Be-10 was given the NATO code name "Mallow".
The deep streamlined hull, surmounted by the pilot's blister canopy, had a single step and the long narrow planing bottom extended to the tail. The extreme tip of the bulbous nose was glazed, here the navigator was seated. Defensive armament consisted of two NR-23 0.9 in (23 mm) cannon in a tail barbette beneath the radio-operator/gunner's glazed position. All three crew were seated on ejection seats. In the weapons bay immediately after the bottom step four 1,695 lb (769 kg) torpedoes could be carried or up 7,275 lb (3,300 kg) bombs, mines or depth charges.
Four aircraft, reported to the FAI as Beriev M-10, established twelve world records:
July 22, 1961 (pilot Nikolai Andrievskii and two crew)
speed over 9.5-15.5 mls (15-25 km) course: 566.69 mph (912 kmh).
September 3, 1961 (pilot Georgii Buryanov and two crew)
speed over 621 mls (1,000 km) closed circuit without payload, and with payloads of 2,204 lb (1,000 kg) and 4,409 lb (2,000 kg): 544.1 mph (875.86 kmh).
September 8, 1961 (pilot Georgii Buryanov and two crew)
altitude without payload, and with payloads of 2,204 lb (1,000 kg), 4,409 lb (2,000 kg) and 11,023 lb (5,000 kg): 14,062 m (46,135 ft).
9-12 September, 1961 (pilot Georgii Buryanov and two crew)
altitude with 22,046 lb (10,000 kg): 48,331 ft (12,733 m); altitude with 33,069 lb (15,000 kg): 38,357 ft (11,997 m); maximum load to 6,560 ft (2,000 m): 33,523 lb (15,206 kg); and altitude: 49,687 ft (14,962 m).
Eventually two squadrons of the Black Sea Fleet were equipped with the
Be-10, however, limited operational usefulness led to an early retirement.
Span: 93 ft 10 in (28.6 m)
Length: 100 ft 9.5 in (30.72 m)
Wing area: 1,399 sq.ft (130 sq.m)
Weight empty: 58,420 lb (26,500 kg)
Loaded weight: 99,206 lb (45,000 kg)
Max speed: 567 mph (912 kmh) at sea level
Cruise speed: 488 mph (785 kmh)
Landing speed: 137 mph (220 kmh)
Climb: to 16,404 ft (5,000 m) 7 min