Junkers Ju 188 - Citizendia

Junkers Ju 188

Type	Tactical bomber/Reconnaissance aircraft
Manufacturer	Junkers
Maiden flight	1940 (Ju 88B V1)
Introduced	February 1943
Retired	1951 (France)
Primary users	Germany France (post-war)
Number built	1,234
Developed from	Junkers Ju 88
Variants	Junkers Ju 388

The Ju 188 was a German World War II high-performance medium bomber from Junkers, the planned follow-on to the famed Ju 88 with better performance and payload. An aerospace manufacturer is a company or individual involved in the various aspects of designing building testing selling and maintaining Aircraft, Aircraft parts The maiden flight of an Aircraft is the first occasion on which an aircraft leaves the ground of its own accord This is a list of Aviation -related events from 1940: Events January January 6 - During the Winter War between This is a list of Aviation -related events from 1943: Events January January 27 - the USAAF makes its first This is a list of Aviation -related events from 1951: Events February February 21 - an English Electric Canberra Germany, officially the Federal Republic of Germany ( ˈbʊndəsʁepuˌbliːk ˈdɔʏtʃlant is a Country in Central Europe. This article is about the country For a topic outline on this subject see List of basic France topics. WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout The Junkers Ju 388 Störtebeker was a World War II Heavy fighter based on the Ju 88 airframe by way of the Ju Germany, officially the Federal Republic of Germany ( ˈbʊndəsʁepuˌbliːk ˈdɔʏtʃlant is a Country in Central Europe. World War II, or the Second World War, (often abbreviated WWII) was a global military conflict which involved a majority of the world's nations, including A medium bomber is a Bomber aircraft designed to operate with medium bombloads over medium distances primarily to distinguish them from the much larger Heavy bombers WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout It was produced only in limited numbers, due both to the presence of improved versions of the Ju 88, as well as the deteriorating war condition and the resulting focus on fighter production.

1 Background
2 Prototypes, Ju 88 B-0
3 Ju 188
4 High-altitude versions
5 Operators
6 Specifications (Ju 188E)
7 See also

Background

In 1936 Junkers submitted proposals for the Ju 85 and Ju 88 into competition for the new standardized Luftwaffe high-speed tactical bomber, known as the Schnellbomber. WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout ( German 'luftvafe is a generic German term for an Air force. The two designs were almost identical, differing only in that the Ju 85 used a twin-rudder and the Ju 88 a single fin. At the same time they offered modified versions of each as the Ju 85B and Ju 88B, again similar to the original designs, but using an "egg shaped" forward fuselage that was essentially one large window, another example of the "bullet-nose" design philosophy that almost all new German bomber designs exhibited from the time of the Heinkel He 111P onwards. WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout The new design offered somewhat lower drag, and better visibility. At the time this was considered too radical, and eventually the Ju 88A with its simpler fighter-like "stepped" cockpit won the contest.

By 1939 the original Ju 88 had itself evolved with considerably more window area, but in a fashion that was not well streamlined. The Reich Air Ministry (RLM) was in the process of ordering a "second generation" bomber in a project known as Bomber B, but this was extensively delayed due to the non-delivery of the large 2,500 PS (2,466 hp, 1,839 kW) class engines, like Junkers' own Jumo 222 engine, that the designs would rely on. The Reich Air Ministry (Reichsluftfahrtministerium was a government department during the period of Nazi Germany (1933-45 Bomber B was a German project dating to just before the start of World War II to develop a second-generation high-speed Bomber that would replace all medium WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout Although Junker's own Ju 288 was currently leading the contest, there was no delivery date on the engines and the Ju 88B project was re-submitted as a stop-gap measure. The Junkers Ju 288 was a German Bomber aircraft project designed during World War II, but which only ever flew in prototype form For this version they used the latest Ju 88 A-1 airframe as a baseline, but added the new Junkers Jumo 213 engine, which had recently started bench testing and was expected to deliver 1,500 PS (1,479 hp, 1,103 kW). WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout

