Dornier P.238
The Dornier Do 335 was a formidable combat machine, with a great development potential that was interrupted by the end of the WWII.
The
push-pull formula, combined with the use of different types of engines, proved that it could satisfy the main needs of the Luftwaffe by the end of 1943.
- Conventional night fighter (Do 435 C-1, C-2, D-1 & D-2)
- Mixed power night fighter (Do 335 A&B)
- Antitank,
zerstörer and fighter bomber (Do 335 B-2, B-1 & A-1)
- Light bomber (Do 335 A-2)
- Trainer (Do 335 B-5)
- Recce (Do 435 B-4)
- High altitude Recce (Do 335 B-4)
- Long range Recce (Do 335 Z)
This design served as the base for the four engine, 8,000 km range, Junkers Ju 635 bomber.
The last
push-pull Dornier was the P.238 that derived from the Do 435 with elongated fuselage of up to 17.10 m. and Jumo 222 E/F engines.
The P.238/1 had the wing and tail surfaces of a standard Do 335 and it was presented in two versions:
zerstörer (A-1) and fighter bomber (B-1).
The P.238/2 had the new wing with a 18.33 m span designed by Heinkel for the Do 335 B-4 and it was presented in the escort fighter version (A-2) and high altitude interceptor (B-2) capable to face the Boeing B-29 of the Allies.
There are some night fighter versions, as the time when the project was presented the old
Hirschgeweigh antennae of the Lichtenstein radar had been replaced by parabolic ones, designed to be installed on the nose cone of the aircraft. And this was not possible in the P.238.
For this reason, and for the excessive drag produced by the frontal cooler, the manufacturing of the Do 435 has already been discarded on 28 August 1944. By the end of that year, the Dornier Project Office decided to interrupt the
push-pull developments in favour of the P.247 and P.252 projects, which possessed more advanced aerodynamics and allowed higher speed and the installation of last generation radars.
Technical Data
| Type | single seat zerstörer, escort fighter and high altitude interceptor | |
| Airframe | Light alloy structure and cladding with wooden outer wings panels in the P.238/2 | | |
| Cockpit | Pressurised, control heating, frontal armour against 12.7 mm shelling and from the rear against 20 mm. Heinkel kartusche ejector seat | | |
| Undercarriage | Tricycle type. The main legs retracted inwards and the front gear retractable to the rear after switching 90º to lie flat in the wheel bay | | |
| Engine | Two (tractor and pusher) Jumo 222 E/F, 24 cylinder supercharged, liquid cooled, Star with six banks of four cylinder each and 2,465 hp. (3,000 with MW-50 injection) at take-off, driving two Junkers VS-19 four blade airscrews with a 3.60 m. diameter and fed by two stage, three speeds superchargers with three intercoolers each. | | |
| Armament | Two MG 151/20 (synchro) cannons in the fuselage and two MK 103/30 cannons in the wings. | | |
| Wingspan | 13.80 m. (P.238/1) 18.33 m (P.238/2) | | |
| Length | 17.10 m | | |
| Height | 5.30 m | | |
| Wing area | 38.50 sq. m (P.238/1) 51 sq. m (P.238/2) | | |
| Estimated Max speed | 800 km/h (P.238/1) 770 km/h (P.238/2) | | |
| Service ceiling | 14,000 m (P.238/2) | | |
| Electronics | One EZ42 gyro-gunsight, FuG 16 ZY VHF transmitter/receiver, FuG 25a IFF radio set, FuG 125, K23 automatic pilot. | | |