimed two lives, the ship dropped anchor inside the hook tip of Cape Cod (Provincetown Harbor) on November 11/November 21.[1] The Mayflower was originally destined for the mouth of the Hudson River, near present-day New York City, at the northern edge of England's Virginia colony, which itself was established with the 1607 Jamestown Settlement.[3] However, the Mayflower went off course as the winter approached, and remained in Cape Cod Bay. On March 21/28, 1621, all surviving passengers, who had inhabited the ship during the winter, moved ashore at Plymouth, and on April 5/15, the Mayflower, a privately commissioned vessel, returned to England.[1] In 1623, a year after the death of captain Christopher Jones, the Mayflower was most likely dismantled for scrap lumber in Rotherhithe, London.[4]



The Mayflower has a famous place in American history as a symbol of early European colonization of the future US. With their religion oppressed by the English Church and government,[5] the small party of religious separatists who comprised about half of the passengers on the ship desired a life where they could practice their religion freely. This symbol of religious freedom resonates in US society and the story of the Mayflower is a staple of any American history textbook. Americans whose roots are traceable back to New England often believe themselves to be descended from Mayflower passengers.

The main record for the voyage of the Mayflower and the disposition of the Plymouth Colony comes from William Bradford who was a guiding force and later the governor of the colony.

Ship

The Mayflower was used primarily as a cargo ship, involved in active trade of goods (often wine) between England and other European countries,[6][7] (principally France, but also Norway, Germany, and Spain). At least between 1609 and 1622, it was mastered by Christopher Jones, who would command the ship on the famous transatlantic voyage, and based in Rotherhithe, London, England.[1] After the famous voyage of the Mayflower, the ship returned to England, likely dismantled for scrap lumber in Rotherhithe in 1623, only a year after Jones's death in March 1622. The Mayflower Barn, just outside the Quaker village of Jordans, in Buckinghamshire, England, is said to be built from these timbers, but this is likely apocryphal.[8]

Details of the ship's dimensions are unknown; but estimates based on its load weight and the typical size of 180-ton merchant ships of its day suggest an estimated length of 90–110 feet (27.4–33.5 m) and a width of about 25 feet (7.6 m).[6]

The ship probably had a crew of twenty-five to thirty,[7] along with other hired personnel; however, only the names of five are known, including John Alden.[7] William Bradford, who penned our only account of the Mayflower voyage, wrote that John Alden "was hired for a cooper [barrel-maker], at South-Hampton, where the ship victuled; and being a hopefull yong man, was much desired, but left to his owne liking to go or stay when he came here; but he stayed, and maryed here."[9]


Download Paper Model : Click Here

Sunday, February 8, 2009

DOWODCA LIBERATORA

DOWODCA LIBERATORA Military Papercraft



View full image please click on image

"B-24" redirects here. For other meanings, see B24.
B-24 Liberator
U.S. Army Air Forces Consolidated B-24D Liberator over Maxwell Field, Alabama.
Role Heavy bomber
Manufacturer Consolidated Aircraft
Designed by Isaac M. Laddon
First flight 29 December 1939
Introduced 1941
Retired 1945
Primary users United States Army Air Forces
United States Navy
Royal Air Force
Royal Canadian Air Force
Produced 1940-1945
Number built 18,482
Unit cost $297,627[1]
Variants PB4Y Privateer
XB-41
C-87 Liberator Express
Consolidated R2Y
Consolidated Liberator I


The Consolidated B-24 Liberator was an American heavy bomber, built by Consolidated Aircraft. It was produced in greater numbers than any other American combat aircraft of World War II and still holds the record as the most produced U.S. military aircraft. It was used by many Allied air forces and every U.S. branch of service during the war, attaining a distinguished war record with its operations in the northern European, Pacific and Mediterranean theaters.

Often compared to the better known B-17 Flying Fortress, the B-24 was a more modern design with a higher top speed and greater range yet it had a similar bomb load and defensive armament. Nevertheless, popular opinion among aircrews and general staff tended to favor the B-17's rugged qualities above all other considerations.[2] The B-24 was notorious among American air crews for its tendency to catch fire. The placement of the B-24's fuel tanks throughout the upper fuselage and its lightweight construction, designed both to increase range and optimize assembly line production, made the aircraft vulnerable to battle damage.[3] The B-24 was more difficult to fly as well, with heavy control forces and poor formation flying characteristics. The B-24 nevertheless provided excellent service in a variety of roles thanks to its large payload and long range.

Development


XB-24 in flight

The Liberator originated from a United States Army Air Corps (USAAC) request in 1938 for Consolidated to produce the B-17 under license. This was part of "Project A", a program to expand American industrial capacity for production of the key components of air power.[4] After company executives including President Reuben Fleet visited the Boeing factory in Seattle, Consolidated decided instead to submit a more modern design of its own.[5] In January 1939, the USAAC, under Specification C-212, formally invited Consolidated [6] to submit a design study for a bomber with greater range, higher speed, and greater ceiling than the B-17.

The contract for a prototype was awarded in March 1939, with the requirement that a prototype be ready before the end of the year. The design was simple in concept but advanced for its time. Compared to the B-17, the proposed Model 32 was shorter and had 25% less wing area, but a six foot (1.8 m) greater wingspan and a substantially greater carrying capacity. Whereas the B-17 used 9-cylinder Wright R-1820 Cyclone engines, the Consolidated design used twin-row, 14-cylinder Pratt & Whitney R-1830 Twin Wasp radials of 1,000 hp (746 kW). The 70,547 lb (32,000 kg) maximum takeoff weight was one of the highest of the period. Consolidated also incorporated innovative features: the new design would be the first American bomber to use tricycle landing gear and it had long, thin wings with the efficient "Davis" high aspect ratio design (also used on the projected Model 31 flying boat)[7] promising to provide maximum fuel efficiency. The aircraft also had a distinctive twin tail and rudder assembly.
YB-24.

Wind tunnel testing and experimental programs using an existing Consolidated Model 31, a twin-engined commercial flying boat, provided extensive data on the flight characteristics of the Davis airfoil.[8]

Consolidated finished the prototype, by then known as the XB-24, and had it ready for its first flight two days before the end of 1939. Seven more YB-24 development aircraft flew in 1940 and Consolidated began preparing production tooling.[9] Early orders—placed before the XB-24 had flown—included 36 for the USAAC, 120 for the French Armée de l'Air and 164 for the Royal Air Force (RAF). Most of the first production B-24s went to Britain, including all those originally ordered by the Armée de l'Air after France collapsed in 1940. The name, "Liberator" was initially assigned by the RAF and subsequently was adopted by the USAAC as the official name for the type.[10]

Design

The B-24's spacious slab-sided fuselage (which earned the aircraft the nickname "Flying Boxcar")[11] was built around a central bomb bay that could accommodate up to 8,000 pounds of bombs. The bomb bay was divided into front and rear compartments and further divided by a central catwalk, which was also the fuselage keel beam. A universal complaint arose over the extremely narrow catwalk. The aircraft was sometimes disparaged as "The Flying Coffin" because the only entry and exit from the bomber was in the rear and it was almost impossible for the flight crew and nose gunner to get from the flight deck to the rear if they were wearing their parachutes. An unusual set of "roller-type" bomb bay doors retracted into the fuselage with a minimum of aerodynamic drag, keeping speed high over the target area.[12]

Like the B-17, the B-24 had an array of .50 caliber machine guns in the tail, belly, top, sides and nose to defend it from attacking enemy fighters. Unlike the B-17, the ball turret could be retracted into the fuselage when not in use.