The RLM wasn't impressed with the new design, as it offered only small improvements over the existing Ju 88A's then in service. However they did suggest that Junkers continue with the prototype work anyway, but asked that they consider fitting the design with the BMW 139 radial engine instead. The radial engine is a reciprocating type internal combustion Engine configuration in which the cylinders point outward from a central This engine was cancelled only a few weeks later, and all designs based on it moved to the newer and more powerful BMW 801. WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout

Prototypes, Ju 88 B-0

The prototype Ju 88B V1, D-AUVS, flew for the first time with the 801A/B engines in early 1940. The fuselage was identical to the Ju 88 A-1, which presented a problem: with the extra power, 1,560 PS (1,539 hp, 1,147 kW), the design could now carry considerably more load than the small bomb bay could fit. An additional external shackle was then added to each wing well outside the engines, although using the rack would seriously hamper performance.

During the summer a pre-production run of ten Ju 88 B-0 based on the pre-production Ju 88 A-4 airframes were delivered. The A-4 used a longer wing for better altitude performance, just over 65 feet (20 m) as opposed to the 60 foot (18 m) span of the earlier A-series, but attention to streamlining and new "pointy" wing tips kept drag to about what it was earlier. The airframe changes moved the center of gravity slightly, so the glazed "cockpit" area was made slightly longer to re-balance the aircraft, while also offering better visibility for other members of the crew.

Service tests were all successful, and the pilots generally lauded the new cockpit design. However the RLM still remained unconvinced that the small improvement in performance over the existing A-5's and future A-4's was worth investing time in. Instead the pre-production models were modified as long-range reconnaissance aircraft by removing the guns, bombsights and external bomb shackles, and fitting fuel tanks into the bomb bay. Reconnaissance (also scouting) is a military and medical term denoting exploration conducted to gain information

Several of the airframes were retained by Junkers for further development. One of these was fitted with the slightly updated 801L engines and a small power-operated turret on the extreme top of the cockpit mounting a MG 131 machine gun. The MG 131 (shortened from German: Maschinengewehr 131, or "Machine gun 131" was a 13 mm Machine gun developed in 1938

Ju 188

By 1942 it was becoming clear that the Ju 288 wasn't going to be ready any time soon, and at the same time the Ju 88's were increasingly at the mercy of a rapidly improving RAF and Soviet VVS. The Union of Soviet Socialist Republics (USSR was a constitutionally Socialist state that existed in Eurasia from 1922 to 1991 The RLM finally decided that even the small gains in performance in the Ju 88B were worth considering, and asked Junkers for a series of upgrades as the Ju 188.

The sole Ju 88 E-0 was modified with several additional guns, another MG 131 firing rearward just below the turret, one firing forward through the nose, and the twinned MG 81Z in the ventral bulge firing rearward. The MG 81 was a belt fed 792 mm Machine gun for fixed or flexible installations in World War II Luftwaffe aircraft replacing the older Two other airframes had their engines and outer wings removed to act as testbeds for water ditching, as it was planned to use the Ju 188 in long overwater flights against British shipping. A second Ju 188 test airframe was also built up from another Ju 88 A-4, this one including a larger, more trapezoidal vertical tail surface set to provide more directional control at higher altitudes, a feature also used on future Ju 88 models, such as the Ju 88G night fighters. Originally known as Ju 88 V44, this airframe was later designated Ju 188 V1.

October 1942 the program was given the go-ahead to start planning for production. A second prototype was delivered in January, which moved the outer bomb shackles to a position inboard of the engines. Both started testing the dive bombing system installed in the 88 A-4 in February. The RLM then asked for another change, allowing the aircraft to mount either the BMW 801 or Jumo 213 engines as a complete "power egg", or Kraftei, that would simply be bolted on and hooked up. Concerns about the Jumo 213, now years overdue, were offset by this engine's better altitude performance, so it made sense to delay the aircraft slightly if that meant it could switch to the 213 as soon as they became available. The second Ju 188 V1 prototype was flown in 1943.

Ju 188 A & E

The Ju 188 was designed to be fitted with either the 1,750 PS (1,726 hp, 1,287 kW) Jumo 213A or 1,700 PS (1,677 hp, 1,250 kW) BMW 801G engines without any changes to the airframe. WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout It was originally intended that both would be known as A models, but the naming was later changed: the Ju 188A model powered by the 213, and the Ju 188E by the 801.

