NIIMash has an extensive experience in design of testing stands, measurement and control as well as certifications. They also have a line of custom built air separation plants. They also have extensive experience in rotational forming of metals. The list of space rated products is extensive and is the following:
Current propulsion products Engines in current production: • Propulsion •
Experimental Reactive Control System Module •
KDU 11D414NS •
Fobos-Grunt Sample Return Spacecraft Propulsion System •
Fobos-Grunt Spacecraft Thruster Modules • Thrusters •
MD5 (
RDMT-5): Cold gas thruster. •
MD08 (a.k.a.
RDMT-8): Cold gas thrusters used on the
Ekspress satellite series. •
MD08-02 (a.k.a.
RDMT-8-02): Cold gas thruster: Used on the Fobos-Grunt Sample Return Spacecraft. •
11D428A-16 (a.k.a.
RDMT-135M): N2O4/UDMH thruster. Used on the
KTDU-80. •
11D428AF-16: N2O4/UDMH thrusters used by the Fobos-Grunt space mission. •
11D457: N2O4/UDMH thrusters used by the
Resurs-DK No.1. •
11D457F: N2O4/UDMH thrusters used by the Fobos-Grunt space mission. •
11D458 (a.k.a.
RDMT-400): N2O4/UDMH thrusters used by the
Functional Cargo Block based modules and the
Briz upper stage. •
11D458F (a.k.a.
RDMT-400F): N2O4/UDMH thrusters used by the Fobos-Grunt space mission. •
11D458M (a.k.a.
RDMT-400M): N2O4/UDMH thrusters used by the
Briz-M upper stage. •
17D16 (a.k.a.
RDMT-200K): GOX/Kerosene thruster. Used the
Buran DO thrusters. •
17D58E: N2O4/UDMH thrusters used by the
Briz-M upper stage. •
17D58EF: N2O4/UDMH thrusters used by the Fobos-Grunt space mission. • Experimental thursters •
RDMT2600:
Ethanol/
GOX thruster designed attitude control when the air density is so low that the control surfaces are ineffective. •
RDMT10: thruster designed for space applications. • Propellant tanks & high pressure gas vessels •
Composite high pressure Xenon storage tank: Xenon storage unit for electric propulsion spacecraft. •
Composite Vessel: General high pressure vessel used on the Fobos-Grunt mission. •
Monopropellant Tank with Stiff-Plastic Separation Device (Diaphragm): Monopropellant storage unit used on the Fobos-Grunt mission. •
Bipropellant Tank with Stiff-Plastic Separation Devices (Diaphragms): Bipropellant storage unit used on communications satellites. • Solenoid Valves •
RT.200: •
18RT.200: •
16RT.200: •
12RT.200: •
6RT.200: • Flow stabilizers •
CP1: per second of hypergolic propellant flow. •
CP2: per second of hypergolic propellant flow. •
CP3: /// per second of hypergolic propellant flow. •
CP4: per second of air/nitrogen/oxygen/hydrogen flow.
Former Propulsion Products Engines that are no longer produced. •
RDMT-0.4X: N2O4/UDMH rocket engine. •
RDMT-0.8: Nitrogen and helium cold gas thruster. •
RDMT-12: N2O4/UDMH rocket engine. •
RDMT-50: N2O4/UDMH rocket engine. •
RDMT-100: N2O4/UDMH rocket engine. •
RDMT-135 (a.k.a.
11D428A): N2O4/UDMH rocket engine. Used on the
Soyuz 7K-S,
KTDU-426 and initial
KTDU-80. •
RDMT-200: N2O4/UDMH thruster used on the
Almaz space stations. •
RDMT-400A: Experimental version of the RDMT-200 with
Niobium combustion chamber. •
RDMT-400X: Experimental version of the RDMT-200 with
Carbon combustion chamber. ==See also==