Operational history

Initial deployment

Doomed B-24 over Europe

Liberator GR Is in British service were the first B-24s to be used operationally. The very first use of a Liberator I in March 1941 was as a long-range transport: it was used to bring U.S. ferry pilots back from the United Kingdom.

The most important role for the first batch of the Liberator GR Is was in service with RAF Coastal Command on anti-submarine patrols in the Battle of the Atlantic.

Later in 1941, the first Liberator IIs entered RAF service. This model introduced self-sealing fuel tanks and powered gun turrets. At the same time, Consolidated added a 2 ft 7 in (79 cm) plug in the forward fuselage to create more space for crew members. The Liberator IIs were divided between Coastal Command, Bomber Command, and BOAC. Two RAF squadrons with Liberators were deployed to the Middle East in early 1942, in the first use of the Liberator as a bomber.[13]

America enters the war


B-24s bomb Ploieşti oil fields in August 1943

The United States Army Air Forces (USAAF) took delivery of their first B-24As in 1941. Like the British, they used them as transports first. American B-24s entered combat in June 1942. On June 6, in the Pacific, four B-24s staging through Midway tried to attack Wake Island (they could not find the target).[14] On 12 June, thirteen B-24s flying from Egypt attacked the Axis-controlled oil fields and refineries around Ploieşti, Romania.

Over the next three years, B-24 squadrons deployed to all theaters of the war: Africa, Europe, India, the Atlantic, and the Pacific. In the Pacific, the B-24 was designated the standard heavy bomber to simplify logistics, replacing the shorter-range B-17.

[edit] Later development and production

Continued development work by Consolidated produced a handful of transitional B-24Cs with turbocharged instead of supercharged engines. The turbocharged engines led to the flattened oval nacelles that distinguished all subsequent Liberator models.

The first mass-produced model was the B-24D (or Liberator III in British service), in service in early 1943. It had turbocharged engines and increased fuel capacity. Three more 0.50 caliber (12.7 mm) machine guns brought the defensive armament up to ten machine guns. At 59,524 lb (27,000 kg) maximum takeoff weight, it was one of the heaviest aircraft in the world; comparable with the British "heavies" the Stirling, Lancaster and Halifax.
B-24s under construction at Ford's Willow Run plant

B-24 production increased at an astonishing rate through 1942 and 1943. Consolidated tripled the size of its plant in San Diego and built a large new plant outside Fort Worth, Texas. More B-24s were built by Douglas in Tulsa, Oklahoma. North American built a plant in Dallas, Texas, which produced B-24Gs and B-24Js. None of these were minor operations, but they were dwarfed by the vast new greenfield factory built by Ford at Willow Run near Detroit, which opened in August 1942 and began mass production in August 1943. This was the largest factory in the United States, and the largest anywhere outside the USSR. It had the largest assembly line in the world (330,000 m² or 3,500,000 ft²) at the time of completion. At its peak Willow Run produced 428 B-24s per month. Many pilots slept on cots at Willow Run while waiting for 'their' B-24s to roll off the assembly line.[15]

Each of the B-24 factories was identified with a production code: Consolidated/San Diego, CO; Consolidated/Fort Worth, CF; Ford/Willow Run, FO; North American, NT; and Douglas/Tulsa, DT.

In 1943, the model of Liberator considered by many the "definitive" version was introduced. The B-24H was 10 inches (25 cm) longer, had a powered gun turret in the nose to reduce vulnerability to head-on attack and was fitted with an improved bomb sight, autopilot and fuel transfer system. Consolidated, Douglas and Ford all manufactured the B-24H, while North American made the slightly different B-24G. All five plants switched over to the almost identical B-24J in August 1943. The later B-24L and B-24M were lighter weight versions and differed mainly in defensive weaponry.
WASP pilots (left to right) Eloise Huffines Bailey, Millie Davidson Dalrymple, Elizabeth McKethan Magid, Clara Jo Marsh Stember. In the background, a B-24.

As the war continued, the complexity of servicing the B-24 grew greater and greater. The B-24s made by the different companies were slightly different, so repair depots had to stock many different parts to support various B-24 models. Fortunately, this problem was eased in the summer of 1944, when North American, Douglas, and Consolidated/Fort Worth stopped making B-24s, leaving only the Consolidated plant in San Diego and the Ford plant in Willow Run.

In all, 18,482 B-24s were built by September 1945. Twelve thousand saw service with the USAAF. The U.S. Navy operated about 1,000 PB4Y-1s and almost 800 PB4Y-2 Privateers, which were derived from the B-24. The Royal Air Force flew about 2,100 B-24s in 46 bomber groups and 41 squadrons, the Royal Canadian Air Force 1,200 B-24Js, and the Royal Australian Air Force (RAAF) 287 B-24Js, B-24Ls and B-24Ms. (Liberators were the only heavy bomber used by the RAAF in the Pacific.) Two squadrons of the South African Air Force deployed in the Mediterranean flew B-24s.

[edit] Strategic bombing

The B-24 was one of the workhorse bombers of the U.S. Eighth Air Force in the Combined Bomber Offensive against Germany. Thousands of B-24s, flying from bases in England, dropped hundreds of thousands of tons of bombs and incendiaries on German military, civilian and industrial targets.

B-24s of the Ninth Air Force, operating from Africa and Italy, and the Fifteenth Air Force, operating from Italy, also took a major role in strategic bombing. 13 of the Fifteenth AF's 18 bombardment groups flew B-24s.

The first B-24 lost over German territory occurred on 26 February 1943. By a cruel twist of fate there had been eleven men aboard the aircraft. For some time newspapers had been requesting permission for a reporter to go on one of the missions, and on this date Robert B. Post, and five other reporters of the The New York Times were granted permission. Mr Post was the only reporter assigned to a B-24 equipped group, the 44th Bomb Group, and flew in the B-24 41-23777 Maisey on Mission No. 37 to Bremen. Intercepted just short of the target the B-24 came under attack from JG 1s Messerschmitt Bf 109s. Leutnant Heinz Knoke (who finished the war with 31 kills) shot down the Liberator, only two of the 11 men survived. Neither was Post. Knoke reported:

The fire spread out along the right wing. The inboard propeller windmilled to a stop. And then, suddenly, the whole wing broke off. At an altitude of 900 metres there was a tremendous explosion. The bomber had disintegrated. The blazing wreckage landed just outside Bad Zwischenahn airfield[16]

A total of 178 B-24s carried out the famous second attack on Ploieşti, Operation Tidal Wave, on 1 August 1943.

