Junkers Ju 388
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The Junkers Ju 388 StĂ¶rtebeker was a World War II German Luftwaffe multi-role aircraft based on the Ju 88 airframe by way of the Ju 188. It differed from its predecessors in being intended for high altitude operation, with design features such as a pressurized cockpit for its crew. The Ju 388 was introduced very late in the war, and production problems along with the deteriorating war conditions meant that few were built.
The Reich Air Ministry (RLM) first learned of the American B-29 Superfortress heavy bomber in late 1942. these concerns were heightened in early 1944, when YB-29 "Hobo Queen" made a well- publicised appearance at RAF Bovingdon, which had made a headline photo appearance in a news article in the VĂ¶lkischer Beobachter newspaper. The performance estimates of this aircraft were cause for great concern in the Luftwaffe. The B-29 had a maximum speed of around 560 km/h (348 mph), and would attack in a cruise at about 360 km/h (224 mph) at 8,000-10,000 m (26,247-32,810 ft), an altitude where no current Luftwaffe aircraft was effective.
To counter the B-29, the Luftwaffe would need new day fighters and bomber destroyers with greatly enhanced performance at extreme altitude. The fighter chosen was the Focke-Wulf Ta 152H. This was based on the Fw 190D with longer wings and the new high-altitude "E" model of the Junkers Jumo 213 engine. An alternative was the Messerschmitt Me 155B, a long-winged development of the Bf 109 which had already undergone several stages of design and would ultimately be built in prototype form by Blohm & Voss. The centre-line thrust twin Dornier Do 335, powered with two of the competing Daimler-Benz DB 603 engines also offered a service ceiling of some 11,400 m (37,500 ft), but the promising Dornier heavy fighter and ZerstĂ¶rer was still under development solely with prototype airframes flying, and the first production examples expected to enter operational service late in 1944.
For the bomber destroyer and night fighter roles, the Ta 154 and Heinkel He 219 had the performance needed to catch the bomber; but each of those designs only gained that performance by mounting short wings which were inadequate for flight at high altitude. The Junkers Ju 88 had already been modified for high-altitude use as the S and T models, but these did not have the performance needed. Similar high-altitude modifications to the Ju 188 were being looked at as the projected Ju 188J, K and L models, which included a now nearly-standard "stepless" pressurized cockpit that fully enclosed the entire nose, and wing and elevator deicing equipment for extended flights at very high altitude. These were selected for development, and renamed Ju 388.
In order to improve performance, the Ju 388 was stripped of almost all defensive armament. Whereas the Ju 88 included a number of hand-swung guns in ports all over the cockpit area, on the Ju 388 they were replaced by a single remote-control turret in the tail containing two 13 mm (.51 in) MG 131 machine guns, aimed via a periscope in the cockpit. The turret had an excellent field of fire and could shoot directly to the rear, so the gunner's Bola streamlined casemate-style ventral defensive armament emplacement beneath the nose of Ju 88s and 188s was omitted, improving the aerodynamics.
The aircraft was to be delivered using the same naming as the three original Ju 188 experimental versions: the J, K, and L. The J model was a fighter with two 30 mm (1.18 in) MK 103 cannons and two 20 mm MG 151/20 cannons in a solid nose for use as a daytime bomber destroyer. For use as a night fighter, the long-barreled MK 103s were replaced by the smaller and lighter 30 mm MK 108s, while a second pair of dorsal-mount, upward firing MK 108s were added in a SchrĂ€ge Musik installation behind the cockpit. The K model was a pure bomber, with a pannier under the plane increasing the size of the bomb bay. The L photo-reconnaissance model put its cameras in the pannier along with additional fuel tanks for long-range missions.
Three sub-models of each variant were planned, different only in the engine installation. The -1 would mount the BMW 801J, a turbocharged version of the basic BMW 801 air cooled radial, each engine installed as a unitized Triebswerkanlage engine installation format. The -2 would use the 46.4 litre displacement, 1,864 kW (2,500 hp) Jumo 222A/B 24-cylinder six-bank liquid-cooled engines (the B engine model rotated in the opposite direction of the A model, but was otherwise identical), or the identical displacement 222E/F versions with an improved two-speed supercharger with triple intercoolers on each engine. The -3 would mount the Junkers Jumo 213E liquid cooled inverted V12, which included a supercharger similar to the 222E/F's. Since the 24-cylinder Jumo 222 engine was destined never to emerge beyond development and testing with just under 300 units ever built, the only powerplants actually used for the Ju 388 would be the BMW 801 radial and Jumo 213 series V12s. The Triebswerkanlage designation for the unitized turbocharged BMW 801J radials, meant to be designated with a "T" after the RLM engine type number of "801", led to them being misdesignated as "BMW 801TJ" engines for years in post-war World War II aviation history reference books.
