Multi-seat fighters: "cruiser fighters" and "battleplanes"

Arjen said:
... with some help from me.

Well, that's understatement, as Arjen actually took a much more active part here and
results would have been considerable different without his collaboration, actually
working on the graphics, too.
An interesting, but widely forgotten type, somehow strange looking, even for contemporary
standards. ;)
 
Hi,


here is a wooden Model to Grigorvich DG-56.
 

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Nice find Hesham!

Btw. Jemiba & Arjen - I'm trying to figure out how to get a better set of dimensions from the Lloyd L.K.1 - do you guys have any tips? I've been thinking of dredging up the old Austrio-Hungarian thread to talk about some of the challenges (there may be a couple of issues with the existing reconstruction).
 
Do you mean this one http://www.secretprojects.co.uk/forum/index.php/topic,21084.msg207896.html#msg207896 ?
Didn't check the drawing still yet, so I wasn't aware of faults in it.
Perhaps better to discuss it via PM or mail and just post the results here ?
Maybe not interesting to everybody and a bit out of the scope here ?
Some dimensions can be found here http://www.dieselpunks.org/profiles/blogs/knights-of-the-air-made-in,
although I couldn't find a source mentioned. Firts way could be, to check those against the 3-view.
The prototype wasn't fitted with any weapons, so the only dimensions, that cold be used as a
reference may be the outer engines.
 
Re: Multi-seat fighters and cruiser fighters

Avimimus said:
- Kochergin IT (technically WW2)
? Kochergin DIS (technically WW2)

What was those Projects ?.
 
Re: Multi-seat fighters and cruiser fighters

hesham said:
What was those Projects ?.

Two SA Kocherigin twin-engined fighter designs - Kocherigin IT (Istrebitel' Tyazhelyi - Heavy Fighter) and Kocherigin DIS (Dalnij Istrebitel' Soprovozhdenya - Long-range Escort Fighter). Other sources give that first designation as IT-2 (Istrebitel Tankov - Tank Fighter)

See borovik's post: http://www.secretprojects.co.uk/forum/index.php/topic,12185.0.html
 
Thank you my dear Apophenia,

I don't remember them.
 
Hi! Grokhovsky G-38 images.

http://yuripasholok.livejournal.com/728841.html

http://xn--80aafy5bs.xn--p1ai/aviamuseum/aviatsiya/sssr/istrebiteli-2/1920-e-1930-e-gody/proekt-legkij-krejser-g-38-lk-2/

http://epizodsspace.airbase.ru/bibl/tm/1938/8-9/sam-gryad.html
"Two beam "plane", which was shown at the Paris exhibition. The tail is close to the wing. This plane is a transitional phase to the tailing flights of flying wings."

http://xn--80aafy5bs.xn--p1ai/aviamuseum/aviatsiya/sssr/istrebiteli-2/1920-e-1930-e-gody/proekt-legkij-krejser-g-38-lk-2/
 

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Hi all! First post on the Forum)

Some words about Grokhovsky G-38.

It seems to me, that well known plans, images and 3d model that were posted by Redstar72 and blackkite are fake based on pic from the TM (Техника Молодежи) magazine 08 sep 1938.http://zhurnalko.net/=nauka-i-tehnika/tehnika-molodezhi/1938-08-09
index.php

But in fact this pic described as

Двух балочный» самолет, который демонстрировался на Парижской выставке. Хвостовое оперение приближено к крылу. Этот самолет — переходная ступень к бесхвостым «летающим крыльям»
or in Eng:
Two tail plane demonstrated on Paris air show [in 1936]. Aircraft tail moved closely to wing. This plane is intermediate stage to tailless "flying wings".

So this pic is just an "author`s vision" of Fokker`s G-1 performed by A. Preobrazhensky or S. Lodygin for article.

What a Fate`s joke: real Ivensen-Grokhovsky project replaced by fake, based on picture for (again) Grokhovsky`s article.

But in article about P.A. Ivensen i found another image of G-38
http://sm.evg-rumjantsev.ru/des2/ivensen.html
g-38.jpg

And later - side view of G-38 in book Aircraft industry of USSR 1917-1945 part I (Самолетостроение в СССР 1917-1941 том 1) ch.5 p.245.
5c1008c9860f2_-38.png.a8cc02fa385107f1306418413a8efdfb.png
 
Welcome aboard Stenda,

and than you for the info,here is a more drawing to G-38;

https://www.secretprojects.co.uk/forum/index.php/topic,17629.0.html
 
hesham said:
Welcome aboard Stenda,

and than you for the info,here is a more drawing to G-38;

https://www.secretprojects.co.uk/forum/index.php/topic,17629.0.html
Mea culpa, hesham!
It seems i saw that page being logout whithout pics. Thnx a lot! G-38 was like Grail for me - to find more info.
 
Did anyone mention the World War 1, Llyod Luftkruiser? It was built in Austro-Hungary during WW1 and - thankfully - never entered service. It inherited a god-awful front turret and cockpit arrangement from its single-engine predecessor.
 
Now, radial engines and turrets are about equal width...alternating pusher/tractor nacelles might also give you a good firing arcs, heat-and the props blocking some fire?
 
Tangential, was watching a doc on prototype B-17 (??) gun-ships for escorting bombers. Nice out-bound, probably gave some Luftwaffen a bad time, but was still laden with armour and ammo on return leg, where the now-lighter bombers 'pulled away' leaving those unhappy gun-ships either utterly alone, or pacing damaged bombers with eg one engine out.

Perhaps workable with better engines, but impracticable as-is: Project urgently cancelled...

Besides, very long range fighter escorts had arrived...

I take it the 'Liberator' gun-ship version was similarly beset ??
 
A few tidbits about both the B-40 and the YB-41, both of which I have been researching for some time.

First, the B-40.

The B-40 project was based upon a request early in the war by the British, their daylight bombing experience with the early shark-tail B-17's being decidedly less than sanguine. They weren't terribly well protected and left a huge unprotected area in the tail with no gun back there. By the time the USAAF got around to fielding the B-40 the British wanted no part of it.

The original plans for the B-40 involved the use of the Allison V-1710. It became clear very early on that the amount of modifications for the wings to handle the cooling would take a tremendous amount of time and add a great deal of weight. The AAF wanted a "quick and dirty" escort, thus armament modifications to a standard B-17. The AAF was greatly looking forward to the protection the B-40 seemed to provide, enough so that they developed combat box tactics for entire squadrons of B-40's (which I have). The problems of the overweight B-40 have been presented before so I won't go into them now.

As for the YB-41, the AAF figured out that a flight of B-24's accompanied by a B-17 would just scream "this airplane is an escort!!". Thus the need for an appropriately-modified B-24 to accompany Liberators on combat missions. While I am going to go into a good deal of detail on the YB-41 in a future book title I'm working on, the biggest problem was too much weight on an already-overloaded aircraft. Not only was overheating a problem, but the aircraft could not make it to the altitude at which the bombers would fly and it handled like a brick.

The B-40 and YB-41 were far from the final word on the "convoy escorts". Similar versions of both the B-32 and the B-29 were designed. Beyond that, prospective designs for more advanced escorts were developed, although fairly crudely drawn.

I hope the above is of interest.

I remain,

AlanG
 
Hi.

G6M Heavy Escort Fighter:

G6M1 of Naval Air Technical Arsenal, later used by Takao Kokutai

jap G6M1 schwerer geleitjaeger.jpg


G6M vierseiten.jpg

Some 30 G4M were remodelled this way. Due to the additional weight of the expanded ammunition load the aircraft were too slow to follow the standard bombers, especially after bomb release. The fuel load at start also had to be reduced limiting the range. Both was rated inacceptable so after operational tests the remaining G6M were used for crew training and transport purposes.



Nakajima Ki-58 Heavy Escort Fighter:

jap Ki-58 exp schwerer geleitjaeger hinten.jpg

ki58-1.gif


Escort fighter version of the Nakajima Ki-49 Heavy Bomber. 3 prototypes were built but it seems there were similar problems as with the G6M. No serial production.



Nakajima Ki-80 Formation Leader Bomber:

Ki-80 was a planned formation leader version of the Ki-49. AFAIK it was similar to the standard aircraft but with additional navigation and wireless equipment. 2 prototypes were built before the project was cancelled. At least one was later used as test bed for the planned upgrade of the Ki-49-II with the more powerful HA-117 radials. I wouldn´t count it as a fighter.



