Monthly Archives: November 2018

Cargo

Consolidated RY-3 “Liberator (Privateer) Express”, (Matchbox)

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TYPE: Personal and cargo transport

ACCOMMODATION: Crew of four plus 25 troops or up to 4,500 kg cargo

POWER PLANT: Four Pratt & Whitney R-1820-94 radial engines with General Electric turbo-superchargers, rated at 1,350 hp each

PERFORMANCE: 300 mph at 25,000 ft

COMMENT: The Consolidated RY-3 was a troop and cargo transport aircraft built for the United States Navy on the basis of the patrol bomber Convair PB4Y-2 “Privateer”. This, on the other hand, was a US Navy derivative of the famous USAAF Consolidated B-24 “Liberator” heavy bomber.
In 1942, an urgent need was recognized for a heavy cargo and personnel transport with longer range and better high-altitude performance than the Douglas C-47 “Skytrain”, the most widely available USAAF transport aircraft at the time. So the Consolidated Aircraft Company hastily designed a cargo and transport variant of the “Liberator” bomber under the designation Consolidated C-87 “Liberator Express”. Production began in 1942 and a total of 287 C-87s were built alongside the B-24 at the Consolidated Aircraft plant in Fort Worth, Texas. The C-87 could be fitted with removable seats and racks to carry personnel or litters in place of cargo. In its final configuration, the C-87 could carry between 20 and 25 passengers or 4,500 kg of cargo. Because of war production bottlenecks and shortages, many C-87 aircraft were fitted with turbo-superchargers producing lower boost pressure and power than those fitted to B-24s destined for combat use, and ceiling and climb rate were accordingly adversely affected.
Despite its shortcomings and unpopularity among its crews, the C-87 was valued for the reliability of its Pratt & Whitney engines, superior speed that enabled it to mitigate significantly the effect of head and cross winds, a service ceiling that allowed it to surmount most weather fronts, and range that permitted its crews to fly “pressure-front” patterns that chased favorable winds. The C-87 was never fully displaced on the air routes by the Douglas C-54 “Skymaster” and Curtiss C-46 “Commando”, which offered similar performance combined with greater reliability and more benign flight characteristics.
One of the last developments of the basic USAAF Consolidated B-24 “Liberator” bomber design was a Navy contracted, single tail version with an extended fuselage. Built in San Diego its USN designation was Consolidated PB4Y-2 “Privateer” and the aircraft’ design based on the Consolidated PB4Y-1, the US Navy version of the B-24 “Liberator”.
The “Privateer” was externally similar to the “Liberator”, but the fuselage was longer, and had a tall single vertical stabilizer rather than the PB4Y-1’s twin tail configuration. The single vertical tail was adopted from the USAAF’s canceled B-24N design (and was slightly taller on the “Privateer”) because it would increase stability at low to medium altitudes for maritime patrol.
39 out of totally built 739 „Privateers“ were converted for transport duties as Consolidated RY-3, and were used by the RAF Transport Command No. 231 Squadron, U.S. Marine Corps, and one was used by the RCAF (Ref.: 24).

Heavy Bomber, Projects

Messerschmitt Me P.1108/I “Fernbomber“ with fuselage (Antares Models, Resin)

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TYPE: Long-range turbojet bomber. Project

ACCOMMODATION: Crew of two

POWER PLANT: Four Heinkel/Hirth HeS 011 turbojet engines, rated at 1,200 kp each

PERFORMANCE: 528 mph

COMMENT: In January/February 1945, only four month before the German “Third Reich” surrendered, Messerschmitt proposed two designs of a “Fernbomber” (Long-distant range/long-range bomber), the Me P.1108/I and –II. Although no post-war information provided by Messerschmitt’s employees could be independently verified, since all data had already been removed by the French it seems that both projects were designed by Dr. Wurster from Messerschmitt to a concept by Dr. Alexander Lippisch.
While the Messerschmitt Me P.1108/I, (design drawing Nr. IX-126 from 28th February, 1945) was a more conventional design with a fuselage, 35 degree back-swept wings and a butterfly-type tailplane, the Me P.1108/II (design drawing Nr.117 from January 12th, 1945) was a flying wing concept with 40 degrees sweep of the leading edge without any tailplane. Common to both projects were the installation of four Heinkel/Hirth HeS 011 turbojet engines, the air intakes were under the wings or in the wings leading edge. Calculated fully loaded weight was to be 30 tons, a range of 4,300 mi at a speed of 500–530 mph and a height of 30,000–39,000 ft. was estimated.
The Messerschmitt Me P.1108/I design had an aerodynamic clear fuselage with circular cross section and low positioned swept back wing with four He S 011 turbojet engines in paired nacelles half-embedded in the wing trailing edge. These were fed by a common intake on each lower wing surface. A two man crew sat in tandem position in a pressurized cockpit in the extreme nose of the aircraft. A tricycle landing gear arrangement was designed, with the main wheels retracting into the fuselage. It was planned that the armament of the production aircraft should consist of three twin 20mm cannon turrets, two located on the back of the fuselage and aft of the cockpit and one under the fuselage. All were remotely controlled from the cockpit.
Understandably, at the end of March 1945, only few weeks before the total collapse of the “Third Reich” Messerschmitt was ordered by the RLM to cease all development on long range bomber designs (Ref.: 15, 20).

