Integrated S/X band transceiver for satellites
Integrated S/X band transceiver for satellites
Integrated S/X band transceiver for satellites
We provide an integrated S/X band transceiver for satellites (software-defined transceiver). Below are the main specifications of the unit. Dimensions: 15.3 x 15.3 x 19.1 cm Weight: 3 kg Radiation resistance: TID: 30 kRad (100 kRad option available) Operating temperature range: -30 to +65°C
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basic information
The main specifications of the integrated S/X band transceiver for space use are as follows: Features of the transmission section (X band): 1. Frequency range: 8.025–8.5 GHz 2. Output power: 2.5 W (5 W option available) 3. Power consumption: 52 W (maximum, when transceiver is "ON") 4. Data interface: RS-422 5. Frequency stability: ±10 ppm (standard) (±0.3 ppm also available) 6. Voltage: +28 Vdc (23 Vdc–34 Vdc) Features of the reception section (S band): 1. Frequency range: 2025–2120 MHz 2. Signal level range: ≦-100 dBm to ≧-47 dBm @ 256 kbps 3. Maximum input signal: +10 dBm 4. Uplink data rate: 256 kbps 5. Voltage: +28±6 Vdc 6. Power consumption: 7.5 W (receiving only "ON") 7. Command channel modulation method: BPSK 8. Output interface: Differential RS-422 (other options available) Please contact us for further details.
Price information
Please contact us regarding the price.
Delivery Time
※Please contact us regarding the delivery date.
Applications/Examples of results
We have started offering it for use with artificial satellites.
Company information
The Advanced Technology Research Institute is an engineering company that supports space development and utilization, including rockets and artificial satellites, in Japan and around the world. We conduct a wide range of activities from the design and development of space systems, subsystems, and components for satellites and rockets, both small and large, to the sale of overseas space equipment. Additionally, we sell solar cells for space and ground use, and we design and develop solar cell panels for space as well as sell solar power generation modules and systems for ground use. For small satellites, including CubeSats, we provide system development from 1U to 12U, offer bus components, design and develop bus equipment, assemble satellites, and conduct integration and testing of satellites, including payloads. We also design, develop, and sell small electric propulsion systems for CubeSats and small satellites.
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