Mitsubishi Ki-69 Heavy Escort Fighter:

Planned escort version of the Ki-67 Heavy Bomber. Cancelled before prototype production started.



Mitsubishi Ki-109 Heavy Fighter:

jap Ki-109 exp schwerer abfangjaeger mehrseiten skizze.jpg

jap Ki-109 exp schwerer jaeger bug.jpg

Bomber formation destroyer version of the Ki-67 Heavy Bomber with a fighter aircraft armed with a nose-mounted Ho-501 75 mm gun and 15 shots (modified Type 88 75 mm anti-aircraft gun) developed from late 1944. For night attacks a spotter version equipped with a wing-mounted searchlight was planned. Both versions should work as pairs. Later a searchlight was added on the upper right of the gun making the searchlight version unnecessary.

The first prototype only had the necessary remodelled nose. During innitial tests the aircraft was streamlined by removing the small side armament cupolas and the upper cupola. They were rated unnecessary for the intended purpose.Only the tail gun was kept.

There were also few tests with a simple rocket engine fired from the bomb bay to allow faster approach to the enemy formations. During the innitial tests the aircraft showed various problems reaching the flying height of the B29 bombers. So it was decided to use the aircraft for heavy ground attacks during the expected invasion, especially as landing craft killer. They were kept save for this purpose. Therefore they were never used operational. 22 aircraft were built.

Not an escort fighter but a kind of "battleplane"....



Mitsubishi Ki-112Heavy Escort Fighter:

Planned "Wooden" version of the Ki-69 Heavy Escort Fighter armed with 8 X 12,7 mm Ho-103 MGs and a 20 mm Ho-5 Machine Cannon. Wood should repace as many elements as possible to spare metal. Cancelled during the early development phase.


So much for my knowledge. Corrections and additions welcome.

Yours

tom! ;)
 
Last edited:
Back to the AAF's discussions of "convoy escort" aircraft.

The AAF gave very serious thoughts to using heavily-armed B-26's as convoy escorts. I may even have some photos of an early iteration.

Fortunately, they did not proceed with this. As I see it, there were a number of inherent problems with the plan:
1. There are certainly questions about whether the B-26 could carry both adequate fuel and weapons to keep up with the "convoy" to and from the target.
2. The B-26 was certainly not maneuverable enough to do anything but chug along next to the formation. No dog fighting.
3. After 10 minutes over enemy territory into the first mission it would be perfectly obvious what the purpose of the B-26's was and they would be the first aircraft to be taken out by German fighters, thus leaving the bombers where they would have been had the B-26's never been modified.
4. Could these heavy B-26's have reached and maintained the same cruising altitude as the bombers? Probably not.

The whole issue of the "convoy escort" is much more involved than any book to date has examined or revealed. I intend to eventually give the whole story.

Regards,

AlanG
 
I would think Mosquitos with rocket pods would be perfect candidates...play chicken with FW-190s as they dodge rockets. Rocket boost as the bombers escape-jettison the spent pods as incendiaries-or fire backwards to deter pursuit.
 
Between February 1918 and July 1922, the French Aéronautique Militaire used the Caudron R.XI heavy escort fighters from the Escadrille C 46, in joint operations with the Breguet XIV night bombers of the 3ême regiment de bombardement.

In 1924 a night fighter unit was officially created using Breguet XIV B2 bombers converted into night fighters, fitted with flare launchers and Vérain landing lamps on the lower wings.

The two types of aircraft: CAP (Chasse, Reconnaissance d’Armée et Protection) and CAN (Chasse et Reconnaissance d’Armée de Nuit), were called combattants de nuit and were replaced in 1926 by the Breguet Br. XIX B2 night bombers from the 23ème escadrille du 12ème RAB-Reims.

In 1932, forty Br. XIX B2 bombers were converted into Br. XIX CN2 (Chasseur de Nuit- Biplace) night escort fighters armed with two nose mounted machine guns.

Between 1932 and 1934 these aircraft were used by the 22ème and 23ème Escadrilles de Chasse de Nuit from GB III/22-Chartres.

Caudron R. XI C.3 technical data

Wingspan: 58.8 ft. (17.92 m), length: 36.8 ft. (11.22 m), height: 9.84 ft. (3 m), wing area: 602.7 sq. ft. (54.25 sq. m.), max weight: 4,779 lb. (2,165 kg), max speed: 114 mph (183 km/h), service ceiling: 19,516 ft. (5,950 m.), range: 110 miles (177 km), power plant: two Hispano-Suiza 8Bda, eight cylinder, Vee, liquid cooled engines rated at 215 hp. each, armament: five 7.7-mm Lewis machine guns.

Paint scheme (1919): overall three shades of Brun Foncé (Dark Brown /Federal Standard Reference FS 30045), Terre de Sienne (Sienna FS 30219), Vert Foncé (Dark Green FS 30219) and four positions cocardes (French roundels).

Breguet XIV CN2 technical data

Wingspan: 47 ft. (14.36 m), length: 28.8 ft. (8.87 m), height: 10.8 ft. (3.3 m), wing area: 540 sq. ft. (50.2 sq. m.), max weight: 3,900 lb. (1,769 kg), max speed: 121 mph (195 km/h), service ceiling: 20,300 ft. (6,200 m), power plant: two Renault 12 Fcx, twelve cylinder, Vee, liquid cooled engines rated at 300 hp. each, armament: two nose mounted 7.7-mm Vickers 7.7-mm and two movable 7.7-mm Lewis machine guns.

Paint scheme (1919): overall three shades of Brun Foncé (Dark Brown FS 30045), Terre de Sienne (Sienna FS 30219), Vert Foncé (Dark Green FS 30219) and four positions cocardes.

Breguet XIX CN2 technical data

Wingspan: 48.6 ft. (14.83 m), length: 31,5 ft. (9.61 m), height: 12 ft. (3.69 m), wing area: 538 sq. ft. (48.42 sq. m.), max weight: 5,511 lb. (2,500 kg), max speed: 133 mph (214 km/h), service ceiling: 23,620 ft. (7,200 m), range 497 miles (800 km), power plant: one Lorraine-Dietrich 12 Hb, twelve cylinder, Vee, liquid cooled engine rated at 500 hp., armament: two nose mounted 7.7-mm Vickers 7.7-mm and two movable 7.7-mm Lewis machine guns.

Paint scheme: overall Vert-Kaki (Dark Green FS 34257), Couleur Aluminium (Natural Metal) engine cowling and four positions cocardes.
 

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During the interwar period the British Air ministry continued to refine their night interception tactics using upward firing guns.

The Specification F 4/24, calling for a multi-seat twin-engine night defense fighter armed with two 37-mm C.O.W. cannons, led to the Bristol Bagshot and the Westland Westbury heavy fighters.

These designs were based on the French concept multiplace de combat that had been so successful in 1918.

The Bristol Type 95 Bagshot prototype (J7767) was flown on July 15, 1927, showing serious structural problems and the project was abandoned.

Bristol Type 95 technical data

Wingspan: 70 ft. (21.34 m), length: 45 ft. (13.69 m), height: 9.5 ft. (2.89 m), wing area: 840 sq. ft. (78 sq. m.), max weight: 8,195 lb. (3,717 kg), max speed: 125 mph (201 km/h), power plant: two Bristol Jupiter VI, nine cylinder, radial, air cooled engines rated at 450 hp. each, armament: two 37-mm Coventry Ordnance Works cannons and two 0.303-in Lewis machine guns.



The Westbury prototype (J7765) was flown in September 1926 and a second prototype (J7766) with a modified nose was flown in May 1927.

The first firing trials with C.O.W. cannons resulted in wing structural damage caused by the blast and recoil.

The concept was abandoned in favor of Specification F 27/24 for a single-seat, twin-engine night fighter capable of breaking up groups of heavy bombers.

Westland Westbury technical data

Wingspan: 69 ft. (21 m), length: 43.3 ft. (13.2 m), height: 13.7 ft. (4.19 m), wing area: 875 sq. ft. (81.3 sq. m.), max weight: 7,887 lb. (3,573 kg), max speed: 125 mph (201 km/h), power plant: two Bristol Jupiter VIII, nine cylinder, radial, air cooled engines rated at 480 hp. each, armament: two 37-mm Coventry Ordnance Works cannons and two 0.303-in Lewis machine guns.