RAF Bomber Command did not use B-24s as bombers over Europe. No. 223 Squadron RAF, one of Bomber Command’s 100 (Bomber Support) Group squadrons, used twenty Liberator VIs to carry electronic jamming equipment to counter German radar.

[edit] Other Roles

The B-24's long operating range made it suitable for other duties including maritime patrol, anti-submarine patrol, reconnaissance, tanker, cargo hauler, and personnel transport. Winston Churchill used a refurbished Liberator II as his personal transport aircraft.

[edit] Operation Carpetbagger

Between August 1943 until the end of the war in Europe, specially modified B-24Ds were used in classified missions. A joint venture between the Army Air Force and the Office of Strategic Services (OSS) code named "Operation Carpetbagger", pilots and crews flew the specially modified B-24Ds painted with a glossy black anti-searchlight paint to supply friendly underground forces throughout German occupied Europe. They also flew C-47s, A-26 Invaders, and British De Havilland Mosquitos. They flew spies called "Joes" and commando groups prior to the Allied invasion of Europe on D-Day and afterwards and retrieved over 5,000 officers and enlisted men who had escaped capture after being shot down. The low altitude, night-time operation was extremely dangerous and took its toll on these airmen. The first aircrews chosen for this operarion came from the anti-submarine bomb groups because of their special training in low altitude flying and pinpoint navigation skills. Also, because of their special skills, they were called upon to fly fuel to Patton when he outran his fuel supply. When this mission was completed, it was recorded that 822,791 gallons of 80 octane gasoline had been delivered to three different airfields in France and Belgium..[17]

[edit] Maritime Patrol
B-24 Very Long Range Liberators at the Consolidated-Vultee Plant, Fort Worth, Texas in the foreground with the dark green and white paint scheme. To the rear of this front line are C-87 "Liberator Express Transports" in various assembly stages.

The B-24 made a massive contribution to Allied victory in the Battle of the Atlantic against German U-boats. The decision to allocate some Liberator Is to Coastal Command in 1941 produced immediate results. The Very Long Range (VLR) Liberators "almost doubled the reach of Britain's maritime reconnaissance force". [18] This added range enabled Coastal Command patrols to cover the Mid-Atlantic gap, where U-boats had operated with near impunity. [19]

For twelve months, No. 120 Squadron RAF of Coastal Command, with its handful of much patched and modified early model Liberators, supplied the only air cover for convoys in the Atlantic Gap.

The Liberator was the only aircraft with the range for this. The VLR Liberators sacrificed some armor and often some gun turrets to save weight while adding extra fuel in bomb bay tanks. Liberator Is were equipped with ASV Mark II radar. Radar and the Leigh light gave them the ability to hunt U-boats by day and night.

They were operated from both sides of the Atlantic with the RCAF to the west and the RAF from the UK and Iceland. This role was dangerous, especially after many U-boats were armed with extra Flak guns and adopted a policy of staying on the surface to fight.

The sudden and decisive turning of the Battle of the Atlantic in the Allies' favor in May 1943 was the result of many factors. However, it was no accident that it coincided with the long delayed arrival of many more VLR Liberators for maritime patrol. Liberators were credited in full or part with 72 U-boat kills.

In addition to very long range patrols, the B-24 was vital for patrols of a radius less than 1,000 miles (1,600 km), in both the Atlantic and in the Pacific where B-24s and PB4Y-1s took a heavy toll of Japanese shipping. A total of 977 USN PB4Y-1s were used in the Pacific Theater in VB and VPB squadrons.

See also: PB4Y Privateer

[edit] Transport

Early model Liberators were used as unarmed long-range cargo carriers. They flew between Britain and Egypt (with an extensive detour around Spain over the Atlantic) and were used in the evacuation of Java. Liberator IIs were converted for this role and used by the British Overseas Airways Corporation (BOAC) for trans-Atlantic service and other assorted long-range transport duties. This variant was designated LB-30A by the USAAF.[10]

In early 1942, a B-24 Liberator damaged in an accident was converted into a cargo transport aircraft by elimination of the transparent nose and installation of a flat cargo floor. In April 1942, the C-87 Liberator Express transport version entered production at Fort Worth. The C-87 had a large cargo door, less powerful supercharged engines, no gun turrets, a floor in the bomb bay for freight and side windows. The navigator's position was relocated behind the pilot. Early versions were fitted with a single .50 Browning machine gun in the tail, and a few C-87s were also equipped with two .50 fixed machine guns in the nose, operable by the pilot, though these were also eventually eliminated. A more elaborate VIP transport, the C-87A, was also built in small numbers.

The C-87 was also designated the RY-2 or Liberator Cargo VII. The U.S. only made about 300 C-87s but they were nevertheless the backbone of the Army Air Force’s heavy transport operation. The C-87 flew in many theaters, including much hazardous duty in flights from Labrador to Greenland and Iceland in the North Atlantic. The aircraft proved extremely vulnerable to icing conditions, and was prone to fall into a spin with even small amounts of ice collected on the Davis wing.

In the China Burma India Theater (CBI), the C-87 was used to transport cargo and fuel over the Hump from India to China. The C-87 was not popular with either the military or the civilian transport crews assigned to fly them. The aircraft had a distressing habit of losing all cockpit electrical power on takeoff and landings, while engine power and reliability with the less-powerful superchargers often left much to be desired. The plane was designed as a bomber that dropped its loads while airborne. So the C-87's nose gear was not designed for landing with heavy loads, and frequently collapsed from the strain. Fuel leaks from the transport's hastily-modified fuel system were a common occurrence. In his autobiography, Fate is the Hunter, author Ernest K. Gann reported, while flying cargo in India, he barely avoided crashing a severely overloaded C-87 into the Taj Mahal. As Douglas C-54 transports became available, the C-87 was rapidly phased out of service.

The USAAF also converted 218 B-24Ds and B-24Es into C-109 tankers. These tankers were used in all theaters but they were most heavily employed transporting fuel in the CBI theater. C-109s flew from India to B-29 bases in China. With all armor and military equipment removed to save weight, a C-109 could carry almost 2,905 gal (11,000 L) of fuel, over 22,000 lb (10,000 kg). However, while a combat-loaded B-24 could safely take off with room to spare from a 6,000-foot (1,800 m) runway, a loaded C-109 required every foot of such a runway to break ground, and crashes were not uncommon. With its forward fuel tank filled to capacity, the C-109 tanker version proved to be longitudinally unstable while airborne as well.

The B-24 was also used heavily in the Pacific after the war to transport cargo and supplies during the rebuilding of Japan, China, and the Philippines.

In addition, a large number of unmodified B-24s were pressed into transport duties. Qantas Empire Airways used Liberators on the Perth-Colombo route, at the time the longest non-stop route in the world at 3,580 miles, until they were replaced by Avro Lancastrians.

