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RPZ

RPZ
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Structure
Persons

Anatoly V.Chumakov

General Director

Presents

Аccelerometers

А-15

Is used to measure the linear acceleration along one of the body axis.

Gyro Stabilized Magnttic Compass

”STRIZH”

Autonomous determination and output of: gyromagnetic heading, DG heading.
The unit axcels previous versions with regard ...

Gyroscope

GPA-L2-2

The support of gyromotor rotor is of spool-shaped with hard-coated working surfaces and is made of artificial stone with ball en...

GL-1

GL-1 is a single-axis laser rate gyro with mechanical vibration support.
Prisms of full internal reflection are applied a...

GPA-200

GPA-200 is designed for gyro platform as a position transmitter of a/c relatively two axes. The specification of GPA-200 are pro...

MG-4

Free two-degree-of-freedom gyroscope dynamically tuned has been designed to measure angular velocity in strapdown Inertial Navig...

GL-2

GL-2 is a single-axis angular velocity laser meter with mechanical vibration support. Prisms of full internal reflection are app...

Torquer Motors

DM-18, DM-20

The torque motors are intended to be used as final-control elements in various automatics, telemetring & measuring systems as we...

Motors-Generators

MGD-0.1D / MDG-0.25D

The unit represents a two-phase wound motor and a generator of AC. It is used as servomotor in automatic system with speed feed-...

Radiomagnetic Indicators

RMI-3

RMI provides navigation information:
- magnetic heading,
- relative bearing for two radio stations,
- dista...

INP-RD

Stand-by HSI displays aircraft position, heading & pitch with respect to the radio beacon & four cardinal points. The indicator...

Two-Degree-Of Freedom Astatic Floated Gyros

I-21

I-21 Inertial Navigation System - a fully selfcontained automatic aircraft control system. The high-precision reckoning ability...

Inertial Navigation System

INS-8

Intended to determine and outout flight and navigation data of aircraft. INS-80 is made as a single unit comprising a gyro-stabi...

Strap-Down Integrated Intrtial Navigation Systems

I-42-1I

I-42-1I System is designed to measure & calculate flight & navigation parameters of a/c and means of ground transport.
Th...

Attitdde Heading Referense System

705-6

Performs functions of pickoff providing with following information:
- gyroscopic heading,
- pitch & roll angles,...

Course Indicators

PNP-72


Flight Director Indicators

PKP-77


MK Compass Systems

MK COMPASS SYSTEM

Compass System is designed to produce and output the gyromagnetic, magnetic & true present courses by operating with external pi...

Slip Ring

GK 11

Is used for commutation of electrical circuits between rotating parts with no limitation of rotation angle.
It prodvides...

Activities

The Ramensky Instrument Engineering Plant (RPZ) has been working in avionics engineering since 1939. Nowadays, we are the manufacturers of inertial navigation systems, integrated flight control and navigation systems and instruments, flight director systems, AHRS, compass systems, multifunctional LCD displays, dynamically tuned and floated gyros, accelerometers, temperature and pressure transmitters, low power motors, cutting and measuring tools. For many years we have been supporting production links with the most of aviation design bureau: Sukhoi, Mikoyan, Ilushin, Tupolev, Antonov, Yakovlev, Kamov, Mil.

<< Home
   About company
   Persons
Anatoly V.Chumakov
   Main activity
Аccelerometers
А-15
Gyro Stabilized Magnttic Compass
”STRIZH”
Gyroscope
GPA-L2-2
GL-1
GPA-200
MG-4
GL-2
Torquer Motors
DM-18, DM-20
Motors-Generators
MGD-0.1D / MDG-0.25D
Radiomagnetic Indicators
RMI-3
INP-RD
Two-Degree-Of Freedom Astatic Floated Gyros
I-21
Inertial Navigation System
INS-8
Strap-Down Integrated Intrtial Navigation Systems
I-42-1I
Attitdde Heading Referense System
705-6
Course Indicators
PNP-72
Flight Director Indicators
PKP-77
MK Compass Systems
MK COMPASS SYSTEM
Slip Ring
GK 11
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