The first three production Ju 188 E-1 machines were delivered with the BMW engines in February 1943, another seven in March, and eight in April. A conversion testing unit was formed up in May, and after testing were attached to an operational unit. By the end of the year 283 aircraft had been delivered, and two new factories were added to the production effort. Most operational machines differed from the prototypes only in having a 20 mm MG151/20 cannon in the nose and dorsal turrets in place of the 13 mm MG 131. The Ju 188 E-2 was built as a torpedo-bomber.

Although the A and E models were to have been delivered at the same time, the Jumo engine was still having difficulties getting into production. Nevertheless the first Jumo powered Ju 188 A-1 versions were shipped only shortly after the BMW versions, albeit at a much slower rate. By the time delivery rates were finally picking up in late 1943 the Jumo was available in a new MW50 methanol-water injection "boosted" version that delivered 2,100 PS (2,071 hp, 1,545 kW) for takeoff. MW 50 was a 50-50 mixture of Methanol and Water (hence the name that was sprayed into the Supercharger of World War II German Aircraft With this engine the plaers were known as the Ju 188 A-2, and started deliveries in early 1944.

A modified version mounting a small FuG 200 Hohentwiel sea-search radar set under the nose and shackles for a torpedo for naval strike missions was delivered as the Ju 188 E-2, and with the Jumo as the Ju 188 A-3. Radar is a system that uses electromagnetic waves to identify the range altitude direction or speed of both moving and fixed objects such as Aircraft, ships The modern torpedo (historically called an automotive automobile locomotive or fish torpedo is a self-propelled explosive Projectile weapon launched above or below The only other difference was the removal of the outer pair of wing bomb shackles.

For all its good points, the Ju 188 was only a small improvement over the Ju 88 it was supposed to replace. The bombload and bomb-bay was no larger than the earlier plane, so although it could handle a larger load by mounting externally, doing so hurt performance. Even then the performance was rather poor considering all the effort – only 325 mph (523 km/h) or less. One has to wonder about the German armament designers as well, the fancy dorsal turret had only one gun in it, yet they retained the single-gun flexible position only a few centimeters away from it. In the meantime the various projects to finally provide the plane with real tail armament were all abandoned.

Delivery problems of the Jumo were never entirely sorted out, and the only model to be built in large numbers were the E series with the BMW 801. Even then so few were available that they were generally given out to Ju 88 units, who flew them on "special" missions where the longer range or better performance would be helpful.

Ju 188C

It was planned all along to skip over a "B model" to avoid confusion with the original Ju 88B, but in the original planning the A and E models would both be called A's. The Ju 188C would thus be the next model in line.

The C series was built to the extent of a single example, by modifying one of the few A-1 machines. To this they added the new power-operated FA 15 turret in the tail. The turret mounted two 13 mm MG 131 machine guns, aimed with a double-periscope (top and bottom) system mounted in the cockpit. For other uses of the phrase see Machine Gun (disambiguation.

This modification would have greatly improved defensive firepower, always lacking on German designs, but reliability was so poor it was decided to abandon the system.

Ju 188 D & F

In early 1944 it was decided to focus on reconnaissance versions of the A and E models The airframe was modified with the removal of the bomb aimer and the forward gun, and additional fuel cells were added to extend the range to 2,110 miles (3,400 km). The Ju 188 D-1 was otherwise similar to the A-1, and the Ju 188 D-2 fitted nose radar for naval reconnaissance. Similar conversions of the E models were the Ju 188 F-1 and Ju 188 F-2.

Ju 188 G & H

One problem with the Ju 88 that carried into the 188 was the lack of internal room for bomb storage. Both carried the majority of their bombload on the outside of the plane on racks under the wing, where it greatly affected performance. This was to have been addressed in the G and H models, which extended the fuselage downward for more room with the addition of a wooden pannier.

This modification also left enough room at the tail to fit a manned turret in place of the C model's remote-control one. However this system proved to be just as limited as the remote-control FA 15, being so small that only gunners could fit into it, and had basically no ability to escape in an emergency. The RLM rejected the design and planned on mounting the FA 15 even if it were unreliable. Oddly, the designs still had the nose area extended under the plane for a rear gunner, when this would no longer be needed and its removal would have greatly cleaned up the lines of the plane.

