LEADER 03598nam 2200601 a 450 001 9910781433303321 005 20230213212249.0 010 $a1-60086-564-X 010 $a1-60086-345-0 035 $a(CKB)2550000000072635 035 $a(EBL)3111682 035 $a(OCoLC)922979130 035 $a(SSID)ssj0000565895 035 $a(PQKBManifestationID)12222286 035 $a(PQKBTitleCode)TC0000565895 035 $a(PQKBWorkID)10533914 035 $a(PQKB)11290736 035 $a(Au-PeEL)EBL3111682 035 $a(CaPaEBR)ebr10516787 035 $a(MiAaPQ)EBC3111682 035 $a(EXLCZ)992550000000072635 100 $a19840530d1984 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aSpacecraft contamination$b[electronic resource] $esources and prevention /$fedited by J.A. Roux, T.D. McCay 210 $aNew York, N.Y. $cAmerican Institute of Aeronautics and Astronautics, Inc.$dc1984 215 $a1 online resource (343 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 91 300 $a"Technical papers selected from the AIAA 21st Aerospace Sciences Meeting, January 1983, and the AIAA 18th Thermophysics Conference, June 1983, and subsequently revised for this volume." 311 $a0-915928-85-X 320 $aIncludes bibliographical references and index. 327 $aCover; Title; Copyright; Table of Contents; Chapter I. Contamination Overview; Improved Methods for Characterizing Material-Induced Contamination; Potential for Cross Contamination for Payloads in the STS Bay; Chapter II. Sources and Prevention of Contamination; Debris from Spallation of Foam Insulation of Cryogenic Fuel Tanks in Space Launch Systems; Particle Dispersion around a Spacecraft; Impact of the STS Ground/Launch Particle Contamination Environment on an Optical Sensor; Analysis of Contamination Degradation of Thermal Control Surfaces on Operational Satellites 327 $aAbatement of Gaseous and Particulate Contamination in a Space InstrumentChapter III. Properties and Effects of Contamination; Infrared Optical Properties of Thin CO,NO, CH4, HCI, N2O, O2, N2, and Ar Cryofilms; Infrared Optical Properties of Solid Mixtures of Molecular Species at 20 K; Measurements of Infrared Optical Properties of A12O3 Rocket Particles; Improvements in Rocket Engine Nozzle and High Altitude Plume Computations; as/eH Measurements of Thermal Control Coatings over Four Years at Geosynchronous Altitude 327 $aCalorimetric Measurements of Thermal Control Surfaces on Operational SatellitesExperimental Investigation of Bipropellant Exhaust Plume Flowfield, Heating, and Contamination and Comparison with the CONTAM Computer Model Predictions; Particle Sampling of Solid Rocket Motor Exhausts in High-Altitude Test Cells; Postfire Sampling of Solid Rocket Motors for Contamination Sources in High-Altitude Test Cells; Author Index 410 0$aProgress in astronautics and aeronautics ;$vv. 91. 606 $aSpace vehicles$xContamination$vCongresses 615 0$aSpace vehicles$xContamination 676 $a629.1 s 701 $aRoux$b J. A$01463126 701 $aMcCay$b T. D$01463127 712 02$aAmerican Institute of Aeronautics and Astronautics. 712 12$aAIAA Aerospace Sciences Meeting$d(21st :$f1983) 712 12$aAIAA Thermophysics Conference$d(18th :$f1983) 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910781433303321 996 $aSpacecraft contamination$93672338 997 $aUNINA