The Boulton Paul P.31 Bittern was designed to meet the Specification F 27/24.

The first prototype (J7936) was flown in February 1927 showing excessive wing flexibility and lack of lateral control.

The second machine (J7937) had re-designed wings with additional struts and was armed with two Lewis machine guns carried in revolving barbettes mounted in the fuselage sides.

Trials were not satisfactory because of the low performance of the two airplanes.

The project was abandoned in favor of Specification F 29/27.

Boulton Paul P.31 (J7936) technical data

Wingspan: 41 ft. (12.5 m), length: 32.3 ft. (9.86 m), height: 8.5 ft. (2.59 m), max weight: 4,500 lb. (2,041 kg), max speed: 152 mph (245 km/h), power plant: two Armstrong Siddeley Lynx, seven-cylinder, radial, air cooled engines rated at 230 hp. each, armament: two 0.303-in Lewis machine guns.

Paint scheme: overall Dark Green (FS 34079) with six positions Type B low visibility roundels.
 

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To circumvent the limitations imposed by the Treaty of Versailles, the German High Command negotiating a mutual assistance agreement with the Soviet Government that gave Germany use of Russian air base at Lipetsk between 1925 and 1930.

These secret facilities were initially used for the training of pilots with aircraft Fokker D.VII, D.XI and D. XIII acquired in Holland, but from 1926 they were also used to test new models of German aircraft, evading inspections of the Inter Allied Control Commission.

The tests were carried out with single-seat fighters Arado SD I, SD II, SD III, SSD I, Ar 64, Heinkel HD.37 and HD.38, two-seat attack fighters Albatros L.65, Heinkel HD.17, Junkers Ju 21 and A.35, two-seat reconnaissance airplanes Albatros L.78, Focke-Wulf S.39 and Heinkel HD.5, passenger airplanes Dornier B, Rohrbach Roland VIII and Junkers G.24 converted in bombers, experimental dive bombers Junkers K.47 and experimental chemical warfare airplanes Albatros L.76.

In the late 1920s the British firm Fairey Aviation Co. designed the first all-metal low-wing monoplane bomber, named Hendon, with 1,360 miles (2,188 Km) range.

The German answer was the NAKUJA specification Nachtjagd und Erkundungs Flugzeug (Night Fighter).

The project was commissioned to the firm BFW/Messerschmitt which proposed to modify its project of medium bomber M.22 adapting it for night fighting duties.

In November 1930 the Hendon made its first flight exceeding its own specification B.19/27 by 37 mph and by 16 mph the maximum speed of the German fighter.

The M.22 did not pass the prototype phase and BFW bankrupt in June 1931.

Messerschmitt M.22 technical data

Wingspan: 55.7 ft. (17 m), length: 44.6 ft. (13.6 m), height: 15.7 ft. (4.8 m), max weight: 8,380 lb. (3,800 kg), max speed: 137 mph (220 km/h), power plant: two Siemens-Halske Sh-20 air cooled radial engines rated at 500 hp. each.
 

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The Chasse Obscure (Dark Fighting) tactic adopted by l'Armèe de l'Air after the Munich Agreement, did not use searchlights to prevent the loss of night vision of the pilots.

The French divided the front into sectors 15 km (9.3 mi) wide and 20 km (12.4 mi) deep guarded by sound locators. When an intruder was detected, trained personnel tried to predict its possible trajectory and reported to the Control Center to direct night fighters in their interception, using the R/T and Direction Finder (D/F) systems.

In January 1939 l'Armèe de l'Air had two Groupes de Chasse de Nuit (Night Fighters Group) with two Escadrilles de Chasse de Nuit, the ECN III/1 based at Etampes and the ECN II/4 based at Reims, both escadrilles were equipped with night fighters ANF Mureaux 113 CN2 (170 mph-274 km/h) and Dewoitine D.501CN (228 mph-367 km/h).

Both types were fitted with 20 mm cannons, night instruments, OTC 31 R/T devices and overall Vert Foncé (Dark Green- FS34201) paint scheme with Couleur Aluminium (Natural metal) engine cowling and four positions cocardes. In April 1940 the aircraft received the same type of camouflage as the day fighters, with six positions cocardes.

The organization of the Chasse de Nuit, based on ideas and tactics developed during the First World War did not surpass the reality of the combats in 1940.

According to the theory, the pilots should approach the target up to 500 yards and identify it visually with the help of a small searchlight before firing.

In practice the maximum speed of the French night fighters proved insufficient to hunt down the new Bombers Heinkel He 111 P-2 (247 mph-397 km/h), Dornier Do 17 Z-3 (255 mph-410 km/h) and Dornier Do 215 B-0 (292 mph-470 km/h).

In February 1939, Mureaux and Dewoitines began to be replaced by the Potez 630 type (286 mph-460 km/h) twin engine heavy fighter, but this model was prematurely withdrawn from service with the GCN I/13, due to engine problems, and was replaced in turn by the Potez 631 CN3 in August.

The new night fighter was somewhat slower (275 mph-442 km/h) but was very well armed with two 20 mm cannon and four 7.5 mm machine guns.

A few days after the declaration of war against Germany, some Potez 631 CN3 were concentrated at the Melun-Villaroche air base to perform night fighting simulations using different combinations of searchlights, sound locators and D/F devices.

The results of the new tactics were inconclusive and eventually the Chasse Obscure doctrine prevailed.

The day of the German attack (May 10, 1940) l'Armèe de l'Air had five Escadrilles de Chasse de Nuit, the ECN 1/13, ECN 2/13, ECN 3/13, ECN 4/13 and ECN 5/13 equipped with 58 Potez 631 CN3 of which only 47 were in flying condition.

His combat career was very brief, limiting himself to making 78 night sorties, between May 11 and 16, without achieving any kill, and l'Armèe de l'Air decided to use them in day time fighting and ground attacks to the Wehrmacht motorized columns in Fourmies and Moirans areas.

In their new role the Potez managed to destroy eight Heinkel He 111s and one Dornier Do 17, but suffered numerous attacks erroneously carried out by French and British fighters who mistook them for German Messerschmitt Bf 110s. Three Potez heavy fighters were shot down and three others badly damaged by friendly fire.

These aircraft used the same paint scheme as the French day fighters: upper surfaces in three shades of Gris-Bleu Foncé (Dark-Blue Grey-FS 36320), Brun Foncé (Dark Brown-FS 30045) and Vert Foncé (Dark Green- FS 34201), under surfaces in Gris-Bleu Ciel (Skygrey Blue-FS 35352).

Between January and February 18, 1940 the Potez 631 c/n 117 was painted with an experimental night camouflage scheme: upper surfaces in three shades of Gris-Bleu Foncé (Dark-Blue Grey-FS 36320), Noir (Black FS 37038) and Vert Foncé (Dark Green- FS 34201), under surfaces in Noir (Black FS 37038).

At the end of May l'Armèe de l'Air ordered that all Potez of the models 63.11, 631 and 637 Bons de Guerre (in flying condition) be identified with additional markings to avoid confusion with the Messerschmitt Bf 110.

The aircraft were painted with longitudinal white bands on the fuselage sides and to the 120 cm cocardes located on the upper surface of the wings were added two additional cocardes of only 30 cm diameter on the wingtips.
 

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During the summer of 1940 it was formed in Gilze-Rijen/Netherlands the NJG2, one specialized Fernnachtjagd Gruppe (long-range fighter unit) with four Nachtjagd staffeln (night fighter squadrons) of Junkers Ju 88 C-2 night intruders.



The availability of this model was scarce (less than three per cent of production) because the bomber units KG2, KG3, KG76 and KG 77 began to exchange its Dornier Do 17 Z-2 bombers (218 mph-350 km/h) for Ju 88 As.



The Oberkommando der Luftwaffe (OKL) decided to equip the 2./NJG2 with modified Do 17s and Dornier Werke was instructed to investigate their adaptation as a long-range intruders for interim use.



Tests were conducted with the Do 17 Z-2 (R4+ZK) with an MG FF cannon fitted under the glazed nose, RLM 70 Schwarzgrün (Black-Green FS 34050)/RLM 71 Dunkelgrün (Dark Green FS 34079) upper surfaces and RLM 22 Schwarz (Black FS 37038) under surfaces. This aircraft was used by the Oberleutnant Werner Streib in the shooting down of a Whitley bomber during the night 20/21 July 1940.