Fighter-Torpedobomber

Aichi B7A1 ‘Ryusei’ (“Shooting Star”, “Grace”), (Fujimi Models)

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TYPE: Carrier-borne torpedo- and dive bomber

ACCOMMODATION: Crew of two

POWER PLANT: One Nakajima NK9B “Homare 11” radial engine, rated at 1,560 hp at 21,000 ft

PERFORMANCE: 367 mph

COMMENT: The Aichi B7A “Ryusei” (“Shooting Star”, Allied reporting name “Grace”) was a large and powerful carrier-borne torpedo-dive bomber produced by Aichi Kokuki KK for the Imperial Japanese Navy Air Service during the Second World War. Built in only small numbers and deprived of the aircraft carriers it was intended to operate from, the type had little chance to distinguish itself in combat before the war ended in August 1945.
The B7A “Ryusei” (originally designated AM-23 by Aichi) was designed in response to a 1941 16-Shi requirement issued by the Imperial Japanese Navy Air Service for a carrier attack bomber that would replace both the Nakajima B6N “Tenzan” torpedo plane and the Yokosuka D4Y “Suisei” dive bomber in IJN service. It was intended for use aboard a new generation of “Taihō”-class aircraft carriers, the first of which was laid down in July 1941. Because the deck elevators on the “Taihōs” had a larger square area than those of older Japanese carriers, the longstanding maximum limit of 11 m (36 ft) on carrier aircraft length could now be lifted.
The Aichi’s designers chose a mid-wing arrangement for the B7A to provide for an internal bomb-bay and to ensure enough clearance for the plane’s 3.5 m four-bladed propeller. This in turn necessitated the adoption of an inverted gull wing, reminiscent of the Vought F4U “Corsair”, in order to shorten the length of the main landing gear. The wing featured extendable ailerons with a ten-degree range of deflection, enabling them to act as auxiliary flaps. Dive brakes were fitted underneath just outboard of the fuselage. The B7A’s outer wing panels were designed to fold upwards hydraulically for carrier stowage, reducing its overall span from 14.4 m to approximately 7.9 m.
Selection of a power plant was dictated by the Japanese Navy which requested that Aichi design the aircraft around the 1,825 hp Nakajima NK9C “Homare 12” 18-cylinder two-row air-cooled radial engine. This was expected to become the Navy’s standard aircraft engine in the 1,800 hp to 2,200 hp range.  The B7A had a weight-carrying capacity stemming from its requirements, resulting in a weapons load no greater than its predecessors. The presence of an internal bomb bay with two high-load-capability attachment points allowed the aircraft to carry two 250 kg or six 60 kg bombs. Alternatively, it could carry a single externally mounted Type 91 torpedo, weighing up to 848 kg.
Defensive armament initially consisted of two 20mm Type 99 Model 2 cannons in the wing roots and one flexible 7.92mm Type 1 machine-gun mounted in the rear cockpit. Later production models of the B7A2 featured a 13mm Type 2 machine-gun in place of the 7.92mm gun.
Despite the plane’s weight and size, it displayed fighter-like handling and performance, besting the version of the Mitsubishi A6M “Zero” in service at the time. It was fast and highly maneuverable.
Given the codename “Grace” by the Allies, the B7A1 first flew as a prototype in May 1942, but teething problems with the experimental NK9C “Homare” engine and necessary modifications to the airframe meant that the type did not enter into production until two years later in May 1944. Nine prototype B7A1s (the second prototype is shown here)  were built and were progressively modified to eradicate minor airframe and equipment problems.
In April 1944 an improved engine version, the 1,825 hp “Homare 12”, became available and powered by this engine the aircraft was finally placed in production as the Aichi B7A2 “Ryusei” (Ref.: 24).