[edit] Variants and conversions

[edit] U.S. Army Air Force Variants

XB-24 (Consolidated Model 32)
Designed in 1938 as an improvement on the B-17 Flying Fortress, at the request of the Army Air Corps. It had a wing specially designed for a high aspect ratio, tricycle landing gear, and twin vertical stabilizers. The XB-24 was ordered in 1939 March, and first flew on 29 December 1939. (Total: one)
YB-24/LB-30A Preproduction prototypes
Six examples were sent to Great Britain under lend-lease, under the designation LB-30A.
B-24
Service test version of the XB-24, ordered on 27 April 1939, less than 30 days after the XB-24 was ordered, before the XB-24 design was complete. A number of minor modifications were made: elimination of leading edge slots, addition of de-icing boots. (Total: seven; only one used for actual testing)

B-24 ex-"Diamond Lil" from the Commemorative Air Force collection. Airframe returned to B-24A configuration and renamed "Ol 927".[20]

B-24A/LB-30B
Ordered in 1939, the B-24A was the first production model. Due to the need for heavy bombers, the B-24A was ordered before any version of the B-24 flew. The main improvement over the XB-24 was improved aerodynamics, which led to better performance. Some sent to Great Britain under Lend Lease as LB-30B. (Total: 38,20 LB-30Bs, nine B-24Cs)
XB-24B
When the XB-24 failed to reach its projected top speed, the Pratt & Whitney R-1830-33 radials rated at 1,000 hp (746 kW) it carried were replaced with R-1830-41 turbo-supercharged radials rated at 1,200 hp (895 kW), increasing its top speed by 37 mph (59 km/h). The addition of the turbo-superchargers made the engine cowlings elliptical. The XB-24B version also lacked the engine slots of the original. (Total: one converted XB-24)
B-24C
Conversion of the B-24A using turbo-supercharged R-1830-41 engines. To hold the supercharger and the intercooler intake, the cowlings were made elliptical and the new items added on the sides. The tail air gunner position was improved by adding an Emerson A-6 power turret with twin .50-caliber (12.7 mm) machine guns; a Martin power turret was added to the forward fuselage. (Total: nine converted B-24As)

B-24D Liberator flight in formation.

B-24D
First model produced on a large scale; ordered from 1940 to 1942, as a B-24C with better engines (R-1830-43 supercharged engines). During the production run, the tunnel gun in the belly was replaced by a remote-sited Bendix belly turret; this was later replaced by a Sperry ball turret. In late B-24Ds, 'cheek' guns were added. (Total: 2696, 2381 Consolidated, San Diego; 305 Consolidated, Fort Worth, ten Douglas, Tulsa, Oklahoma). One famous B-24D was the Lady Be Good which was a basis for the TV movie Sole Survivor (1970 film).
B-24E
A slight alteration of the B-24D built by Ford, using R-1830-65 engines. Unlike the B-24D, the B-24E retained the tunnel gun in the belly. The USAAF used the B-24Es primarily as training aircraft since this model was not current in armaments and other technology as the aircraft being produced by Consolidated / San Diego (CO). Ford also built sub-assemblies for Douglas; these sub-assemblies were identical to Ford-built B-24Es, except that they used the same engines as the B-24D (R-1830-43 radials). These sub-assemblies were called PK ships and were shipped by truck from Willow Run to the final assembly in Tulsa, Oklahoma. (Total: 801)
XB-24F
A prototype made to test thermal de-icers, instead of the standard inflatable rubber "boots." (Total: one converted B-24D)
B-24G
Sperry ball turret, three .50 caliber- (12.7 mm) machine guns in nose. All B-24Gs were built by North American Aviation, which was contracted in 1942. (Total: 25)
B-24G-1
Modified Emerson A-6 tail turret in nose instead of two- three .50 caliber (12.7 mm) machine guns in earlier models. The B-24G-1 was based on the design of the B-24H (Total: 405)
B-24H
Because of obvious vulnerability of the B-24 to head-on attack, the B-24H design made by Ford used a nose turret, generally a modified Emerson A-6 tail turret. The entire aircraft was redesigned to better fit the turret; 50 airframe changes were made, including a redesigned bombardier compartment. The tail turret was given larger windows for better visibility, the top turret a higher bubble, and the waist gunner positions were offset, to reduce their interference during battle. (Total: 3100)

Consolidated B-24J-55-CO Liberator, Serial number 42-99949 belonged to 93rd BG, 328th BS; lost 21 September 1944 over Belgium.

B-24J
The B-24J was very similar to the B-24H, although the defensive improvements made in the B-24H were not incorporated in the B-24J. The B-24J featured an improved autopilot (type C-1) and a bombsight of the M-1 series. B-24H sub-assemblies made by Ford and constructed by other companies and any model with a C-1 or M-1 retrofit, were all designated B-24Js. (Total: 6678)
XB-24K
An experimental aircraft, made by Ford by splicing a B-23 Dragon tail empennage onto a B-24D airframe. The aircraft was more stable and had better handling than other models, but changing the B-24 design was too expensive to do at the time. However, the XB-24K was the ancestor of the Navy's PB4Y-1. (Total: one converted B-24D)
B-24L
Because of the immense weight of the B-24J, the Army pushed for a lighter version. In the B-24L, the ball turret was replaced by a floor ring mount with two .50 caliber (12.7 mm) machine guns, and the A-6B tail turret by an M-6A. In later aircraft, no tail armament was installed, and when it arrived at its airfield, either an A-6B, an M-6A, or a dual-mount manual .50-caliber (12.7 mm) gun was field-installed. (Total: 1667)
B-24M
An enhancement of the B-24L with further weight-saving devices. The B-24M used a more lightweight version of the A-6B tail turret; the waist gunner positions were left open. For better visibility, the windshield was replaced by a "knife-edge" dual pane versions. The B-24M became the last production model of the B-24; a number of the B-24s built flew only the course between the factory and the scrap heap. (Total: 2593)
XB-24N
A redesign of the B-24J, made to accommodate a single tail. It also featured improved nose and tail turrets. While 5168 B-24Ns were ordered, World War II ended and there was no longer any need for them. (Total: one)
YB-24N
Pre-production service test version of the XB-24N. (Total: seven)
XB-24P
A modified B-24D, made by Sperry Gyroscope Company to test airborne fire control systems. (Total: one converted B-24D)
XB-24Q
A General Electric conversion of the B-24L, using radar-controlled tail turrets. (Total: one converted B-24L).
XB-41
Because there were no fighters capable of escorting bomber formations on deep strike missions early in World War II, the Army authorized tests for heavily armed bombers to act as escorts for bombing missions. It was completed in 1942. The results of 1943 testing were very negative and the project was quickly cancelled. Performance changed drastically with the addition of more turrets. The escorts were also unable to keep up with bomber formations once the bombs had been dropped.
The XB-41 had 14, .50-caliber (12.7 mm) machine guns, through the addition of a Bendix chin turret and a dorsal Martin power turret on the mid-fuselage. (Total: one converted B-24D)
AT-22 or TB-24
C-87 used for flight engineer training.

* ;RB-24L: Developed for training B-29 gunners on an identical remote gun system installed on a B-24L.
* ;TB-24L: As with the RB-24L, but with additional radar equipment.

Experimental B-24J with B-17 nose section, containing chin turret, grafted on; modification not adopted for production.