There is a report of a Dornier Do 17 P-1 (246 mph-396 km/h) also being tested as a long-range night fighter for interim use.



Finally the OKL decided to modify the last nine production Do 17 Z-3 (255 mph-410 km/h) long-range reconnaissance airplane, fitted with one 440 liters fuel tank in the bomb bay, FuBl 2 blind landing device, FuG 350 Naxos Z passive radar receiver for the British H2S and the Waffenkopf solid nose cone of a Ju 88 C-2, housing 3x7.92-mm MG 17 machine guns, one 20-mm MG FF cannons and 11-mm armor bulkhead.



FuG 350 Zc Naxos passive radar-receiver of H2S, H2X and AN APS 15 allied radars Passive Ortungsgerät developed by Telefunken.

Weight of 24 kg.

With EA 350Zb rotating antennae (250 mm of diameter) and SG 350 Zc display unit.

Frequency 2,500-3,750 Mhz.

Range of 100 km.

Provided azimuth measurement only.



The new version, named Do 17 Z-7 Kauz I, had the crew reduced to three members and was painted RLM 22 Satin Black overall, with RLM 77 Lichtgrau (Grey FS36492) codes and the individual letter outlined in White.

On November 9, 1940 the Kauz I (R4+HK) from 2./NJG was shot down by British night fighters, this model did not have much success but also few combat losses, By June 1941 the 2./NJG2 still had six operational aircraft in Gilze-Rijen.



In the summer of 1941, the Luftwaffe started using Spanner I infra-red searchlights installed under the nose of some Bf 110 D-3 and E-1 night fighters. The radiation reflected on the target was made visible for the human eye through and IR telescope named Q-Rohr installed in front of the pilot.



The system entered into service in 1941 with some Messerschmitt Bf 110 D-3 of the 4./NJG1 and ten Dornier 17 Z-7 Kauz I and Z-10 Kauz II of the I./NJG2. The latest were equipped with a more powerful searchlight Spanner III with a diameter of 60 cm, installed in the nose cone. The main shortfall of the first Spanner devices was the reduced field of view of the telescope. The image also suffered interferences from the moon, the stars, the flares and the explosions of flak.



The first Spanner kill was achieved by one Do 17 Z-10 from 4./NJG1 on the evening of October 16, 1940, over Oosterwalde.

The night fighter was guided to visual identification range of a Wellington bomber from No. 115 (BK) Squadron by the Nunspeet Freya station.



In late 1941 one Kauz II from IV./NJG2 was experimentally fitted with two 20-mm cannons in Schräge Musik configuration.



Dornier Do 17 P-1 technical data

Wingspan: 59 ft. (18 m), length: 53 ft. (16.16 m), height: 14.1 ft. (4.3 m), wing area: 611 sq. ft. (55 sq. m.), max weight: 16,998 lb. (7.700 kg), max speed: 255 mph (410 km/h), range: 1,367 miles (2,200 km), service ceiling: 21.320 ft. (6,500 m), power plant: two BMW 132 N, nine-cylinder, radial air-cooled engines each rated at 865 hp., armament: one forward-firing 20-mm MG FF cannon and two rear-firing 7.92-mm MG 15 machine guns.



Dornier Do 17 Z-2 technical data

Wingspan: 59 ft. (18 m), length: 51.8 ft. (15.8 m), height: 17.3 ft. (4.56 m), wing area: 611 sq. ft. (55 sq. m.), max weight: 19,426 lb. (8.800 kg), max speed: 267 mph (430 km/h), range: 715 miles (1,150 km), service ceiling: 23.944 ft. (7,300 m), power plant: two BMW 323 P, nine-cylinder, radial air-cooled engines each rated at 1,000 hp., armament: one forward-firing 20-mm MG FF cannon under the nose and six 7.92-mm MG 15 machine guns in front, rear upper, rear lower and cockpit positions.



Dornier Do 17 Z-7 Kauz I technical data

Wingspan: 59 ft. (18 m), length: 51.8 ft. (15.8 m), height: 17.3 ft. (4.56 m), wing area: 611 sq. ft. (55 sq. m.), max weight: 19,482 lb. (8.825 kg), max speed: 255 mph (410 km/h), range: 715 miles (1,150 km), service ceiling: 22,965 ft. (7,000 m), power plant: two BMW 323 P-1, nine-cylinder, radial air-cooled engines each rated at 1,000 hp., armament: one forward-firing 20-mm MG FF cannon and three 7.92-mm MG 17 machine guns in the solid nose.



Dornier Do 17 Z-10 Kauz II technical data

Wingspan: 59 ft. (18 m), length: 53.4 ft. (16.28 m), height: 14.3 ft. (4.36 m), wing area: 592 sq. ft. (53.3 sq. m.), max weight: 16,100 lb. (7,300 kg), max speed: 265 mph (426 km/h), range (with auxiliary fuselage tanks): 1,865 miles (3,000 km), service ceiling: 26,240 ft. (8,000 m), power plant: two BMW 323 R-2, nine-cylinder, radial air-cooled engines each rated at 1,200 hp., armament: two forward-firing 20-mm MG FF cannons and four 7.92-mm MG 17 machine guns in the solid nose.



Early in 1941 thirty Dornier Do 215 B-1 and B-4 schnellbombers were converted into Do 215 B-5 Kauz III night fighters fitted with Spanner III infra-red detection system, FuG 10 R/T device, FuG 350 Naxos Z, FuBl2 blind landing device and exhaust flame dampers.

These airplanes were faster than most Ju 88s and had five hours endurance, 1.5 hours longer than the Bf 110s.



During the spring of 1941 the 4./NJG2 used some Kauz IIIs for intruder sorties over British bomber bases.



In July the G9+OM intruder was converted to carry the low-UHF band AI radar FuG 202 Lichtenstein B/C. During one operational trial conducted the night of 8/9 August 1941, the Dornier downed one Wellington bomber from No. 301 (GR) Squadron.

In February 1942 the B/C radar was operational with all the Kauz III night fighters from I./NJG in Gilze-Rijen and II./NJG2 in Leeuwarden.



The paint scheme of the type in 1941 was overall RLM 22 Schwarz (Satin Black FS 37038) with RLM 77 Lichtgrau (Light Grey FS 3649) fuselage codes and the individual letter outlined in RLM 77.

In May the Balkenkreuz national markings of the wings were overpainted RLM 22 in some airplanes from 4./NJG1.

Early in 1942 the II./NJG2 painted its night fighters with RLM 75 Grauviolett (Grey-Violet FS 36122) upper surfaces, RLM 76 Lichtblau (Light Blue FS 36473) undersurfaces and RLM 22 codes.

By the summer the Kauz IIIs paint scheme from the II./NJG2 was RLM 74 Graugrun (Grey-Green FS 36801)/RLM 75 Grauviolett (Grey-Violet FS 36122) upper surfaces, RLM 76 Lichtblau under surfaces and RLM 77 Lichtgrau codes.



Dornier Do 215 B-5 Kauz III technical data

Wingspan: 59 ft. (18 m), length: 52 ft. (15.79 m), height: 15 ft. (4.56 m), wing area: 592 sq. ft. (55 sq. m.), max weight: 18,959 lb. (8,600 kg), max speed: 315 mph (507 km/h), range: 1,572 miles (2,450 km), service ceiling: 29,500 ft. (9,000 m), power plant: two Daimler-Benz DB 601 Ba, twelve cylinder, inverted Vee, liquid cooled engines each rated at 1,159 hp. with anti-glare exhaust shrouds, armament: two nose mounted 20-mm MG FF cannons, four nose mounted 7.92-mm MG 17 machine guns and one rear-firing 7.92-mm MG 15 machine gun.
 

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In dog fight the Dornier J-1 (Ein Klotz- One Brick for the crews) could not hunt the British Wellington bombers because these make tighter turns.

The OKL thought that the long endurance would make it a useful addition of the Nachtjagd, but the type proved disappointing in the defensive fighter role, their crews complained it was too heavy and poor maneuverable in combat, with weak undercarriage, underpowered engines, bad take-off and landing characteristics and only 6 m/sec climb rate, less than half that of the Ju 88 C-2.

