Title :
A channelized 2nd IF/LO downconverter for the EOS Microwave Limb Sounder
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Abstract :
The Earth Observing System (EOS) Microwave Limb Sounder (MLS) is scheduled for launch in 2004 on the EOS Aura spacecraft. The design, assembly and test of the flight 2nd Intermediate Frequency/Local Oscillator (2nd IF/LO) subsystem for this instrument has been completed and is presented here. The 2nd IF/LO subsystem consists of 5 separate microwave assemblies, 1 for each of the 5 millimeter wave radiometer front ends, providing a total of 33 separate IF channels. Some key requirements of the subsystem are as follows: provide frequency multiplexing of overlapping or closely spaced 1st IF channels while maintaining low ripple in the passbands; generate 18 different 2nd LO frequencies, in the range of 4-20 GHz, with low phase noise and a placement resolution of 400 KHz; downconvert the 1st IF´s to a common 2nd IF frequency centered at 900 MHz; minimize cost and schedule by using common designs for the 5 different assemblies wherever possible.
Keywords :
artificial satellites; microwave frequency convertors; microwave generation; microwave oscillators; millimetre wave frequency convertors; millimetre wave oscillators; multiplexing; phase locked oscillators; radiometers; space vehicle electronics; 4 to 20 GHz; 400 kHz; 900 MHz; AD 2004; EOS Aura spacecraft; channelized IF/LO downconverter; earth observing system microwave limb sounder; flight 2nd intermediate frequency/local oscillator subsystem; frequency multiplexing; microwave assemblies; millimeter wave radiometer front ends; passband ripples; phase noise; Assembly; Earth Observing System; Frequency division multiplexing; Instruments; Local oscillators; Microwave radiometry; Multilevel systems; Passband; Space vehicles; Testing;
Conference_Titel :
Microwave Conference, 2003. 33rd European
Print_ISBN :
1-58053-834-7
DOI :
10.1109/EUMC.2003.1262857