TM-E 30-451 Handbook on German Military Forces   LoneSentry.com

[DISCLAIMER: The following text is taken from the U.S. War Department Technical Manual, TM-E 30-451: Handbook on German Military Forces published in March 1945. — Figures and illustrations are not reproduced, see source details. — As with all wartime intelligence information, data may be incomplete or inaccurate. No attempt has been made to update or correct the text. — Any views or opinions expressed do not necessarily represent those of the website.]


CHAPTER X. GERMAN AIR FORCE

Section V. EQUIPMENT

5. Tabulated Data

BOMBERS

Aircraft Manufacturer and Model  Type  Normal Crew Engines, Model and Rated HP Wing Span Max. Speed MPH Radius
of
Action
(40%
Normal
Range)
(Miles)
Typical Armament Bomb or Freight Load (Pounds) Normal Weight (Pounds) Service Ceiling (Feet)
Single-Engine
(1) Junkers JU 87 (Stuka) (Dive-bomber)
Inverted
Gull
Wing
2 1xJumo 211 J 12 cyl. liquid-cooled—1335 HP 45' 4" 255 at 13,500 ft. 280 Forward fuselage
2x12.7-mm.
Forward wings
2x7.9- or 37-mm.
Dorsal
2x7.9-mm.
2,200 12,600 18,500
(2) Focke-Wulf FW 190 (Fighter-bomber) LWM 1 1xBMW 801D 14 cyl. twin-row, air-cooled radial—1755 HP 34' 6" 370 at 19,000 ft. 165 Forward fuselage
2x7.9- or 13-mm.
Forward wings
2/4x20-mm.
550 9,800 31,500
Twin-Engine
(1) Henschel HS 129
LWM 1 2xGnome-Rhone 14M 04/05, 14 cyl. twin-row, air-cooled radial—800 HP 44' 6" 275 at 9,000 ft. 220 Forward fuselage 2x7.9-mm plus 2x15- or 20-mm plus 1x30-mm or 6x7.9-mm.
Dorsal
Possibly 2x20-mm.
220 11,400 25,000
(2) Dornier DO 217 K-2 HWM 4 2xBMW 801 A-2 14 cyl. twin-row, air-cooled radial—1595 HP (est.) 80' 6" 325 at 20,000 ft. 470 Forward fuselage
2x7.9-mm or larger caliber
Dorsal
1x13-mm.
Lateral
2x7.9-mm.
Ventral
1x13-mm.
Tail
4x7.9-mm.
6,600 35,000 25,000
(3) Heinkel HE 111 LWM 5/6 2xJumo 211F 12 cyl. liquid-cooled—1230 HP 74' 252 at 14,000 ft. 215 Forward fuselage
1x20-mm plus 1/2x7.9-mm.
Dorsal
1x13-mm.
Ventral
2x7.9-mm.
2,020 25,500 26,000
(4) Heinkel HE 177 MWM 7 2xDB610 (DB 605 doubled) 24 cyl. liquid-cooled—2800 HP 103' 6" 300 at 20,000 ft. 460 Forward fuselage
1x7.9-mm.
Forward dorsal
1/2x13-mm.
Rear dorsal
1/2x13-mm.
Forward ventral
1x20-mm.
Rear ventral
1x13-mm.
Tail
1x20-mm.
12,320 68,000 21,000
(5) Junkers JU 88 A4 LWM 4 2xJumo 211J 12 cyl. liquid-cooled—1335 HP 65' 11" 291 at 14,000 ft. 490 Forward fuselage
1/2x7.9-mm and/or 1x20-mm.
Dorsal
2x7.9-mm.
Ventral
2x7.9-mm.
4,400 28,300 24,200
(6) Junkers JU 88 S LWM 3 2xBMW 801 G-2 14 cyl. twin-row, air-cooled radial—1530 HP (est.) 65' 11" 339 at 20,000 ft. 245 Forward fuselage
1x7.9-mm.
Dorsal
1x13-mm.
1,980 26,400 30,000
(7) Junkers JU 188 (Estimated performance) LWM 4 2xJumo 213 A/1 12 cyl. liquid-cooled—1700 HP (est.) 72' 6" 325 at 20,000 ft. 320 Forward fuselage
1x20-mm.
Cockpit rear
1x13-mm.
Dorsal turret
1x20-mm.
Ventral
2x7.9-mm or 1x13-mm.
4,400   33/34,000
(8) Messerschmitt ME 110G LWM 2 2xDB 605B, 12 cyl. liquid-cooled—1460 HP 53' 11" 325 at 19,000 ft. 250 Forward fuselage
4x7.9-mm plus 2x20- or 30-mm.
Dorsal
2x7.9-mm.
2,640 20,900 29,000
Four-Engine
Focke-Wulf FW 200
LWM 5/7 4xBramo "FAFNIR" 323 R, 9 cyl. air-cooled radial—1,000 HP 107' 7" 240 at 13,000 ft. 750 Dorsal forward
1x15- or 20-mm.
Rear dorsal
1x13-mm.
Lateral
2/4x7.9-mm or 2x13-mm.
Forward ventral
1x15- or 20-mm.
Rear ventral
1x7.9-, 13-, or 20-mm.
3,600 50,000 20,500
 


  

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