用于EOS微波临边测深器的信道化第二中频/本征降频器

R. LaBelle
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引用次数: 1

摘要

地球观测系统(EOS)微波边缘探测仪(MLS)计划于2004年在EOS Aura航天器上发射。本仪器的flight2中频/本振(2nd IF/LO)子系统的设计、组装和测试已经完成,并在此介绍。第二个IF/LO子系统由5个独立的微波组件组成,每个组件对应5个毫米波辐射计前端,总共提供33个独立的IF通道。该子系统的一些关键要求如下:提供重叠或紧密间隔的第一中频信道的频率复用,同时在通带中保持低纹波;产生18个不同的第二本极频率,范围在4-20 GHz,相位噪声低,放置分辨率为400 KHz;将第一中频下变频到以900 MHz为中心的第二中频;尽可能使用5种不同组件的通用设计来降低成本和进度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Channelized 2nd IF/LO Downconverter for the EOS Microwave Limb Sounder
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 flight2nd 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.
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