With the BMW 801J or Jumo 213E, the fighter versions flew at 616 km/h (383 mph) when equipped as a destroyer, losing about 25 km/h (16 mph) to the eight-dipole Hirschgeweih antenna array used for late-war, VHF-band German AI radar and SchrĂ€ge Musik when equipped as night fighters. This was similar in speed to existing Luftwaffe night fighters, but the Ju 388 maintained this speed at much higher altitudes. With the Jumo 222 engine, the aircraft was estimated to be capable of reaching around 700 km/h (435 mph), again losing about 25 km/h (16 mph) in night fighter versions. The bomber versions flew at roughly the same speeds depending on bombload, while the reconnaissance versions would have been about 25 km/h (16 mph) faster.
The first prototype, Ju 388 L-0/V7, mainly built from Ju 188 series production components, made its first flight on December 22, 1943. It demonstrated much better handling at altitude than the Ju 88S due to an increase in tail surface area, as the streamlined-nose Ju 88S, also omitting the Bola gondola, still used the original Ju 88A vertical tail surface design. This was followed by six new prototypes. It was some time before deliveries of the production models started due to engine delivery delays. By the time the engines were widely available, it was clear that B-29 bombers were being sent to the Pacific and would not be operating over Germany anytime soon. German photo-reconnaissance efforts had practically disappeared due to the increased performance of the Allied defenses, so production mostly concentrated on the L model.
Deliveries started in August 1944 but few Ju 388s were completed. About 47 L models seem to have been built, the majority as -1s with the BMW 801J engine, and just three -3s with the Jumo 213E. Fifteen K-1s were built; and only three J-1 models were produced.
The exact number of Ju 388s built is difficult to determine. One of the reasons is that various pre-series aircraft were used as prototypes, and some were damaged or destroyed by Allied bombs before completion. Furthermore, several official records terminate before the end of production or contradict each other.
Based on available documentation and research the following can be assumed as proven:
- 6 Ju 388 prototypes, 2 each for J-1, K-1 and L-1
- 20 Ju 388 L-0, including prototypes V7, V8, V30 - V34
- 10 Ju 388 K-0, first batch, including Ju 488 V401/V402 (never flown)
- 1 Ju 388 K-1 manufactured by ATG for static tests in July 1944
- 46 Ju 388 L-1 manufactured by ATG in 1944
- 8+ Ju 388 L-1 manufactured by ATG in 1945
- 10 Ju 388 L-1 (max.) manufactured by Weserflug (WFG), initially planned as K-1
More aircraft and prototypes were planned and partially completed:
- 10 Ju 388 K-0, second batch, some prototypes, partially completed
- 30 Ju 388 K-0, third batch, planned, only few units completed
Also, an unknown number of Ju 388 L-1 and Ju 388 J were in advanced stages of production by the end of the war.
Several reconnaissance missions were flown by operational Ju 388s, generally believed to be "L" models, during the final days of the war in Europe. Most were flights over England, and were similar to the reconnaissance missions being flown by the jet-powered Arado Ar 234 at the same time period.
In early 1945, a Ju 388 was intercepted while flying at approximately 13,500 m (44,291 ft) over the English Channel by a Supermarine Spitfire. The Spitfire, operating above its service ceiling, was not able to reach the altitude of the Ju 388 but was able to fire upon it from below and bring it down. It is one of the highest successful interceptions recorded in World War Two.
- Ju 388J
- Heavy fighter / night fighter.
- Ju 388K
- High-altitude bomber.
- Ju 388L
- Photo-reconnaissance aircraft.
- Ju 388M
- Proposed torpedo bomber based on the Ju 388K.
- A single Ju 388L extensively modified with irreversible electromechanical powered flying controls to support the '150' in the USSR.
- Erprobungsstelle Rechlin
- Erprobungsstelle Werneuchen
- Erprobungskommando Ju 388
- 3./Versuchsverband O.K.L. operated Ju 388 V32, W.Nr 300 295, T9+DL.
- Nachtjagdgeschwader 2 operated four Ju 388J-0 nachtjager during April/May 1945, under operational trial/evaluation conditions. Aircraft were pre-production prototypes.
In August 1944, a Japanese delegation led by military attachĂ© Brigadier General Otani expressed interest in a license production of the Ju 388. Complete drawing sets for the Ju 388 were handed over to the Japanese as well as the rights for a license production. Most likely, the planned delivery of all these documents to Japan via submarine failed.
ULTRA decrypts of signals to and from the Japanese embassy in Berlin in August 1944 reveal that Otani (named 'Kotani' in the signals) was seeking return passage by U-boat in August 1944, but was told others had greater priority for places on U-boats. After 23 August 1944 and the departure of U-219, no other U-boat successfully departed for Japan. U-871 and U-864 were sunk outbound. U-234 sailed with a 240-ton cargo. Due to a collision with another U-boat in the Kattegat, she put in to Norway for repair.
When U-234 was later unloaded by the U.S. Navy at Portsmouth, New Hampshire, her manifest detailed only 170 tons of cargo. Radio operator Wolfgang Hirschfeld wrote a book Atlantik Farewell: Das Letzte U-boot in which he said the highest priority cargo needed to be unloaded and flown to Japan. He said that there was a proposal to use a Fw 200 Condor, but this aircraft was abandoned. Russian historian Sergey Platov claims Otani was on a Ju 290 flight to Japan which occurred 28 March 1945. Other historians also assert that Otani was not found in Europe at the end of the war.
