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KTDU 80

  • KTDU-80
  • The KTDU-80 (Russian: Корректирующе-Тормозная Двигательная Установка, КТДУ) is the latest of a family of integrated propulsion system that KB KhIMMASH

    KTDU-80

    KTDU-80

    KTDU-80

  • S5.80
  • Liquid pressure-fed rocket engine

    propulsion module KTDU-80, and its sibling, the S5.79 rocket engine, is still used as the main propulsion of the Zvezda ISS module. The S5.80 generates 2.95 kN

    S5.80

    S5.80

  • Soyuz (spacecraft)
  • Series of spacecraft designed for the Soviet space programme

    Evaluation of Thermal Protection System (TPS) Penetration Characteristics "KTDU-80". www.astronautix.com. Retrieved 21 October 2022. Anatoly Zak (3 August

    Soyuz (spacecraft)

    Soyuz (spacecraft)

    Soyuz_(spacecraft)

  • 11D428
  • Model of Soviet liquid pressure-fed rocket engine

    crew-rated spacecraft propulsion applications. It is currently used in the KTDU-80 spacecraft propulsion module. The previous version, the 11D428A (manufacturer's

    11D428

    11D428

  • Research and Development Institute of Mechanical Engineering
  • Subsidiary of Roscosmos

    11D428A-16 (a.k.a. RDMT-135M): 135 N (30 lbf) N2O4/UDMH thruster. Used on the KTDU-80. 11D428AF-16: N2O4/UDMH thrusters used by the Fobos-Grunt space mission

    Research and Development Institute of Mechanical Engineering

    Research_and_Development_Institute_of_Mechanical_Engineering

  • A.M. Isayev Chemical Engineering Design Bureau
  • DMT-500 DMT-600 DMT-1000 DMT-2200 Main propulsion S5.80 S5.92 S5.98 KVD-1 Propulsion Modules KTDU-80 Experimental Engines S5.86.1000-0 Engines that are

    A.M. Isayev Chemical Engineering Design Bureau

    A.M. Isayev Chemical Engineering Design Bureau

    A.M._Isayev_Chemical_Engineering_Design_Bureau

  • S5.142
  • was used in KTDU-80 propulsion module from the Soyuz-TM to the Soyuz-TMA-M, as the low thrust thruster (DPO-M). As of the Soyuz MS, KTDU-80 does not use

    S5.142

    S5.142

  • Soyuz-TM
  • Fourth-generation of the Soyuz spacecraft

    and lightweight material for the parachute domes. It also featured a new KTDU-80 propulsion module that permitted the Soyuz-TM to maneuver independently

    Soyuz-TM

    Soyuz-TM

    Soyuz-TM

  • Progress-M1
  • Russian spacecraft which is used to resupply space stations

    The spacecraft had a tare weight of 5,050 kilograms (11,130 lb), and its KTDU-80 engine, producing 2,950 newtons (660 lbf) of thrust, used up to 892 kilograms

    Progress-M1

    Progress-M1

    Progress-M1

  • Venera program
  • Soviet program that explored Venus with multiple probes

    KTDU-425A liquid-propellant engine used on Venera spacecraft from 9 to 16

    Venera program

    Venera program

    Venera_program

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