Before entering combat some pilots preferred to dump all the bomber bay fuel in order to lighten the plane in 800 Kg.

Despite all its shortcomings the J-1 was used as day fighter against the American B-17 and B-24 bombers between August and October 1943.

In the autumn the type was relegated to the training role, with the armament removed, in the 4./NJG 101 Nachtjagdschule-Lechfeld.

Some airplanes were modified as Do 217 J-2 night fighters with the installation of one FuG 202 Lichtenstein B/C airborne radar, new MG 151/20 cannons, armored windshields and shrouded exhaust flame dampers.

The nose mounted Matratzen antenna cutting its top speed down to less than a Halifax bomber.

In October 1942 two prototypes (Do 217 J-1/U2 and Do 217 J-1/U4) were tested with the experimental Bänderfallschrim-Sturzflugbremse No. 25 semi-rigid brake parachute, allowing the fighter to adjust to the bomber speed before firing.

The Do 217 J-1/U1 prototype was also tested at the time with four MG 151/20 cannons in Schräge Musik configuration, firing at 70 degrees upwards.

This device, named Schusswaffenanlage, was later used by several Do 217 N-2 night fighters as standard Rüstsatz 22.

In the winter of 1942-43 some Do 217 J-1 night fighters were experimentally painted overall in RLM 77 Lichtgrau (Light Green FS 36492) and Black codes, to make them less visible to the British gunners. In the spring they were over spayed with loose Arabesken in RLM 75 Grauviolett (Grey-Violet FS 36122).

By mid-1943 the new paint scheme was the official ‘splinter pattern’ RLM 74 Graugrün (Grey-Green FS 36801)/RLM 75 Grauviolett (Grey-Violet FS 36122) upper surfaces with over sprayed blotches of RLM 77 and RLM 76 Lichtblau (Light Blue FS 36473) undersurfaces, with low fuselage demarcation. RLM 22 Schwarz (Black FS 37038) codes.


Dornier Do 217 J-1 technical data

Wingspan: 62.3 ft. (19 m), length: 59.7 ft. (18.20 m), height: 16.4 ft. (5 m), wing area: 614 sq. ft. (57 sq. m.), max weight: 29,059 lb. (13,180 kg), max speed: 304 mph (489 km/h), range: 1,274 miles (2,050 km), service ceiling: 27,560 ft. (8,400 m), power plant: two BMW 801 ML 14 cylinder, radial, air cooled engines each rated at 1,580 hp, armament: four nose mounted 20-mm MG FF/M cannons with flash hiders, four nose mounted 7.92-mm MG 17 machine guns and two rear-firing 13-mm MG 131 machine guns.
 

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In the spring of 1941, the Ju 88 C-4 (304 mph-490 km/h) entered service. It was a night fighter based on the airframe of the Ju 88 A-5 bomber, with Jumo 211 G engines rated at 1,400 hp, using B4 (86 octane) fuel and fitted with anti-glare exhaust shrouds.

This version differed from the C-2 in an extended wingspan from 18.38 to 20.13 m, the elimination of lower forward fuselage windows and the replacement of the MG FF cannon by one MG FF/M Minengeschoss and the installation of armor protection for the crew.

Some aircraft were fitted with two additional MG FF in the ventral gondola and others received a new bulged rear canopy, with two MG 15 rear-firing machine guns. In this version the ventral antenna of Fu Bl 2 was installed in a position closer to the tail, housed in a semi-transparent Plexiglas cover.

Sixty-six C-4 night fighters were built in 1941, these aircraft were used in Europe and the Mediterranean by the same units and paint scheme as the C-2.

Junkers Ju 88 C-4 technical data

Wingspan: 66 ft. (20.13 m), length: 48 ft. (14.66 m), height: 15.9 ft. (4.85 m), wing area: 587 sq. ft. (54.5 sq. m.), max weight: 25,386 lb. (11,500 kg), max speed: 304 mph (490 km/h), range: 2,113 miles (3,400 km) with two 900 lt. drop tanks, service ceiling: 36,080 ft. (11,000 m), power plant: two Junkers Jumo 211F, twelve cylinder, Vee, liquid cooled engines each rated at 1,410 hp., with anti-glare exhaust shrouds, armament: two 20-mm MG FF cannons and three nose mounted 7.92-mm MG 17 machine guns, with 5 degrees downward angle, two 20-mm MG FF/M cannons in the ventral gondola, two rear-firing 7.92-mm MG 81 machine guns and one 13-mm MG 131 heavy machine gun.

In 1942 the C-4 was replaced by the new version C-6/C-6b.

Of a total production of 257 aircraft built, some were modified as Schnellbombers (fast bombers) for the KG 76 and others were used by the KG 40 in anti-shipping missions.

The night fighter version Ju 88 C-6b (290 mph-466 km/h) was powered by two Jumo 211J-1 engines rated at 1,400 hp, with extended anti-glare exhaust shrouds, enlarged spinners, wooden VS-11 propellers and asymmetric bulges under the cowlings.

In this version the MG FF had been replaced by the new 20-mm MG 151/20 cannons with flash hidders and the protection of the crew had been increased with armor glass windscreens.

The electronic equipment comprised FuG 10 R/T with EZ6 Direction Finder antenna, FuG 101 radio-altimeter, FuG 25 (IFF), FuG 16 ZY R/T and FuBl 2 blind landing set.

FuG 25a Erstling IFF device Kenngerät manufactured by GEMA and Brinkler

Emission frequency of 160 MHz, reception frequency of 125 Mhz

Range of 100 km

Power of 600 W

Rod antenna under the fuselage (300 mm long) 10º rear swept

Responded to Freya, Würzburg and Gemse ground control radars

It could be used to calculate the distance of an airplane from the ground radar

The need to operate in several frequencies between 0.53 and 2.40 m considerably delayed its entering into service with the Luftwaffe

It was used in combination with the EGON (Erstling-Gemse-Offensive-Navigation) for radio navigation of bombers in combination with the FuMG 401A Freya LZ radar, as an alternative to the Y-Gerät

Weight 12 Kg.

FuBl 2 Funklandegerät blind landing device developed by Lorenz in combination with the FuG 130, the FuG 101a and the FuG 10/FuG 17(EB4).

Weight of 10 Kg.

FuG 101a Feinhöhermesser of 1.5 Kw, radio altimeter developed by Siemens/LG

Operation frequencies between 337 and 400 MHz in continuous wave and frequency modulation (CW-FM with 2 m. error)

Power 1.5 W

Weight of 16 kg

Range between 150 and 1500 m

It used two Sender S101 and Empfänger E 101 dipoles to transmit and receiver.


In some C-6b fighters the ventral gondola was deleted to get more speed (308 mph-496 Km/h) and the factory test plane (DU+GO) was experimentally armed with two 20-mm Mg 151/20 cannons in Schräge Musik configuration.

The C-6b was used in Europe and the Mediterranean by the NJGI and NJGIII Gruppen in Europe, by the NJG II in the Mediterranean Front and by the NJG 100 and NJG 200 in the East Front.

In April 1944 some C-6bs of the 2./NJG2 and 4./NJG2 were used in daytime combat against U.S bombers armed with four underwing W.Gr. 21 rockets.

In June 1942 the Ju 88 A-4 bomber (R4+CK) was used in night intruder missions by the 2./NJG2, this aircraft was overall painted RLM 22 Satin Black.

In November 1943 one Ju 86 C-6 was tested by the Erprobungskommando 25-Tarnewitz with two oblique MK 108/30 cannons in Schräge Musik configuration and the Ju 88 A-4 (NN+CX) with four upward-firing MG 151/20 cannons.

Both aircraft were transferred to the I./NJG100 and I./NJG4 for operational combat trials until the end of the year.

In May 1944 the Ju 88 C-6 (R4+DA) was experimentally equipped with one FuG 351Z Korfu passive homing device, with better range (300 km) and discrimination that Naxos, and dorsal mounted antenna, covering 1,660 to 11,100 frequencies used by all Allied AI radars.

Early C-6s were factory camouflaged in the standard ‘splinter’ scheme RLM 70 Schwarzgrün (Black Green FS 34050)/RLM 71 Dunkelgrün (Dark Green FS 34079) upper surfaces and RLM 65 Hellblau (Bright Blue FS 35414) under surfaces.