C-87 Liberator Express
Passenger transports with accommodation for 20 passengers.

* ;C-87A: VIP transports with R-1830-45 instead of -43 engines and sleep accommodations for 16 passengers.
* ;C-87B: Projected armed transport variant with nose guns, dorsal turret, and ventral tunnel gun; never produced.
* ;C-87C: U.S. Army Air Force/Air Force designation for the RY-3.

XC-109/C-109
Tankers with specialized equipment to help prevent explosions, used to ferry fuel from India to China to support initial B-29 raids against Japan.
XF-7
Photographic reconnaissance variant developed from the B-24D.
F-7
Photographic reconnaissance variant developed from the B-24H; -FO block.
F-7A
Photographic reconnaissance variant developed from the B-24J; three cameras in the nose and three in the bomb bay.
F-7B
Photographic reconnaissance variant developed from the B-24J; six cameras in the bomb bay.

[edit] U.S. Navy nomenclature and sub-variants

PB4Y-1
B-24D with different nose turret for U.S. Navy. Designation later applied to all G, J, L and M models received by the U.S. Navy.[21]

* ;PB4Y-1P: Photographic reconnaissance variant developed from the PB4Y-1.

PB4Y-2 Privateer
See Main Article
RY-1
U.S. Navy designation for the C-87A.
RY-2
U.S. Navy designation for the C-87.
RY-3
Transport variant of the PB4Y-2.

[edit] British nomenclature and sub-variants
Rare color photograph of an LB-30A (YB-24) in RAF service

Liberator B Mk I
B-24A (Total: 20), direct purchase aircraft for the RAF. Consider unsuitable for combat, some rebuilt as the GR.1 and used in British anti-submarine patrol squadrons.
Liberator B Mk II
The first combat ready B-24. The modifications included a three foot nose extension as well as a deeper aft fuselage and wider tailplane–there was no direct B-24 equivalent but similar to the B-24C - built to meet British specifications with British equipment and armament. A small series of B Mk IIs were reconstructed as unarmed transports, designated the LB-30 with the USAAF. (Total production: 165)
Liberator B Mk III
B-24D variant with single .303 Browning machine gun in the nose, two in each beam position, and four in a Boulton Paul tail turret - similar to that on contemporay British heavy bombers such as the Lancaster - as well as other British equipment. The Martin dorsal turret was retained. (Total: 156)

* ;Liberator B Mk IIIA: Lend-Lease B-24Ds with American equipment and weapons.

Liberator B Mk IV
Reserved for the B-24E, but there is no record of the RAF actually receiving any.
Liberator B Mk V
B-24D modified for extra fuel capacity at the cost or armor, with the same armament fit as the Liberator Mk III.
Liberator B Mk VI
B-24Hs in RAF service fitted with Boulton Paul tail turrets, but retaining the rest of their armament.
Liberator B Mk VIII
RAF designation for B-24Js.
Liberator GR Mk V
B-24D modified by RAF Coastal Command for the anti-submarine role with search radar and Leigh Light. Some were fitted with eight zero-length rocket launchers, four on each wing.
Liberator GR Mk VI
B-24G/H/J type used as a long-range general reconnaissance aircraft by RAF Coastal Command.
Liberator GR Mk VIII
B-24J modified by RAF Coastal Command for the anti-submarine role.
Liberator C Mk VI
Liberator B Mk VIII converted for use as a transport.
Liberator C Mk VII
British designation for C-87.
Liberator C Mk VIII
Liberator G Mk VIII converted for use as a transport.
Liberator C Mk IX
RAF designation for the RY-3/C-87C



Download Paper Model
: Click Here

RADZIECKI SAMOLOT BOMBOVY IL-4

Military Papercraft

RADZIECKI SAMOLOT BOMBOVY IL-4


View full image please click on image

Download Paper Model : Click Here

typu KRONSZTAD

typu KRONSZTAD Paper Model


View full image please click on image

Download Paper Model : Click Here

Samolot akrobacyjny RWD-10

Samolot akrobacyjny RWD-10 Paper Model


View full image please click on image

Samolot akrobacyjny
Z Wikipedii
Brak wersji przejrzanej
Skocz do: nawigacji, szukaj

Samolot akrobacyjny - samolot, który dzięki swoim cechom konstrukcyjno-pilotażowym może wykonywać akrobację lotniczą i jest dopuszczony do wykonywania bądź tylko określonych figur akrobacji bądź do akrobacji pełnej (wszystkie figury akrobacji).

Samolot przeznaczony do wykonywania akrobacji z figurami generującymi jedynie przeciążenia dodatnie są zwane czasem samolotami półakrobacyjnymi, zaś te, które dopuszczają zakres przeciążeń od -10g do +12g - samolotami akrobacji pełnej (wyczynowej).

Zasadnicze cechy konstrukcyjne to:

* zwarta konstrukcja (małe momenty bezwładności)
* konstrukcja wytrzymała na przeciążenia zarówno dodatnie jak i ujemne
* duże powierzchnie sterowe warunkujące doskonałą sterowność
* stosunkowo małe obciążenie mocy (silnik o dość wysokiej mocy)

Zasadnicze cechy pilotażowe to:

* duża czułość sterów, szybka reakcja na sterowanie
* małe siły na sterach (znaczne odciążenie sterów)
* stosunkowo mała stateczność


The RWD-10 was a Polish aerobatics sports plane, single-seat parasol wing monoplane, used from 1933 to 1939 by the Polish aviation, constructed by the RWD team.

Development

The aircraft was designed as a single-seater aerobatic sports plane, that could also be used as a trainer for fighter aircraft pilots. The main designer was Jerzy Drzewiecki of the RWD construction team in the DWL (Doświadczalne Warsztaty Lotnicze) workshops. Its silhouette was similar to the RWD-8. The first prototype (registration SP-ALC), was flown in July 1933 by Drzewiecki. Its stability was not satisfactory, but after modifications, including lengthening a fuselage, it appeared a successful design and it completed state trials in 1935. In a mock dogfight with the PZL P.11c fighter, the RWD-10 kept on the P.11's tail. The first public aerobatics show of the RWD-10 took place during a Gordon Bennett Cup in ballooning in September 14-15, 1935 in Warsaw.

In 1936, a series of 20 aircraft was ordered by the LOPP paramilitary organization, funded by a public collection for aviation development. They were built in 1937 and then distributed among the Polish regional aero clubs - most (5) for Warsaw Aero Club. In 1938, another two were built. In total, approximately 22 serial RWD-10s were produced.

Three aircraft were crashed before the war, the rest were probably destroyed during the Invasion of Poland in 1939.