One Ju 388 survives today. The Ju 388L-1 reconnaissance version with construction number (Werknummer) 560049 was the eighth of the series manufactured at Weser Flugzeugbau's Nordenham plant. Parts of the airframe were also built at ATG in Altenburg and at NiedersĂ€chsische Metallwerke Brinckmann & Mergell in Hamburg-Harburg. The aircraft was completed early in 1945. It was captured by U.S. troops in May 1945 at the Junkers plant in Merseburg, then flown to Kassel/Waldau.
The aircraft was examined and test flown by "Watson's Whizzers", led by United States Army Air Forces (USAAF) Colonel Harold E. Watson, as part of Operation Lusty and it is believed that Watson himself flew in the aircraft in preparation for flying it directly back to the U.S. Instead, on 17 June 1945 the aircraft was flown to Cherbourg, France where it was shipped to the United States aboard the Royal Navy escort carrier HMS Reaper together with other captured German aircraft for detailed evaluation in the U.S.
The aircraft was flown to Freeman Field in Indiana for evaluation, and in September 1945 made a flight demonstration for the press. The Ju 388 was flown for 10 hours of flight tests at Wright Field near Dayton, Ohio with the "foreign evaluation" serial number FE-4010 (later changed to T2-4010). Following these tests the aircraft was displayed at the Dayton Air Show in 1946 along with other captured German aircraft.
On 26 September 1946, 560049 was transferred to Orchard Place Airport in Park Ridge, Illinois, near the present O'Hare International Airport. This temporary storage facility was a vacant U.S. Government-owned factory previously used by the Chrysler Corporation to build the Douglas C-54. The Ju 388 was donated to the Smithsonian Institution's National Air Museum on 3 January 1949 and arrived at Silver Hill, Maryland, for storage in November 1954.
Today the aircraft is disassembled and remains in generally good condition, having never been stored outside. The cockpit area is in particularly good condition and complete with all instruments. The aircraft is just one of several unique German aircraft still awaiting restoration at the National Air and Space Museum's Paul E. Garber Preservation, Restoration, and Storage Facility in Silver Hill, Maryland, all intended to be transferred in the coming years to the Steven F. Udvar-Hazy Center's restoration annex of the Smithsonian, on the Dulles International Airport property.
Specifications (Ju 388J)
- Crew: 3
- Length: 16.29 m (53 ft 5 in)
- Wingspan: 22.00 m (72 ft 2 in)
- Height: 4.35 m (14 ft 3 in)
- Wing area: 56.00 mÂČ (602.77 ftÂČ)
- Empty weight: 10,400 kg (22,928 lb)
- Max. takeoff weight: 14,675 kg (32,352 lb)
- Powerplant: 2 Ă BMW 801J 14-cylinder air-cooled radial engine, 1,350 kW (1,810 hp) each
- Maximum speed: 616 km/h at 12,285 m (383 mph at 40,305 ft)
- Cruise speed: 540 km/h (335 mph)
- Service ceiling: 13,440 m (44,095 ft)
- Rate of climb: 378 m/min (1,240 ft/min)
- Boost speed:655 km/h (407 mph) at 9,080 m (29,790 ft) with MW 50 water-methanol boost (Jumo 213E only)</ul></ul>Armament
- Ju 388J: 2 Ă 20 mm MG 151/20 cannons and 2 Ă 30 mm (1.18 in) MK 103 or MK 108 forward-firing cannons in underfuselage pod and 2 Ă 13 mm (.51 in) MG 131 machine guns in remote-control Hecklafette tail turret
- Ju 388K: 3,000 kg (6,612 lb) of bombs internally and 2 Ă 13 mm (.51 in) MG 131 machine guns in remote-control Hecklafette tail turret
- Ju 388L: 2 Ă 13 mm (.51 in) MG 131 machine guns in remote-control Hecklafette tail turret
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- C. Vernaleken, M. Handig (2006). Junkers Ju 388: Development, Testing and Production of the Last Junkers High-Altitude Aircraft. Schiffer Publishing.
- C. Vernaleken, M. Handig (2006). Junkers Ju 388: Development, Testing and Production of the Last Junkers High-Altitude Aircraft. Schiffer Publishing.
- Vernaleken, Christoph and Handig, Martin. Junkers Ju 388: Development, Testing And Production of the Last Junkers High-altitude Aircraft. Atglen, PA: Schiffer Publishing, 2006. ISBN 0-7643-2429-2.
- Green, William. Warplanes of the Third Reich. London: Macdonald and Jane's Publishers Ltd., 1970. ISBN 0-356-02382-6.
- Smith, J.R. and Kay, Anthony. German Aircraft of the Second World War. London: Putnam and Company, Ltd., 1972. ISBN 0-370-00024-2.
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