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タイトルPrediction of the pattern performance for the Aeroassist Flight Experiment (AFE) spacecraft
本文(外部サイト)http://hdl.handle.net/2060/19920001847
著者(英)Torres, R.; Rudduck, R.; Yang, C.
著者所属(英)Ohio State Univ.
発行日1991-10-01
言語eng
内容記述In order to provide a set of benchmark flight data for a reusable Aeroassisted Orbit Transfer Vehicle (AOTV) application, NASA undertook the development of an Aeroassisted Flight Experiment (AFE) which will be launched from the Space Shuttle. A representative aeroassist trajectory will be flown and sensor measurements of aerodynamic performance, thermal protection response, and plasma ionization reentry effects will be obtained. Discussed here is the spacecraft antenna. Estimates of signal transmissions from the AFE to the Tracking and Data Relay Satellites (TDRS) during the reentry period are given. The computer modeling of the antennas is presented with and without the reentry plasma.
NASA分類SPACE COMMUNICATIONS, SPACECRAFT COMMUNICATIONS, COMMAND AND TRACKING
レポートNO92N11065
OSU-715559-7
NASA-CR-4409
NAS 1.26:4409
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/130266


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