[edit] Description

Mixed construction single-engine single-seat braced high-wing (parasol wing) monoplane, conventional in layout. Fuselage of a steel frame, covered with canvas on a wooden frame, in aluminum in engine section. Straight double-trapezoid two-part wing, of wooden construction, covered with canvas and plywood in front, two-spar. The wing was supported by a central pyramid and twin struts. Wooden construction cantilever empennage, covered with plywood (stabilizers) and canvas (rudder and elevators). A pilot in an open cockpit, had a windshield. Conventional fixed landing gear, with a rear skid. Four-cylinder air-cooled inverted straight engine PZInż. Junior (licence built Walter Junior) with 82 kW (110 hp) nominal power and 90 kW (120 hp) take-off power. Two-blade wooden propeller Szomański, of a fixed pitch. Fuel tank in the fuselage: 54 l (fuel consumption 25 l/h).

[edit] Specifications (RWD-10)

Data from Glass, A. (1977)

General characteristics

* Crew: One, pilot
* Length: 6.2 m (20 ft 4 in)
* Wingspan: 7.5 m (24 ft 7 in)
* Height: 1.9 m (6 ft 3 in)
* Wing area: 9 m² (96.65 ft²)
* Empty weight: 350 kg (770 lb)
* Loaded weight: 475 kg (1,050 lb)
* Useful load: 125 kg (lb)
* Powerplant: 1× PZInż. Junior 4-cylinder air-cooled inverted straight engine, 120 hp (90 kW)

Performance

* Maximum speed: 218 km/h (135 mph)
* Cruise speed: 180 km/h (mph)
* Stall speed: 95 km/h (mph)
* Range: 360 km (224 mi)
* Service ceiling 6,000 m (19,680 ft)
* Rate of climb: 6.2 m/s, 372 m/min (1,220 ft/min)
* Wing loading: 53 kg/m² (10.9 lb/ft²)
* Take-off: 70 m
* Landing: 100 m

[edit] See also

Comparable aircraft

* Focke-Wulf Fw 56

[edit] References

* Glass, Andrzej: "Polskie konstrukcje lotnicze 1893-1939" (Polish aviation constructions 1893-1939), WKiŁ, Warsaw 1977, p. 308-311 (Polish)



Download Paper Model
: Click Here

Friday, February 6, 2009

HARVARD MK-IIB

HARVARD MK-IIB Paper Model


View full image please click on image

This article is about the first T-6 Texan. For the newer Beech aircraft, see T-6 Texan II.
T-6 Texan/SNJ/Harvard
Role Trainer aircraft
Manufacturer North American Aviation
First flight 1 April 1935
Number built 15,495
Variants CAC Wirraway

The T-6 Texan was a single-engine advanced trainer aircraft designed by North American Aviation, used to train fighter pilots of the United States Army Air Forces, United States Navy, Royal Air Force and other air forces of the British Commonwealth during World War II. The T-6 is known by a variety of designations depending on the model and operating air force. The USAAC called it the "AT-6", the US Navy, the "SNJ", and British Commonwealth air forces, the Harvard. It remains a popular warbird aircraft.



Development
Harvard under restoration exposing internal structure
WAVES washing a SNJ at NAS Jacksonville.
A SNJ-5 variant flying in an airshow in 2004.
RNZAF North American Harvards at Onerahi Aerodrome, near Whangarei, New Zealand in 1961.

The T-6 originated from the North American NA-16 prototype (first flown on April 1, 1935) which, modified as the NA-26, was submitted as an entry for a USAAC "Basic Combat" aircraft competition in March, 1937. The first model went in to production and 180 were supplied to the USAAC as the BC-1 and 400 to the RAF as the Harvard I. The US Navy received 16 modified aircraft, designated the SNJ-1, and a further 61 as the SNJ-2 with a different engine.

A further 92 BC-1A and three BC-2 aircraft were built before the shift to the "advanced trainer" designation, AT-6, which was equivalent to the BC-1A. The differences between the AT-6 and the BC-1 were new outer wing panels with a swept forward trailing edge, squared-off wingtips and a triangular rudder, producing the definitive Texan appearance. After a change to the rear of the canopy, the AT-6 was designated the Harvard II for RAF/RCAF orders and 1,173 were supplied by purchase or Lend Lease, mostly operating in Canada as part of the Empire Air Training Scheme.







Next came the AT-6A which was based on the NA-77 design and was powered by the Pratt & Whitney R-1340-49 Wasp radial engine. The USAAF received 1,549 and the US Navy 270 (as the SNJ-3). The AT-6B was built for gunnery training and could mount a .30 in machine gun on the forward fuselage. It utilised the R-1340-AN-1 engine which was to become the standard for the remaining T-6 production. Canada's Noorduyn Aviation built a R-1340-AN-1 powered version of the AT-6A which was supplied to the USAAF as the AT-16 (1,500 aircraft) and the RAF/RCAF as the Harvard IIB (2,485 aircraft), some of which also served with the Fleet Air Arm and Royal Canadian Navy.

In late 1937 Mitsubushi purchased two NA-16's as technology demonstrators and possibly a licence to build more. However the aircraft developed by Watanabe/Kyushu as the K10W1 (Allied code name Oak) bore no more than a superficial resemblance to the North American design. It featured a full monocoque fuselage as opposed to the steel tube fuselage of the T-6 and NA-16 family of aircraft, as well as being of smaller dimensions overall and had no design details in common with the T-6. It was used in very small numbers by the Imperial Japanese Navy from 1942 onwards. The IJA did not operate any, as they had other aircraft that they used for training. After the war the Japanese Air Self Defense Force operated Texans.

The NA-88 design resulted in 2,970 AT-6C Texans and 2,400 as the SNJ-4. The RAF received 726 of the AT-6C as the Harvard IIA. Modifications to the electrical system produced the AT-6D (3,713 produced) and SNJ-5 (1,357 produced). The AT-6D, redesignated the Harvard III, was supplied to the RAF (351 aircraft) and Fleet Air Arm (564 aircraft). Subsequently the NA-121 design with a completely clear rearmost section on the canopy, gave rise to 25 AT-6F Texans for the USAAF and 931, as the SNJ-6 for the US Navy. The ultimate version, the Harvard 4, was produced by Canada Car and Foundry during the 1950s, and supplied to the RCAF, USAF and Bundeswehr.

A total of 15,495 T-6s of all variants were built.

Operational history

During the Korean War and to a lesser extent, the Vietnam war, T-6s were pressed into service as forward air control aircraft. These aircraft were designated T-6 "Mosquito"s.[1] The RAF used the Harvard in Kenya against the Mau Mau in the 1950s where they operated with 20 lb bombs and machine guns against the gangs. Some operations took place at altitudes around 20,000 ft asl. A Harvard was the longest-serving RAF aeroplane, with an example, taken on strength in 1945, still serving in the 1990s (as a chase plane for helicopter test flights - a role the Shorts Tucano's high stall speed was ill-suited for). The T-6G was also used in a light attack or counter insurgency role by France during the Algerian war in special Escadrilles d'Aviation Légère d'Appui (EALA), armed with machine guns, bombs and rockets. At its peak there were 38 EALA's active. The largest unit was the Groupe d'Aviation Légère d'Appui 72, which consisted of up to 21 EALAs. Portugal also used ex-French aircraft during the Portuguese Colonial War.

