Ка-band transceiver.
Basic technical data:
Bandwidth, MHz: Ка-band;
Type of modulation: pulse-type;
Duration of received pulses, microseconds: 0,3-0,5;
Receiver sensitivity, maximum, dBm: -60;
Duration of transmit pulses, microseconds : 1 ± 0,01;
Pulse power, minimum, dBm: 33.
Ka-band single-chip micromodule.
Ka-band single-chip micromodule is intended to be used in
transmitting devices “point-to-point”, VSAT and SATCOM
systems.
Basic technical data:
Bandwidth, GHz: 34 - 36;
Output power, minimum, Watt : 3;
Operating regime: pulse ;
Power supply voltage, V: 5,5;
Current consumption, maximum, A: 6.
Control module of automatic system of suit thermal
control.
Control module of automatic system of suit thermal control is
intended for information reception and issuing of commands
and control of valves of thermal control system.
Basic technical data:
Power supply voltage, V: 23 - 34;
Current consumption, maximum
(without considering the valves), mA: 40;
Three channels of telemetry input, V: 0-6;
Operating temperature range, °C: from -55 to + 55.
Control module of airlocking system of the international space
station.
Control module of airlocking system of the international space
station is intended for automated control over operating regimes of
two spacesuits in the process of airlocking in accordance with the
preset algorithm.
Basic technical data:
Power supply voltage, V: 23 - 34;
Power consumption, maximum, Watt: 10;
Operating temperature range, °C: from -20 to + 55.
L-band power amplifier .
L-band transmit-receive module is
intended for amplification as part
of AESA.
Basic technical data:
Output pulse power, minimum, Watt: 450;
Gain, dB : 25 ± 1;
Efficiency, minimum, % : 40.
S-band transmit-receive module
S-band transmit-receive module is intended for
amplification of received and transmit radio pulses as part
of AESA.
Basic technical data:
Bandwidth, MHz: 2700-2900;
Noise figure, maximum, dB: 2;
Gain, dB: 25 ± 2;
Output pulse power, minimum, Watt: 16;
Efficiency, minimum, % : 25;
Power supply voltage, V: 32.
Low-noise amplifier (LNA).
LNA is intended for work as part of air-borne and satellite
transponders of communications, navigation and radar systems.
Basic technical data:
Bandwidth, MHz: from 225 to 4000;
Noise figure, maximum, dB: 3;
Gain, dB: 28 ± 2;
Operating supply voltage, V: 100;
Power consumption, maximum, Watt: 6.
Receiver block.
Receiver block is intended for work as part of air-borne and satellite
transponders of communications, navigation and radar systems.
Basic technical data:
Bandwidth, MHz: from 225 to 4000;
Noise figure, maximum, dB: 7;
Gain, dB: 33 - 37;
Operating supply voltage, V: 100,
Power consumption, maximum, Watt: 30.
L-band transmit-receive module for the
antenna system.
L-band transmit-receive module is intended for
amplification as part of AESA.
Basic technical data:
Noise figure, maximum, dB: 3;
Gain, dB: 38 ± 2;
Output pulse power, minimum, Watt: 400;
Efficiency, minimum, % : 25.
Technological L-band power amplifier for the
antenna system.
Technological power amplifier is intended for
providing of the desired level of the input signal of
L-band AESA.
Basic technical data :
Output peak power, minimum, Watt: 400;
Pulse front/rise, maximum, nsec: 200;
Pulse droop, maximum, dB: 0,5;
Power supply voltage, V: 48.
S-band module.
S-band module is intended for work as part of AESA
and solid-state radio transmitters.
Basic technical data:
Gain, dB: 25 ± 1;
Output peak power, minimum,
Watt: 30;
Bandwidth, MHz: 3000-3500;
Efficiency, minimum, %: 30;
Operation voltage, V: 30.
L-band transmitting module for AESA.
L-band module is intended for work as part of AESA and
solid-state radio transmitters.
Basic technical data:
Gain, dB: 25 ± 1;
Output peak power, minimum, Watt: 200;
Bandwidth, MHz: 1215-1400;
Efficiency, minimum, %: 40;
Operation voltage, V: 30.

