Martin XB-16

This article needs additional citations for verification. Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed. Find sources: "Martin XB-16" – news · newspapers · books · scholar · JSTOR (April 2017) (Learn how and when to remove this template message)

The Martin XB-16, company designation Model 145, was a projected heavy bomber designed in the United States during the 1930s.

Design and development

The XB-16 was designed to meet the United States Army Air Corps (USAAC) request for a bomber that could carry 2,500 lb (1,100 kg) of bombs 5,000 mi (8,000 km; 4,300 nmi).

The XB-16 (Model 145A) was to use four

The XB-16 was canceled for essentially the same reason that the Boeing XB-15 project was, as it was not fast enough to meet the requirements set by the Army. Since both were canceled around the same time, Martin did not have time to produce an XB-16.

Specifications (Model 145A)

Data from U.S. bombers, 1928 to 1980s^[1]

General characteristics

• Crew: ten
• Length: 114 ft 10 in (35 m)
• Wingspan: 140 ft (43 m)
  

  Model 145B: 173 ft (53 m)

• Gross weight: 65,000 lb (29,484 kg)
  

  Model 145B: 104,880 lb (47,570 kg)

• Fuel capacity: 4,238 US gal (16,040 L; 3,529 imp gal)
• Powerplant: 4 ×
  Allison V-1710-3
  V-12 liquid-cooled piston engines, 1,000 hp (750 kW) each (Model 145B ×6)

Performance

• Maximum speed: 237 mph (381 km/h, 206 kn) at 20,000 ft (6,100 m)
• Cruise speed: 140 mph (230 km/h, 120 kn)
• Range: 5,000 mi (8,000 km, 4,300 nmi)
• Combat range: 3,200 mi (5,100 km, 2,800 nmi) with 12,180 lb (5,520 kg) of bombs
• Endurance: 18 hours
• Service ceiling: 22,500 ft (6,900 m)
• Rate of climb: 740 ft/min (3.8 m/s)
• Power/mass: 0.049 hp/lb (0.080 kW/kg)

Armament

• Bombs: 12,180 lb (5,520 kg) of bombs

See also

Aircraft of comparable role, configuration, and era

• Boeing XB-15
• Boeing Y1B-20
• Douglas XB-19

Related lists

• List of bomber aircraft
• List of military aircraft of the United States

References