During the winter of 1942-43 some airplanes were painted overall with RLM 77 Lichtgrau (Light Grey FS 36492) or RLM 65 with upper surfaces speckled in RLM 75 Grauviolett (Grey Violet FS 36122), RLM 22 Schwarz (Black FS 37038) codes with the individual letter outlined in RLM 77.

In 1943 some aircraft from Stab IV./NJG5 based at Bryanks-Orel and II./NJG2 based at Comiso-Sicily had the undersurfaces painted in RLM 22.

The East Front identification markings from NJG 100 and NJG 200 were RLM 04 Gelb (Yellow FS 23539) undersides of wingtips and fuselage band.

The Mediterranean Front markings were RLM 21 Weiss (White FS 37886) undersides of wingtips and fuselage band.

In March 1944 some C-6s from 2./NJG2 had the starboard wing under surface painted in RLM 22 for Flak identification.

During 1943 a number of Ju 88 C-6 “Cat’s Eyes” from 10./NJG1, 1./NJG2, 2./NJG2, 11./NJG3, 12./NJG3, Stab IV./NJG5 and 4./NJG 100 were equipped with AI FuG 202 Lichtenstein B/C radars and FuG 227 Flensburg passive homing devices which detected emissions from Monica radars.

Junkers Ju 88 C-6b technical data

Wingspan: 66 ft. (20.13 m), length: 48 ft. (14.66 m), height: 15.9 ft. (4.85 m), wing area: 587 sq. ft. (54.5 sq. m.), max weight: 27,152 lb. (12,300 kg), max speed: 290 mph (466 km/h), range: 1,243 miles (2,000 km) with two 900 lt. drop tanks, service ceiling: 32,472 ft. (9,900 m), power plant: two Junkers Jumo 211J-1, twelve cylinder, Vee, liquid cooled engines each rated at 1,400 hp., with extended anti-glare exhaust shrouds, armament: two 20-mm MG FF cannons and three nose mounted 7.92-mm MG 17 machine guns, with 5 degrees downward angle, two 20-mm MG 151/20 cannons in the ventral gondola, two rear-firing 7.92-mm MG 81 machine guns and one 13-mm MG 131 heavy machine gun.

In October 1944, the Ju 88 A-4 bomber (R4+QV), armed with one MG FF cannon, was used by the 10./NJG2 as emergency fighter, this aircraft was painted RLM 70 Schwarzgrün (Black-Green FS 34050)/RLM 71 Dunkelgrün (Dark Green FS 34079) in the upper surfaces, RLM 22 Schwarz (Satin Black FS 37038) under surfaces and RLM 04 Gelb (Yellow FS 33538) in the engine cowlings.


Junkers Ju 88 A-4 technical data

Wingspan: 66 ft. (20.13 m), length: 47.2 ft. (14.40 m), height: 15.9 ft. (4.85 m), wing area: 587 sq. ft. (54.5 sq. m.), max weight: 30,905 lb. (14,000 kg), max speed: 273 mph (440 km/h), range: 1,119 miles (1,800 km) with two 900 lt. drop tanks, service ceiling: 36,080 ft. (11,000 m), power plant: two Junkers Jumo 211J, twelve cylinder, Vee, liquid cooled engines each rated at 1,410 hp., armament: two 20-mm MG FF cannons under the nose, two rear-firing 7.92-mm MG 81 machine guns and one 13-mm MG 131 heavy machine gun.
 

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In May 1942 the second prototype of the reconnaissance plane Caproni Ca.331 O.A. was modified as Ca.331CN night fighter and tested at Furbara firing range armed with two MG 151/20 cannons and four 12.7-mm Breda machine guns, all mounted in the nose.

By January 1943, all production plans were cancelled in favor of the Ro.58 NF project.

Type F1 “Metropolitan” paint scheme: Verde Oliva Scuro 2 (Dark Olive Green FS 34952) upper surfaces, Grigio Azzurro Chiaro 1 (Light Blue Grey FS 36307) under surfaces, “transparent” Fasci roundels in four positions, White fuselage band and Savoy crosses.

The CANSA FC.20 was a reconnaissance plane designed in 1941 to replace the Fiat Cr.25 bis.

One pre-production batch of ten machines was ordered early in 1942 and three of them were used in the summer of 1943 by the 174ª Squadriglia Ricognizione Strategica.

In May 1942 the second prototype MM.404 was modified into anti-tank assault plane armed with one 37/54 (37-mm.) Breda cannon.

During the spring of 1943 the MM.404 was used against the B-24 American bombers which operated over Italian targets at that time, but it was discovered that the aircraft took thirty minutes to reach the flight height of the bombers and at 7,500 m its maximum speed was lower than the cruising speed of the B-24s equipped with supercharged engines.

It was decided to replace the Fiat A.74 RC.38 engines of 840 hp with two Fiat Ar.80 RC.41 of 1,000 hp but the aircraft had turned out not to be stable enough at high altitudes. The flight controls barely responded due to the low air density and the plane uncontrollably fell several hundred meters when trying any combat manoeuver.

In July 1943 construction began on the FC.20 quater, a heavy fighter of the Zerstörer class powered by two Daimler Benz DB 601 engines. But the new aircraft had not yet been completed when Italy signed the armistice.

CANSA FC.20 quater technical data

Wingspan: 52.5 ft. (16 m), length: 41.3 ft. (12.6 m), height: 13.8 ft. (4.22 m), wing area: 431 sq. ft. (40 sq. m.), max weight: 15,750 lb. (7,135 kg), max speed: 311 mph (500 km/h), range: 578 miles (930 km), service ceiling: 26,240 ft. (8,000 m), power plant: two Daimler-Benz DB 601 A-1, twelve cylinder, inverted Vee, liquid cooled engines each rated at 1,175 hp, armament: one 37-mm Breda 37/54 AA naval cannon and two wing roots MG 151/20 cannons.



The construction of 100 CANT Z.1018 M Series II fast bombers was ordered on January 29, 1943 but only five machines (MM.24824 to MM.24828) were completed on September 9.

The first two aircraft in the series were modified as heavy night fighters BZ.303 Lince and the third as torpedo plane.

By 1943 the Italian scientists of the DSSE-Guidonia and SAFAR Company had managed to develop three types of 300 MHz radars:

-Radiotelemetro RDT Argo, early warning ground radar.

-RDT Vespa, airborne naval search radar.

-RDT Lepre, airborne interception radar.

A prototype of the Argo had already been tested at the end of 1942 at the Pratica di Mare airfield.

The Vespa was flight-tested installed in a Savoia Marchetti S.M. 79 bomber and two prototypes of the Lepre were tested on April 29 in SAFAR Cameri-Novara facilities.

It was expected to use the Lepre in the series of night fighters Lince, but to buy time it was decided to install in the MM.24824 one of the FuG 202 Lichtenstein B/C acquired in the spring of 1943. The installation of the Yagi antennas was completed on July 8 but when Italy signed the Armistice of Cassibile in September 8, 1943, the prototype was captured by the Germans and never was completely outfitted for combat.

Type F1 “Metropolitan” paint scheme: Verde Oliva Scuro 2 (Dark Olive Green FS 34952) upper surfaces, Grigio Azzurro Chiaro 1 (Light Blue Grey FS 36307) under surfaces, “transparent” Fasci roundels in four positions, White fuselage band and Savoy crosses.

CANT Z.1018 M Lince technical data

Wingspan: 73.8 ft. (22.5 m), length: 57.7 ft. (17.6 m), height: 22.3 ft. (6.8 m), wing area: 701 sq. ft. (63.1 sq. m.), max weight: 26,490 lb. (12,000 kg), max speed: 395 mph (636 km/h), range: 830 miles (1,335 km), service ceiling: 24,272 ft. (7,400 m), power plant: two Alfa Romeo 135 RC 32, eighteen cylinder, radial, air cooled engines each rated at 1,400 hp, armament: four 20-mm MG 151/20 cannons housed in the ventral pack and one rear firing flexible 12.7-mm SAFAT-Scotti heavy machine gun.
 

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Jack Northrop was in London during the Night Blitz of 1940 and noted British efforts to stop Luftwaffe night raids.

In November 1940, he decided to build a specially designed night fighter, based on the experience gained by the RAF.

The new fighter should be armed with 20-mm guns to overcome the armor of the German bombers during a stern attack but should also be equipped with a barbette dorsal for Defiant-style belly attacks.