Microdevises

  • 2.
    Ка-band transceiver. Basic technicaldata: Bandwidth, MHz: Ка-band; Type of modulation: pulse-type; Duration of received pulses, microseconds: 0,3-0,5; Receiver sensitivity, maximum, dBm: -60; Duration of transmit pulses, microseconds : 1 ± 0,01; Pulse power, minimum, dBm: 33. Ka-band single-chip micromodule. Ka-band single-chip micromodule is intended to be used in transmitting devices “point-to-point”, VSAT and SATCOM systems. Basic technical data: Bandwidth, GHz: 34 - 36; Output power, minimum, Watt : 3; Operating regime: pulse ; Power supply voltage, V: 5,5; Current consumption, maximum, A: 6.
  • 3.
    Control module ofautomatic system of suit thermal control. Control module of automatic system of suit thermal control is intended for information reception and issuing of commands and control of valves of thermal control system. Basic technical data: Power supply voltage, V: 23 - 34; Current consumption, maximum (without considering the valves), mA: 40; Three channels of telemetry input, V: 0-6; Operating temperature range, °C: from -55 to + 55. Control module of airlocking system of the international space station. Control module of airlocking system of the international space station is intended for automated control over operating regimes of two spacesuits in the process of airlocking in accordance with the preset algorithm. Basic technical data: Power supply voltage, V: 23 - 34; Power consumption, maximum, Watt: 10; Operating temperature range, °C: from -20 to + 55.
  • 4.
    L-band power amplifier. L-band transmit-receive module is intended for amplification as part of AESA. Basic technical data: Output pulse power, minimum, Watt: 450; Gain, dB : 25 ± 1; Efficiency, minimum, % : 40. S-band transmit-receive module S-band transmit-receive module is intended for amplification of received and transmit radio pulses as part of AESA. Basic technical data: Bandwidth, MHz: 2700-2900; Noise figure, maximum, dB: 2; Gain, dB: 25 ± 2; Output pulse power, minimum, Watt: 16; Efficiency, minimum, % : 25; Power supply voltage, V: 32.
  • 5.
    Low-noise amplifier (LNA). LNAis intended for work as part of air-borne and satellite transponders of communications, navigation and radar systems. Basic technical data: Bandwidth, MHz: from 225 to 4000; Noise figure, maximum, dB: 3; Gain, dB: 28 ± 2; Operating supply voltage, V: 100; Power consumption, maximum, Watt: 6. Receiver block. Receiver block is intended for work as part of air-borne and satellite transponders of communications, navigation and radar systems. Basic technical data: Bandwidth, MHz: from 225 to 4000; Noise figure, maximum, dB: 7; Gain, dB: 33 - 37; Operating supply voltage, V: 100, Power consumption, maximum, Watt: 30.
  • 6.
    L-band transmit-receive modulefor the antenna system. L-band transmit-receive module is intended for amplification as part of AESA. Basic technical data: Noise figure, maximum, dB: 3; Gain, dB: 38 ± 2; Output pulse power, minimum, Watt: 400; Efficiency, minimum, % : 25. Technological L-band power amplifier for the antenna system. Technological power amplifier is intended for providing of the desired level of the input signal of L-band AESA. Basic technical data : Output peak power, minimum, Watt: 400; Pulse front/rise, maximum, nsec: 200; Pulse droop, maximum, dB: 0,5; Power supply voltage, V: 48.
  • 7.
    S-band module. S-band moduleis intended for work as part of AESA and solid-state radio transmitters. Basic technical data: Gain, dB: 25 ± 1; Output peak power, minimum, Watt: 30; Bandwidth, MHz: 3000-3500; Efficiency, minimum, %: 30; Operation voltage, V: 30. L-band transmitting module for AESA. L-band module is intended for work as part of AESA and solid-state radio transmitters. Basic technical data: Gain, dB: 25 ± 1; Output peak power, minimum, Watt: 200; Bandwidth, MHz: 1215-1400; Efficiency, minimum, %: 40; Operation voltage, V: 30.