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  2. BMD-1 - Wikipedia

    en.wikipedia.org/wiki/BMD-1

    The BMD-1 has a maximum road speed of 80 kilometers per hour, reduced to around 45 kilometers per hour off-road and 10 kilometers per hour while swimming. [2] [3] [5] [10] The BMD-1 can climb 0.8-meter-high (2.6 ft) vertical obstacles, cross 1.6-meter-wide (5.2 ft) trenches, and 30% side slopes. It can climb 60% gradients.

  3. 2A28 Grom - Wikipedia

    en.wikipedia.org/wiki/2A28_Grom

    The 2A28 Grom also known as KBP 2A28 Grom, is the main armament of the Soviet-designed BMP-1 and BMD-1 infantry fighting vehicles.It is a 73 mm low pressure smoothbore semi-automatic gun with a wedge breech block. [1]

  4. 2S25 Sprut-SD - Wikipedia

    en.wikipedia.org/wiki/2S25_Sprut-SD

    In the early 1990s, the Volgograd tractor plant created a new self-propelled tank destroyer based on a modified prototype light tank classified as Object 934. [1] The plant was also the designer and manufacturer of the BMD-1, BMD-2, BMD-3 and latest BMD-4 airborne combat vehicles that are used by the Russian Air Assault Divisions. After the ...

  5. BMD-4 - Wikipedia

    en.wikipedia.org/wiki/BMD-4

    The maximum speed on a highway is 70 km/h and the BMD-4 can maneuver on a 60° gradient and a 35° [14] side slope. The BMD-4 can cross 1.8 m trenches and climb 0.8 m tall obstacles. [24] This vehicle's suspension is hydropneumatic and giving an adjustable ground clearing of 130–530 mm with the normal road clearance being 450 mm.

  6. BMP development - Wikipedia

    en.wikipedia.org/wiki/BMP_Development

    Although the BMP-1 was a revolutionary design, its main armament, the 2A28 Grom and the 9S428 ATGM launcher capable of firing the 9M14 Malyutka (NATO: AT-3A Sagger A) and the 9M14M Malyutka-M (NATO: AT-3B Sagger B) ATGMs, quickly became obsolete. Therefore, the Soviet Union decided to produce an updated and improved version of the BMP-1.

  7. BMD-2 - Wikipedia

    en.wikipedia.org/wiki/BMD-2

    As soon as the rods touch the ground a retrorocket fires, slowing the BMD to a descending speed between 6 m/s and 7 m/s and giving it a relatively soft landing. [5] It allowed a BMD to be relatively safely parachuted with both the driver and the gunner. This system entered service in 1975 for the BMD-1, and was always used for the BMD-2 afterwards.