It would be necessary to build a large and heavy aircraft, capable of carrying a large amount of fuel and electronic equipment with the best available AI radar, excellent communications equipment, and a radar altimeter, but also with the ability to turn very tightly at slow speeds, to elude the attack of enemy night fighters and to avoid losing radar contact while the target attempted to perform evasive maneuvers.

To achieve this, the future fighter would have to be powered by engines of at least 2,000 hp, capable of taking off under overload conditions and operating at maximum power during a prolonged chase.

Northrop hoped to start serial production within a year, but such a complicated project needed too long to become a reality and when the aircraft entered service forty months later, under the Black Widow P-61 codename, the Third Reich was practically defeated.

The first Black Widows sent to the European Theatre, on May 23, 1944, were thirty-five P-61 A-5 aircraft from the second production batch, equipped with R-2800-65W (water-methanol war emergency power) 2,250 hp. radial engines with PT-13G2 Stromberg injection carburettors and gear-driven, two-speed, two-stage superchargers, to hunt the Junkers Ju 188 German bombers at any altitude and fast enough to intercept the V-1 missiles.

The P-61 did not accelerate as rapidly as the P-38, although the heavy plane had dived without compressibility problems at 425 mph and 25,000 feet.

The Black Widow used two radars: an AI SCR-720A (with 10 cm wavelength, 150 Kw power output, 8 Km range and one parabolic antenna RC-286 with 70 cm of diameter and azimuth receiver antennas fitted on the fuselage sides) and one AN/APS-13 tail warning radar designed for night fighting in Europe. The main radar included SCR-695 IFF and beacon/homing device. The P-61 used flame-dampening stacks to eliminate exhaust glow, RC-36 interphone, RC-255A radio set, SCR-718 radio-altimeter, SCR-729 radio-navigation device, SCR-522 radio-set, MN-26 C radio-compass, FR12 A3 gyroscopic fire-control computer and was armed with 4 x 20-mm cannons.

In Airborne Intercept mode the SCR-720A had a range of five miles, the unit also could function as airborne beacon/homing device, navigational aid and IFF interrogator-responder.

The AI radar could be trained in both azimuth and elevation to allow tracking a single target and to allow scanning a larger section of the sky ahead of the fighter.

Black Widows of the A-5 series lacked external drop tanks and their range was only about 1,200 miles.

The paint scheme used in the A-5 series was Dull Olive Drab No. 21 (FS-34087/FS-24098) upper surfaces, Neutral Grey No. 23 (FS-36270/FS-36137) undersides, yellow serials and Black/White invasion stripes in wings and tail booms.

The A-10 series were painted overall in Glossy Jet Black, a paint developed by the Radiation Laboratory at the Massachusetts Institute of Technology (MIT) that reflected the searchlights beams, making the Black Widow practically invisible for 80 per cent of the time that the spotlight passed.

The Plexiglas radome was partially transparent and melted in the sun deforming and preventing the movement of the scanner-receiver antenna, spinning at 360 rpm. This radome was painted internally in reflective Gloss White (FS 17875) and lead paint was sprayed on the underside of the radome to eliminate ground clutter.

In later versions the Plexiglas was replaced by fiberglass painted Satin Black.

The invasion stripes of the A-10 series were painted only in the under surfaces.

In the autumn of 1944, all the Widows based at the Coulommiers and Chateaudun French airfields, were painted in Glossy Jet Black.

In November, the 422nd received one P-61 B-15 replacement aircraft, with GE A-4 dorsal barbette, painted in Glossy Jet Black, with Dull Red serials but without invasion stripes.

The new fighter had 8 inches extended nose, to accommodate the SCR-720C radar, and was fitted with one AN/APN-1 (low altitude) radio-altimeter.

The sophisticated Black Widow required a high maintenance work, but the replacement parts were scarce in the European Theatre, keeping 50 per cent planes serviceable was difficult and combat readiness suffered as a result.

To facilitate interceptions, the night fighter would to be airborne, orbiting and waiting, instead of taking off every time a bogey appeared on the radar screen. The 422nd NFS fighters used to perform four hours nighttime combat air patrols (CAP), flying at altitudes of 10,000-20,000 feet.

Throughout the duration of the CAP missions the crews preferred to use the oxygen masks, because combat experience showed an increase in night vision of 40 per cent with the continuous use of oxygen.

When the early warning radar detected a bogey, the night fighter was vectored by the GCI to be placed at the same altitude as the intruder. The P-61A-5 was equipped with an SCR-718 radio altimeter that allowed it to fly at the altitude indicated by the AN/TPS-1 ground radar.

Using their RC-255-A VHF radio and MN-26 C radio compass, the night fighter was directed by the GCI to a point several miles to the rear of the intruder.

Control radar guidance needed between fifteen and twenty-five minutes before the SCR-720 could detect the target at ranges between eight miles and 300 feet.

After detection, the fighter should increase its speed up to 372 mph to intercept the intruder before reaching the antiaircraft artillery zone, within ten miles of the GCI.

If the fighter approached too fast, it would overshoot the target. To avoid this, it should use its slotted flaps and perforated spoilers to decelerate rapidly to only 70 mph.

At 500 feet range the fighter made a hard as possible 180-degree turn, stood behind the target at a range of 2,000 feet and started adjustments to synchronize its speed with that of the target.

During combat, high-g aerobatics were forbidden because they affected the operation of radar tubes.

The IFF transmissions were not always reliable and visual contact was needed to ensure recognition of the target as required by the rules of engagement.

The pilot could use 5.8 power night binoculars connected to the gunsight, but sometimes visual contact was not possible because of clouds or rain.

Visual identification required to silhouette the target against the sky from below, at the very close range of 850-250 feet, depending on the weather and moonlight.

When the target was identified as a bandit (enemy plane) by its shape and size, the fighter had to position back behind to fire from the shortest possible distance. Four illuminated ‘tick marks’ on the gunsight allowed the pilot to determine the target range.

The Black Widow was armed with four 20-mm AN/M2 belly mounted cannons loaded with armor piercing, incendiary and high explosive shells but without tracers. It was discovered that tracers alerted the enemy and degraded the night vision of the pilot.

Sometimes the target also shot muzzle flashes and tracers could cause the US pilot to lose his night vision, which would force them to abort the attack. When they recovered the night vision, fifteen minutes later, the enemy would have already completed his mission.

The quadruple 0.50 caliber GE A-4 dorsal barbette was capable of a full 360-degree rotation in azimuth and 90-degree in elevation. It could be remotely controlled by the gunner using a Type N-6 gunsight and could be used to engage any target in the hemisphere, above and to the sides of the night fighter.

The turret could be locked forward to be fired by the pilot against targets ahead of the aircraft, using a Type L-1 gunsight.

In theory, the GE A-4 could also be used by the radar operator as a rear defensive armament. But it was of little practical use as the radar screens degraded his night vision. Its possible adversary would have been a Messerschmitt Bf 109 G-6 all-weather Moskitojäger, or a Focke-Wulf Fw 190 A-5 Wilde Sau night fighter crewed by specially selected pilots for their excellent night vision.

Early combat experience with the P-61 A-1 showed that the turret caused severe tail buffeting at high speeds, due to aerodynamic rough air flow when the turret was rotated.

Northrop decided to delete the dorsal barbette from production aircraft beginning with the thirty-eight aircraft. The removal of 1,600 pounds of weight increased the top speed by 20 mph.

When the buffeting problem had been lessened, a new turret with only two 0.50 caliber machine guns and GE2C FR12A3 gyroscopic fire control computer, was re-introduced in the P-61 B-11 series and the later model with four 0.50 caliber guns in the B-15 series.

The first Black Widows sent to the Pacific Theatre were seven P-61 A-1 night fighters, from the first production batch, equipped with 2,000 hp. supercharged engines.

Black Widows of the A-1series lacked external drop tanks, and their range was only about 1,200 miles. To make the long flight over the sea it was necessary to remove the dorsal barbettes and replace them with modified ex-B-24s bomb bay ferry tanks (with AN-F-48 100/130 octane fuel) that protruded above the fuselage.

