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RPZ

International Aviation & Space Salon
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RPZ
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Structure
Persons

Anatoly V.Chumakov

General Director
RPZ
Presents

Gyroscope

GPA-L2-2

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

GL-1

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

GPA-200

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

MG-4

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

GL-2

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

Course Indicators

PNP-72

Inertial Navigation System

INS-8

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

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 operatin...

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 syste...

Torquer Motors

DM-18, DM-20

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

Gyro Stabilized Magnttic Compass

”STRIZH”

Autonomous determination and output of: gyromagnetic heading, DG heading.
The unit axcels previous ver...

Radiomagnetic Indicators

RMI-3

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

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 tr...

Two-Degree-Of Freedom Astatic Floated Gyros

I-21

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

Attitdde Heading Referense System

705-6

Performs functions of pickoff providing with following information:
- gyroscopic heading,
- pitc...

Stand-By Horisontal Situation Indicators

INP-RD

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

Аccelerometers

А-15

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

Slip Ring

GK 11

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

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   Persons
Anatoly V.Chumakov
   Base activity

Gyroscope

GPA-L2-2
GL-1
GPA-200
MG-4
GL-2

Course Indicators

PNP-72

Inertial Navigation System

INS-8

Flight Director Indicators

PKP-77

MK Compass Systems

MK COMPASS SYSTEM

Motors-Generators

MGD-0.1D / MDG-0.25D

Torquer Motors

DM-18, DM-20

Gyro Stabilized Magnttic Compass

”STRIZH”

Radiomagnetic Indicators

RMI-3

Strap-Down Integrated Intrtial Navigation Systems

I-42-1I

Two-Degree-Of Freedom Astatic Floated Gyros

I-21

Attitdde Heading Referense System

705-6

Stand-By Horisontal Situation Indicators

INP-RD

Аccelerometers

А-15

Slip Ring

GK 11
   Structure
   Exhibitor of
MAKS
Engines
IMDS

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