Since the Second World War, the T-6 has been a regular participant at air shows, and was used in many movies. For example, in Tora! Tora! Tora! and The Final Countdown, converted single-seat T-6s painted in Japanese markings represent Mitsubishi Zeroes. The New Zealand Warbirds "Roaring 40s" aerobatic team use ex-Royal New Zealand Air Force Harvards. The Reno National Air Races also has a class specifically for the T-6 during the National Air Races each year.


Download Paper Model : Click Here

HMS DIDO

HMS DIDO Paper Model


View full image please click on image

HMS Dido was the name ship of her class of light cruisers for the Royal Navy. She was built by Cammell Laird Shipyard (Birkenhead, UK), with the keel being laid down on 26 October 1937. She was launched on 18 July 1939 and commissioned 30 September 1940.



History

After working up was completed early November 1940, Dido became a member of the 15th cruiser squadron deployed in blockading the approaches to the Bay of Biscay. This duty was designed to prevent raids by the German heavy cruiser Admiral Scheer. In March 1941 she provided cover for the successful commando raid on the Lofoten Islands (Operation Claymore).


A 20 mm Oerlikon gunner on board HMS Dido getting a light from a pal between bombing attacks in the eastern Mediterranean

Mediterranean

In April 1941, Dido was transferred to the Mediterranean, to reinforce the fleet based at Alexandria. During May she was involved in escorting convoys from Alexandria to Malta. On the 29th of that month, Dido and the cruiser HMS Orion were both badly damaged by German bombs after embarking troops from Sphakia and Heraklian in Crete. In June, she was a member of Rear Admiral Halifax's force. Halifax was Senior Officer Red Sea Force, tasked to capture the port of Asseb, and his fleet consisted of a transport ship, an armed merchant cruiser, and two Indian sloops. On the morning of 11 June, whilst still under cover of darkness, two motor boats, each carrying 30 men of the Punjab Regiment, went into the harbour under an umbrella of air bombardment, and the broadside from Dido.
A 20 mm Oerlikon gunner on board HMS Dido getting a light from a pal between bombing attacks in the eastern Mediterranean

The troops landed without a shot being fired at them, in fact two Italian Generals were captured in their pyjamas, by 0600 the Task Force entered Asseb, this was the last Italian occupied harbour in the Red Sea. In July 1941, the cruiser entered the Simonstown dockyard in South Africa for repairs, and was docked in the Selborne dry dock. After this she retired to Durban for more extensive repairs. On 15 August 1941 she set sail for the USA, and was refitted at the Brooklyn Navy Yard. By December 1941, the cruiser was back in the Mediterranean, where she was involved in escorting convoys from Alexandria to Malta.

During January-February 1942, Dido was escorting, and also used as a covering force for the Malta bound convoys. In March, Dido and her sister HMS Euryalus and six destroyers shelled the Island of Rhodes, on the 20th, Dido was employed as convoy escort to the commissioned auxiliary supply ship HMS Breconshire loaded with 5,000 tons of precious fuel, the SS Clan Campbell, the bomb damaged ship of the previous convoy, the Pampas and the Norwegian ship Talabot, fully loaded with ammunition. Getting this convoy through to Malta was afterwards referred to as the Second Battle of Sirte. Admiral Vian was in command of the operation. Of the total of 26,000 tons of stores carried by the four ships only 5,000 tons finally reached Malta.


Photograph taken from the destroyer USS MacKenzie during the successful bombardment of enemy batteries, dumps, and roads to the west of Gaeta, Italy carried out by HMS Dido in support of the army.


On 19 July 1942, Dido along with her sister ship HMS Euryalus and the destroyers HMS Jervis, HMS Javelin, HMS Pakenham and HMS Paladin shelled Mersa Matruh.

18 August 1942 Captain H. W. U. McCall brought Dido to Massawa for major repairs to a bomb-damaged stern. Because Dido was at that time one-quarter of British surface power in the Eastern Mediterranean it was critical that she be repaired as quickly as possible. The only working drydock in Massawa wasn't large enough to lift Dido entirely so she was partially floated up to clear the stern, leaving the bow low in the water. Six days later Dido was undocked to return to battle alongside her three sister ships, Euryalus, Cleopatra and Sirius. [2]

On 19 September, HMS Dido and once again the destroyers HMS Jervis, HMS Javelin, HMS Pakenham and HMS Paladin bombarded the Daba area in Egypt. In November 1942, HMS Dido, HMS Arethusa, HMS Euryalus and ten destroyers, proceeded from Alexandria to Malta with a supply convoy, despite many heavy German air attacks, the convoy of four supply ships reached Malta. With this the Island was regarded as relieved.
Photograph taken from the destroyer USS MacKenzie during the successful bombardment of enemy batteries, dumps, and roads to the west of Gaeta, Italy carried out by HMS Dido in support of the army.

In April 1943, Dido was based at Algiers but she left later for the UK for a much needed refit. In July she was back in the Mediterranean where she was part of the Reserve Covering Force for the Allied invasion of Sicily. During August she carried out the shelling of bridges in the Gulf of Eufemia in Calabria, in support of the 8th Army in Sicily. In September she was involved in the landing of the 1st British Airborne Division in Taranto.

[edit] Arctic

During January-March 1944, Dido was tasked in providing the support for the troops being landed at Anzio. During May-June, she bombarded targets in the Gulf of Gaeta, in support of the army. In August 1944, she supplied the fire support to the Allied landings on the French Mediterranean coast, between Cannes and Toulon. In October, she was sent up to the Arctic Ocean area to escort the convoys to Russia. During November, off Norway, Dido provided carrier escort for HMS Implacable which attacked a southbound German convoy in the Mosjoen area, north of the island of Namsos. In May 1945 Europe, Dido set sail for Copenhagen, where the German cruisers Prinz Eugen and Nürnberg lay surrendered, she escorted them to Wilhelmshaven.

During March-August 1946, Dido retained her fifth 5,25 inch turret in Q position while undergoing her refit. Although modern, this class of cruiser was regarded as being too cramped and insufficiently stable to receive new equipment. In September 1946, she joined the 2nd Cruiser Squadron. In October 1947, the cruiser was placed in reserve in the Gareloch. In 1951 Dido was moved to the Portsmouth Reserve Fleet. In November 1956 Dido and her sister ship HMS Cleopatra, which formed the Reserve Fleet flagship group, were replaced by the battleship HMS Vanguard. On 16 July 1958 Dido was broken up by Thomas W. Ward Ltd. at Barrow-in-Furness, Cumbria, England.

Dido’s badge can be seen displayed on the Selborne dry dock wall at Simonstown, South Africa.