The ferry tanks were replaced in Isley Field by fixed turrets, a field modification with four forward-firing M2 Browning heavy machine guns.
Early warning ground radars could pick the intruders at ranges of 150 miles. To confuse US defenses, Japanese bombers used chaff as they approached, thirty miles out of Saipan. This tactic had the effect of blocking the older SCR-270 (3-meter) and SCR-527 (1.5 meter) radar sets but it did not manage to cancel the detection capacity of the new SCR-615 (early warning) and AN/TPS-1 (height finder) ‘centimetric’ radars.

The Black Widow’s SCR-720 A (airborne interception) radar, operating in 10 cm wavelength, did not prove very vulnerable to chaff interference, but the Japanese signal intelligence services, monitoring US radio transmissions, were able to track the position of the American airplanes by their IFF emissions.

At other times the bogey mysteriously disappeared from ground control and airborne radar screens. It was a Japanese tactic using floatplanes that would land on water to confuse the US defenses.

In Saipan the P-61 A-1 proved too slow in climbing to operational altitudes and performed poorly above 25,000 feet.

The huge fighter lacked the speed advantage necessary to intercept the high-flying Betty bombers powered by supercharged engines.

The Black Widow used a system of flame dampening to reduce the visibility of the engine exhaust at night, but the Japanese did not use flame dampers because it reduced the power of the engines, and their exhaust could be seen up to 5,000 feet away.

Visual identification of the bogey was risky because sometimes bombers were escorted by Mitsubishi A6M5 Zeke fighters and the radar operator could not see them because their night vision was degraded by the radar screen glare.

In the Pacific Theatre, visual identification was especially complicated because most of the aircraft, used by both sides, were powered by radial engines and had very similar silhouettes.

In addition, the Japanese used several indigenous versions of American airplanes: Douglas DC-2 Tess, Douglas DC-3/Showa L2D Tabby, Lockheed Model 14 Thelma, Seversky A8V Dick and Vultee V-11G Millie.

In 1945, some of these models were used in suicide missions. The L2D carried airborne commandos of the Kaoru and Takachiho suicide units that carried out attacks against the B-29 bases in Guam, Tinian and Saipan.

In the fall of 1944, the 6th NFS received several P-61 A-5 fighters with R-2800-65 two-stage, two-speed supercharged engines and P-61A-10 with R-2800-65 W water injection and 2250 hp. war emergency power, that could climb to 20,000 feet in 8.5 minutes.

The new fighters arrived at Saipan without dorsal barbettes and painted in Glossy Jet Black.

The second squadron that received the Black Widows in May 1944 was the 419th NFS based in Buka Airfield-Bougainville.

These P-61 A-1 airplanes were shipped in crates, with the wings disassembled, and still retained their original General Electric A-4 remotely controlled, full-traverse, upper turrets.

In theory, the GE A-4 could also be used by the radar operator as a rear defensive armament, but it was of little practical use as the radar screens degraded his night vision. Its possible adversary would have been a Mitsubishi A6M5, or a Nakajima J1N1 night fighter crewed by specially selected pilots for their excellent night vision, enhanced with M-33-N Philopon methamphetamine.

The P-61 A-1 fighters of the 419th NFS were painted in Olive Drab/Neutral Grey with Gloss White radomes and three digit white numbers on the nose.

In August 1945, the 419th received several Glossy Jet Black P-61 B-1 night fighters fitted with SCR-720 C AI radar, AN/APS-13 tail warning radar, SCR-718 radio-altimeter, IFF/beacon locators, resin-impregnated fiberglass radomes in the extended nose and night-vision binoculars connected to the pilot’s rangefinder-gunsight Type LY-3N. The new fighters were delivered without turrets, and it was necessary to make a field modification with four (fixed) forward-firing M2 Browning heavy machine guns.

The P-61 A-10 fighters were delivered with water injection boosted engines but without turrets. They were modified with the installation of fixed gun barbettes in Hollandia.

At the end of 1944 the squadron received several P-61 B-15 fighters fitted with GE A-4 dorsal barbettes.

In June 1944, the 421st NFS received some P-61 A-1 armed with GE A-4 dorsal barbettes. These airplanes were delivered with Olive Drab/ Neutral Grey camouflage scheme and Satin Black nose radomes.

At the end of 1944 the 421st squadron received the new Glossy Jet Black P-61 B-10 fighters, fitted with four underwing hard points and four 310 US gallon drop tanks for 3,000 miles extended range.

The 547th NFS, based at Owi Airfield-New Guinea, did not receive its P-61 A-10 until September 1944.

In January 1945 the squadron was moved to Philippines and received some P-61 B-1 nigh fighters fitted with SCR-720C AI and SCR-718 tail warning radars but without gun turrets. These aircraft were field-modified as P-61 B-2 with two underwing hard points to carry external ordnance and night interdiction missions were carried out on Japanese airfields.

Between October 1944 and August 1945, the 548th NFS used five types of Black Widows: P-61 A-11, received in Hawaii; P-61 B-1, in Saipan; P-61 B-2 and B-6, in Iwo Jima and P-61 B-15 in Le Shima.

All aircraft were painted with the Glossy Jet Black scheme and armed with fixed forward gun turrets, except the B-15s ones which had been delivered with GE A-4 barbettes.

The squadron was used in CAP defense over the B-29s airfields on Saipan and Iwo Jima. It also provided night escort to the Superfortress against the Japanese night fighters and performed Heckler nighttime ground attack raids on the Japanese mainland.

The 549th NFS, based at Hickam Field-Hawaii, received its P-61 A-5 night fighters in October 1944 and was moved to East Field-Saipan in February 1945, to provide night coverage to the B-29s bases on Saipan and Guam.

In March, the squadron received some P-61 B-6 and B-15 Black Widows at Central Field-Iwo Jima. These fighters, fitted with four 300 US gallon drop tanks, flew long CAP missions over water and night interdiction missions over Eastern China and Chichi Jima Island.

The USAAF used two other Black Widows squadrons against the Japanese in the China-Burma-India (CBI) Theater.

All Black Widows operating at the CBI Theatre were of the A-10 model, without gun turrets.

During the war the Black Widows night fighters downed a total of 107 enemy airplanes and 18 flying bombs.

Northrop P-61 A-1 technical data

Wingspan: 66 ft. (20.11 m); length: 48.8 ft. (14.88 m); height: 14 ft. (4.31 m); wing area: 662 sq. ft. (61.49 sq. m); max weight: 27,700 lb. (12,565 kg); max speed: 372 mph (599 km/h); service ceiling: 34,000 ft. (10,363 m); range: 1,210 mi (1,974 km); power plant: two Pratt & Whitney R-2800-10 air-cooled radial engines each rated at 2,000 hp.; armament: 4x20 mm AN/M2 cannon.

Northrop P-61 A-5 technical data

Wingspan: 66 ft. (20.11 m); length: 48.9 ft. (14.90 m); height: 14 ft. (4.31 m); wing area: 662 sq. ft. (61.49 sq. m); max weight: 27,675 lb. (12,537 kg); max speed: 369 mph (594 km/h); service ceiling: 33,620 ft. (10,250 m); range: 1,150 mi (1,850 km); power plant: two Pratt & Whitney R-2800-65W (water-methanol injection) air-cooled radial engines each rated at 2,250 hp.; armament: 4x20 mm AN/M2 cannon.

Northrop P-61 A-10 technical data

Wingspan: 66 ft. (20.11 m); length: 48.9 ft. (14.90 m); height: 14 ft. (4.31 m); wing area: 662 sq. ft. (61.49 sq. m); max weight: 27,350 lb. (12,394 kg); max speed: 362 mph (583 km/h); service ceiling: 33,980 ft. (10,360 m); range: 1,206 mi (1,940 km); power plant: two Pratt & Whitney R-2800-65W (water-methanol injection) air-cooled radial engines each rated at 2,250 hp.; armament: 4x20 mm AN/M2 cannon.

Northrop P-61 B-15 technical data

Wingspan: 66 ft. (20.11 m); length: 49.5 ft. (15.11 m); height: 14 ft. (4.31 m); wing area: 662 sq. ft. (61.49 sq. m); max weight: 29,700 lb. (13,472 kg); max speed: 366 mph (589 km/h); service ceiling: 33,100 ft. (10,089 m); range: 3,000 mi (4,228 km); power plant: two Pratt & Whitney R-2800-65 air-cooled radial engines each rated at 2,250 hp.; armament: 4x20 mm AN/M2 cannon and 4x0.50-in, M2 Browning machine guns.
 

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