Space Hardware Marketplace

Antenna Feeder Device AC-25KRL-Ku/S

• Reflector diameter2,4 m
• Receive Frequency Range2,025-2,1092; 10,712-10,770 GHz
• Transmission Frequency Ranges2,2-2,29; 14,52-14,575 GHz

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a 2.4 m…

Antenna feeder device

• Reflector diameter2,4 m
• Receive Frequency Range3,4-4,2 GHz
• Transmission Frequency Range5,7-6,6 GHz

The transceiver single-mirror antenna system includes an antenna with a 2.4 m reflector with an irradiating system, a…

Antenna-feeder System 9.3 m

• Reflector diameter9,3 m
• Receive Frequency Range3,4- 4,2 GHz
• Transmission Frequency Range5,7- 6,725 GHz

The transceiver two-mirror antenna system is constructed according to the Cassegrain system, it includes an antenna with a…

Antenna Post L- and S-bands

• Reflector diameter6,0 m
• Receive Frequency Range1,586-1,616; 1,233- 1,263; 1,187- 1,217; 2,197- 2,227 GHz
• Transmission Frequency Range2,197-2,227 GHz

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a 6.0 m…

Electrolysis Unit

Spacecraft water electrolysis oxygen supply unit (30 kg, 99.9% purity, 25–160 L/h, 10–70 A, zero-gravity capable, solid polymer…

Active Weightlessness System

Active suspension system for large-sized transformable spacecraft systems at ground modal testing. Simultaneously with the suspension, the dynamic…

Automatic Control System of Thermal-vacuum-testing

Spacecraft thermal-vacuum test chamber automation (600 m³, ±150 °C, 750+ test points, 2000+ parameters, 720+ hr continuous operation).

Control Complex of a Large-sized Products

Programmable control complex of large-sized product forms in real time. The principle of operation is based on measurement…

Angular accelerometer

The accelerometer provides measurement of the apparent acceleration of ballistic and space equipment.

String accelerometer

The accelerometer provides measurement of the apparent acceleration of ballistic and space equipment.

Bipropellant Thruster

Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands.

Universal Upper Stage “Fregat”

In accordance with the specification of the customer. On the basis of the basic upper stage "Fregat" a…

Dynamic Pressure Sensor Vt 206

Version: strain gauge sensor with cable jumper. Upon customer's request, it is made with a screwed fitting and…

Pressure Sensor DAV 067

Exception: the strain gage sensor can be supplied with a shock absorber at the request of the consumer.…

Pressure Sensor DAV 068

It is made according to "Regulation 98". Execution: the strain gage sensor at the request of the consumer…

Transition Compartment

Flight-proven transition/adapter compartments for Soyuz (Ø3715/4110 mm) and Zenit (Ø4100 mm) launch vehicles (345–465 kg) for spacecraft-LV interface.

Asynchronous controlled electric motor

The asynchronous controlled electric motor has a 2-phase supply voltage of 40 V, 1000 Hz; the speed of…

Thermoelectric Converter DT 27

Version: thermoelectric converter (TC) consists of a sensitive element placed in the housing, a cable jumper and a…