With the Jumo 213s now being sent to fighter production, the Ju 188 G-2 was to use the BMW 801 only, with the reconnaissance conversion known as the Ju 188 H-2. Neither entered production before the war ended.

Ju 188R

In the summer of 1944 three E models were modified as night fighters with the addition of radar and either four 20 mm MG 151/20s or two 30 mm MK 103s in the nose. A night fighter (also all-weather fighter) is a Fighter aircraft adapted for use at night or in other times of bad visibility However the added visibility of the 188 was not useful in the night role, and as the added drag of the radar washed out any speed difference, so the Ju 188 R-0 was not ordered.

High-altitude versions

In 1943 it was planned to upgrade the entire lineup with even more wing area and a pressurized cockpit for high-altitude work. A single basic airframe would be offered in three versions, the Ju 188J heavy fighter, Ju 188K bomber, and the Ju 188L reconnaissance version. A heavy fighter is a Fighter aircraft designed to carry heavier weapons or operate at longer ranges All three did away with the under-slung gunner's compartment, leading to a cleaner nose profile, and the bomber and recce versions mounted their loads in a long pannier under the middle of the plane instead of the deeper fuselage of the G and H models.

Simpler versions of these with no defensive armament and even longer wings became the Ju 188S fighter and Ju 188T intruder. With Jumo 213 E-1 engines 2,050 PS (2,022 hp, 1,508 kW) at take-off and 1,690 PS (1,667 hp, 1,243 kW) at 9,500 m (31,400 ft), the Ju 188T could reach 700 km/h (435 mph). Operating at this altitude, the Ju 188S could carry only 800 kg of bombs.

Before any of these could start production, the entire lineup was renamed the Ju 388, the vastly improved performance warranting this change in name. The Junkers Ju 388 Störtebeker was a World War II Heavy fighter based on the Ju 88 airframe by way of the Ju

Operators

France

Aviation Navale operated several captured Ju 188 post war. This article is about the country For a topic outline on this subject see List of basic France topics. The Aviation navale ( Naval aviation) of the French Navy includes 162 airplanes (138 of them combat-capable and 6800 men both civilians and military personnel

Germany

Luftwaffe

Specifications (Ju 188E)

General characteristics

Crew: 5
Length: 15 m (49 ft 1 in)
Wingspan: 22 m (72 ft 2 in)
Height: 4. Nazi Germany and the Third Reich are the common English names for Germany under the regime of Adolf Hitler and the National Socialist German Workers ( German 'luftvafe is a generic German term for an Air force. The wingspan (or just span) of an airplane or a Bird, is the distance from the left wingtip to the right wingtip 4 m (14 ft 7 in)
Wing area: 56 m² (603 ft²)
Empty weight: 9,900 kg (21,825 lb)
Loaded weight: 14,500 kg (31,967 lb)
Powerplant: 2× 1 BMW 801 G-2, 1,250 kW (1,700 PS) each

Performance

Maximum speed: 499 km/h (310 mph)
Range: 2,190 km combat (1,360 miles)
Service ceiling 9,500 m (31,170 ft)
Wing loading: 258. WikipediaWikiProject Aircraft. Please see WikipediaWikiProject Aircraft/page content for recommended layout In Aviation, V-speeds or Velocity-speeds are standard terms used to define Airspeeds important or useful to the operation of Aircraft, such The maximal total range is the distance an Aircraft can fly between Takeoff and Landing, as limited by fuel capacity in powered aircraft or cross-country In Aeronautics, a ceiling is the maximum Density altitude an aircraft can reach under a set of conditions In Aerodynamics, wing loading is the loaded weight of the aircraft divided by the area of the wing 9 kg/m² (53. 0 lb/ft²)
Power/mass: 0. Power-to-weight ratio (specific power is a calculation commonly applied to Engines and other mobile power sources to enable the comparison of one unit or design to another 175 kW/kg (0. 106 hp/lb)

Armament

Guns:
- 1 × MG 151 20 mm cannon
- 3 × MG 131 13 mm machine gun
Bombs:
- 3,000 kg (6,600 lbs)

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