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August 19-24, 2003, FRI named after M.M.Gromov, Zhukovsky, Russia
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RAMENSKY INSTRUMENT ENGINEERING PLANT

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RAMENSKY INSTRUMENT ENGINEERING PLANT
- leader in output of intertial navigation system, flyingnavigation indicators and trajectory control sustems
 

"STRIZH" GYRO STABILIZED MAGNETIC COMPASS

Autonomous determination and output of: gyromagnetic heading, DG heading. 
The unit axcels previous versions with regard to number of functions, parameters and type of connection and can replace ones.

SPECIFICATIONS
The error (2 sigma) of determination and output of gyromagnetic heading at 0.17±0.3 Ersted of magnetic intensity in the range of 360 deg is:

- under normal conditions                      0.7deg max
- at-50 to +50 °C of operational 
temperatures                                        1.0 deg max
Readiness time                                     3min
Weight                                                  3,5 kg

DESIGN FEATURES 
The unit consists of ИД-7 Flux-data detector and БГМК-7 Gyromagnetic Heading Unit.

OPERATING CONDITIONS 
Flight speed                                                           up to 1,000 km/h
Flight altitude                                                         up to 15,000m
Angular velocity along any axis.                             up to 200 deg/s
Linear acceleration                                                 up to 4 g
Angles of heading                                                  0-360 deg
Angles of roll                                                          0-180 deg
Angles of pitch                                                       0-90 deg
Latitude                                                                 0-75 deg

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About company

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 - News, press-releases

 - Brief information

Production and services

 - SLIP RING GK 11

 - АССELEROMETER A-15

 - 705-6 ATTITDDE HEADING REFERENCE SYSTEM

 - STAND-BY HORIZONTAL SITUATION INDICATOR INP-RD

 - TWO- DEGREE- OF FREEDOM ASTATIC FLOATED GYRO

 - I-42-1I STRAP-DOWN INTEGRATED INERTIAL NAVIGATION SYSTEM

 - RMI-3 RADIOMAGNETIC INDICATOR

 - "STRIZH" GYRO STABILIZED MAGNETIC COMPASS

 - TORQUER MOTORS DM-18, DM-20

 - MGD-0.1D / MDG-0.25D MOTORS- GENERATORS

 - MK COMPASS SYSTEM

 - PKP-77 FLIGHT DIRECTOR INDICATORS PNP-72 COURSE INDICATOR

 - INS-80 INERTIAL NAVIGATION SYSTEM

 - GYROS

 1997 - 2001 ®