Among the available products are the following:
- low- and high-frequency data collection and accumulation
solid storage systems;
- vibration parameters measuring devices ;
- instant temperature sensors;
- miniaturized flat piezoresistance beat and pressure
distribution sensors;
- hot-wire airflow velocity vector transducers and
instrumentation for aerodynamic friction stress measurement.
- aircraft performance improvement - mobile ramp, aeronavigation complex
based on satellite technology, screw vibration reduction, aircraft
operation on gas fuel, high reliability airborne communication, mid-air
refuling automation;
- Flight safety - ejection seat path control, icing shape calculation
techniques, methods of reducing damage to an engine caused by foreign
objects, aircraft protection from anti-air missiles, unified computerized
training class, recovery technique for crash-damaged records of
emergency recorders;
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In accordance to its status of a parent enterprise in charge
of prototype flight testing, the Institute offers the following testing-support
services to construction offices:
- the testing airfield with a proper service package;
- the airborne command and measurement post based on
the II-76MD aircraft
- for information support when testing manned, unmanned,
and space objects - on long unequipped ranges;
- advanced development of various issues of flight dynamics,
engine units, - control systems, and instrumentation components using
flying laboratories and flying models;
- self-supported conduction of the most complex tests,
such as critical flight modes, structural strength, flutter, assessment
of flight control and navigation equipment and weapon system components,electromagnetic
safety, etc.;
- participation of the Institute's experts in aerospace
machinery prototype testing, including certification;
- use of the GLL-31 and GLL-VK Flight Experimental Complexes in carrying
out research into crucial problems of hypersonic flight, among which
the following are the most important:
- construction of an effective engine unit;
- determination of an aircraft's aerodynamic configuration;
- creation of heat-protective material and development
of a structure of aircraft and engine heat-protection;
- research into flight dynamics and construction
of a control system. Traditionally, the Institute gives recommendations
and exercises assessment of aircraft operational and performance
characteristics.<<Back
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