Ka-Band Test Loop Translator for Satellite Communications

SKU: TRR-29.75-19.95

Test Loop Translator by GeoSync Microwave (76 more products)

Note : Your request will be directed to GeoSync Microwave.

TRR-29.75-19.95 Image

The TRR-29.75-19.95 from GeoSync Microwave is a Test Loop Translator with an input frequency range of 29.5-30 GHz and an output frequency range of 19.7-20.2 GHz. It has an LO frequency of 9.8 GHz and an impedance of 50 Ohms. This test loop translator has an attenuation adjustment range of 30 dB and an amplitude response of ±0.25 dB. It has an input/output return loss of 18 dB and a conversion loss of 15-25 dB. The test loop translator has a noise figure of 15-25 dB and a phase noise of up to -120 dBc/Hz. It supports an RS-485 or RS-422 serial interface and a 10/100 Base-T ethernet interface. The test loop translator requires an input supply voltage of 90-250 VAC and has a power consumption of 40 W. It has a mass of 4.5-6.4 Kg and measures 19 x 1.75 x 20 inches. The test loop translator is designed for satellite communication applications where frequency translation is needed with a minimum amplitude and group delay distortion.

Product Specifications

Product Details

  • Part Number
    TRR-29.75-19.95
  • Manufacturer
    GeoSync Microwave
  • Description
    Ka-Band Test Loop Translator for Satellite Communications

General Parameters

  • Segment
    Ground
  • Type
    Single Band
  • Translation Band
    Ka to K
  • Downlink Frequency Band
    K Band
  • Downlink Frequency
    19.7 to 20.2 GHz
  • Downlink Frequency 1
    19.7 to 20.2 GHz
  • Uplink Frequency Band
    Ka Band
  • Uplink Frequency
    29.5 to 30.0 GHz
  • Uplink Frequency 1
    29.5 to 30.0 GHz
  • LO Frequency
    9.8 GHz
  • Frequency Stability
    ±2 x 10-8, 0 to 50°C
  • Attenuator Step Size
    0.2 dB
  • Interface
    RS422, RS485, Ethernet
  • Conversion Loss
    25 dB
  • Conversion Loss Stability
    ±0.25 dB/day at 23°C
  • Gain
    20 ±3 dB
  • Gain Slope
    0.03 dB/MHz maximum
  • Gain Stability
    ±0.25 dB/day
  • Attenuation Adjustment Range
    30 dB
  • Noise Figure
    25 dB
  • Group Delay
    1 ns peak-to-peak
  • Input/Output Isolation
    60 dB
  • Phase Noise@1 kHz
    -85 to -77 dBc/Hz
  • Phase Noise@1 MHz/5 MHz
    -127 to -117 dBc/Hz
  • Phase Noise@10 kHz
    -87 dBc/Hz
  • Phase Noise@100 kHz
    -100 to -87 dBc/Hz
  • P1dB
    18 dBm
  • IM3
    -50 dBc
  • Signal Related Spurious
    65 dBc
  • Return Loss
    18 dB
  • Input Return Loss
    18 dB
  • Output Return Loss
    18 dB
  • Impedance
    50 Ohms
  • Input Impedance
    50 Ohms
  • Output Impedance
    50 Ohms
  • AC Voltage
    90 to 250 V
  • Power Consumption
    40 Watts
  • Operating Temp
    0 to 50 Degree C
  • Altitude
    Up to 10, 000 feet, Up to 40, 000 feet
  • Humidity
    Up to 95% at 45°C
  • Connector
    SMA - Female, BNC - Female
  • Dimensions
    19 x 1.75 (panel height) x 20 Inches
  • Package
    Rack Mount
  • Weight
    4.5 Kg, 6.5 Kg

Technical Documents

Space Missions - A list of all Space Missions

esa

Name Date
Altius 01 May, 2025
Hera 01 Oct, 2024
Arctic Weather Satellite 01 Jun, 2024
EarthCARE 29 May, 2024
Arctic Weather Satellite (AWS) 01 Mar, 2024
MTG Series 13 Dec, 2022
Eutelsat Quantum 30 Jul, 2021
Sentinel 6 21 Nov, 2020
OPS-SAT 18 Dec, 2019
Cheops 18 Dec, 2019

isro

Name Date
INSAT-3DS 17 Feb, 2024
XPoSat 01 Jan, 2024
Aditya-L1 02 Sep, 2023
DS-SAR 30 Jul, 2023
Chandrayaan-3 14 Jul, 2023
NVS-01 29 May, 2023
TeLEOS-2 22 Apr, 2023
OneWeb India-2 26 Mar, 2023
EOS-07 10 Feb, 2023
EOS-06 26 Nov, 2022

jaxa

Name Date
VEP-4 17 Feb, 2024
TIRSAT 17 Feb, 2024
CE-SAT 1E 17 Feb, 2024
XRISM 07 Sep, 2023
SLIM 07 Sep, 2023
ALOS-3 07 Mar, 2023
ISTD-3 07 Oct, 2022
JDRS 1 29 Nov, 2020
HTV9 21 May, 2020
IGS-Optical 7 09 Feb, 2020

nasa

Name Date
NEO Surveyor 01 Jun, 2028
Libera 01 Dec, 2027
Artemis III 30 Sep, 2026
Artemis II 30 Sep, 2025
Europa Clipper 10 Oct, 2024
SpaceX CRS-29 09 Nov, 2023
Psyche 13 Oct, 2023
DSOC 13 Oct, 2023
Psyche Asteroid 05 Oct, 2023
Expedition 70 27 Sep, 2023