/Airplanes/Allies/France/06-Aeronautic/Late-298/Data/Late-298.htm | Update: -

 

Latécoère Laté-298/299

GENERAL DATA
-
Recce/Torpedo-Bomber
Floatplane (Laté-298),
Carrier-borne variant (Laté-299)
2 (reconnaissance)
3 (torpedo-bomber)
Latécoère, Breguet
121 (Laté-298), 2 prototypes (Laté-299)
6 May 1936 (Laté-298)
7 July 1939 (Laté-299)

28 October 1938 (Laté-298)
- (Laté-299)

 

Variants
First production variant.
Variant with folding wings for use on seaplane carriers; observation post added; crew of four.
Similar to 298B without the folding wings.
Observation variant with weapon fixation replaced by an observer's gondola; one prototype built.
A three-seat reconnaissance-torpedo bomber derived from the Late 298, powered by a 920 hp Hispano-Suiza 12Y-43, first flight on 7 July 1939
(two prototypes built).

 

DIMENSIONS
12.56 m
3085 kg (Laté-298), 3064 kg (Laté-299)
15.5 m
4533 kg (Laté-298), 4550 kg (Laté-299)
5.25 m (Laté-298), 4.46 m (Laté-299)
4800kg (Laté-298), 4650 kg (Laté-299)
31.6 m²
? kg/m²

 

ARMAMENT
3 x 7.5 mm (0.295 in) Dame MG *
?
-
-
1 x 400 mm (670 kg) DAI torpedo or 450 mm (750 kg) DA torpedo or 500 kg (Laté-298), 900 kg (Laté-299) of bombs

(*) 2 wings-mounted, 1 flexible in rear cockpit

POWERPLANT
1 × Hispano-Suiza 12Ycrs-1 (Laté-298)
1 Hispano-Suiza 12Y-43 (Laté-299)
V-12 liquid-cooled piston, 36.05 L
880 hp (Laté-298)
920 hp (Laté-299)
194.13 hp / ton * (Laté-298)
202.20 hp / ton * (Laté-299)
Fuel capacity internal: ? L, Fuel capacity external: extra 535 L fuel tank

(*) with loaded weight

PERFORMANCES
295 km/h at 2500 m (Laté-298)
356 km/h at 2500 m (Laté-299)
243 km/h (Laté-298)
275 km/h (Laté-299)
? km/h
5500 m (Laté-298), 6600 m (Laté-299)
? m/s
1000-1500 km, 800 km w/ max. payload

(*) vitesse de décrochage

Sources
aviastar.org  

 

Drawings

 

 

 

Navy Bombers