Career (UK) Royal Navy Ensign
Class and type: Dido-class light cruiser
Name: HMS Dido
Builder: Cammell Laird Shipyard (Birkenhead, UK)
Laid down: 26 October 1937
Launched: 18 July 1939
Commissioned: 30 September 1940
Out of service: October 1947
Reclassified: In reserve at Gareloch between 1947 to 1951) and at Portsmouth between 1951 to 1958
Fate: Scrapped, Arrived at Thomas W Ward Ltd, Barrow-in-Furness UK on 18 July 1957.
General characteristics
Displacement: 5,600 tons standard
6,850 tons full load
Length: 485 ft (148 m) pp
512 ft (156 m) oa
Beam: 50.5 ft (15.4 m)
Draught: 14 ft (4.3 m)
Propulsion: Parsons geared turbines
Four shafts
Four Admiralty 3-drum boilers
62,000 shp (46 MW)
Speed: 32.25 knots (60 km/h)
Range: 2,414 km (1,500 miles) at 30 knots
6,824 km (4,240 miles) at 16 knots
1,100 tons fuel oil
Complement: 480
Sensors and
processing systems: Type 281 RADAR from September 1940[1]
Armament: Original configuration:
8x 5.25 in (133 mm) dual guns,
1x 4.0 in (102 mm) gun,
2x 0.5 in MG quadruple guns,
3x 2 pdr (37 mm/40 mm) pom-poms quad guns,
2x 21 in (533 mm) triple Torpedo Tubes. 1941 - 1943 configuration:
10x 5.25 in (133 mm) dual guns,
5x 20 mm (0.8 in) single guns,
3x 2 pdr (37 mm/40 mm) pom-poms quad guns,
2x 21 in (533 mm) triple Torpedo Tubes. 1943 - 1945 configuration:
10x 5.25 in (133 mm) dual guns,
2x 20 mm (0.8 in) single guns,
4x 20 mm (0.8 in) dual guns,
3x 2 pdr (37 mm/40 mm) pom-poms quad guns,
2x 21 in (533 mm) triple Torpedo Tubes.
Armor: Original configuration:
Belt: 3inch,
Deck: 1inch,
Magazines: 2inch,
Bulkheads: 1inch.
Notes: Pennant number 37



Download Paper Model : Click Here

PZL-130 ORLIK

PZL-130 ORLIK Paper Model


View full image please click on image

The PZL 130 Orlik (Spotted Eagle) is a Polish turboprop, single engine, two seat trainer.

Development
PZL-130 Orlik TC-I of Orlik Aerobatic Team


The Orlik was designed by PZL Warszawa-Okecie as a trainer for the Polish Air Force. It was also designed to meet the American FAR 23 standard. The project was under the supervision of Andrzej Frydrychewicz, head engineer of PZL Warszawa-Okecie. The aircraft was originally designed with the Russian Vedeneyev M-14Pm piston engine but, since PZL-130 was thought to have some attributes of a jet plane, it was replaced by a turboprop engine. The first prototype Orlik flew on the 24 October 1984. In 1986 the Turbo Orlik, with a Pratt & Whitney PT6A-25P turboprop engine was flown for the first time. It was later equipped with the Czech-built Walter M-601E turboprop engine.


Variants
PZL 130TC-1 #049

PZL-130 Orlik
The original aircraft with one Vedeneyev M-14Pm piston engine
PZL-130T Turbo Orlik
Variant with a Pratt & Whitney Canada PT6A-25P turboprop engine
PZL-130TM Orlik
Variant with a Walter M601E turboprop engine
PZL-130TB Orlik
Variant with a Walter M601T turboprop engine
PZL-130TC I Orlik
Variant with added Martin-Baker Mk.11, 0-0 class ejection seats and modernized avionics
PZL-130TC II Orlik
Variant with Pratt & Whitney Canada PT6A-25C turboprop, added winglets, modernized avionics and changed tutor's seat position
PZL-130TC III Orlik
Variant with modernized avionics (for example: added Head-Up Display)

Operators

Poland

* Polish Air Force

[edit] Specifications (PZL-130TC II Orlik)

General characteristics

* Crew: 2: student, instructor
* Length: 9.30 m ()
* Wingspan: 10.00 m ()
* Height: 3.53 m ()
* Wing area: 14.56 m² ()
* Empty weight: 1,825 kg ()
* Loaded weight: 2,400 kg ()
* Max takeoff weight: 2,950 kg ()
* Powerplant: 1× Pratt & Whitney Canada PT6A-25C turboprop, 750 hp ()

Performance

* Maximum speed: 501 km/h
* Range: 2,200 km ()


Download Paper Model : Click Here

Niszczyciel ORP PIORUN

Niszczyciel ORP PIORUN Paper Model


View full image please click on image


ORP Piorun - niszczyciel brytyjski typu N przekazany Polskiej Marynarce Wojennej w dniu 5 listopada 1940 w zamian za utracony pod Narwikiem niszczyciel ORP Grom. Zbudowany w stoczni John Brown w Clydebank w latach 1939-1940. Podczas wojny nosił oznaczenie taktyczne "G65". Wcześniej HMS Nerissa.

W maju 1941 brał udział w poszukiwaniach niemieckiego pancernika "Bismarck", podczas których wsławił się odnalezieniem "Bismarcka" i nawiązaniem z nim kontaktu bojowego w nocy 26 maja 1941. Około jednej godziny, od 22.37 do 23.50 polski okręt manewrował w zasięgu widzialności pancernika, który go niecelnie ostrzeliwał. "Piorun" oddał również trzy niecelne salwy, o znaczeniu raczej symbolicznym (nie mogły one wyrządzić poważniejszych szkód). Od września 1941 do początku 1943 brał udział w eskortowaniu konwojów na Oceanie Atlantyckim i Morzu Śródziemnym. Od lipca do listopada 1943 uczestniczył w wielu operacjach u brzegów Sycylii. W czerwcu 1944 brał udział w inwazji w Normandii oraz w bitwach morskich pod Ouessant (9 czerwca) i Jersey (14 czerwca).

Piorun został zwrócony Wielkiej Brytanii w dniu 28 września 1946 roku.

Dowódcy:

* komandor Eugeniusz Pławski
* komandor podporucznik Tadeusz Gorazdowski
* komandor porucznik Stanisław Dzienisiewicz
* komandor podporucznik Jan Tchórznicki
* komandor podporucznik Wszechwład Maracewicz

Załogę okrętu stanowiła w większości uratowana część załogi Groma. Od 12 lutego 1945 r. służył na okręcie por. Mar. Zbigniew Plezia, awansowany na tym okręcie do stopnia kapitana.

ORP Piorun

ORP Piorun po powrocie do Plymouth
Historia
Oddanie do służby 5 listopada 1940
Wycofanie ze służby 1946
Status okrętu złomowany w 1955
Stocznia stocznia John Brown, Clydebank, Wielka Brytania
Wcześniejsza nazwa HMS Nerissa
Następna nazwa HMS Noble
Dane taktyczno-techniczne
Wyporność standardowa - 1773 t
pełna - 2384 t
Długość 112 m
Szerokość 10,7 m
Zanurzenie 3 m
Napęd moc: 40 000 KM
Prędkość 36 węzłów
Załoga 200 marynarzy i oficerów
Uzbrojenie 6 dział 120 mm,
1 działo plot 102 mm,
4 działka plot 40 mm,
2 działka plot 20 mm,
5 wyrzutni torped 533 mm,
4 miotacze bomb głębinowych,
2 wyrzutnie bomb głębinowych


Download Paper Model: Click Here