LEADER 01037nam a2200253 a 4500 001 991003796499707536 008 020 $a9788833932088 035 $ab14389010-39ule_inst 040 $aDip.to di Storia, Società e Studi sull'Uomo$bita 082 0 $a330.1220905 100 1 $aQuintarelli, Stefano$0374499 245 10$aCapitalismo immateriale :$ble tecnologie digitali e il nuovo conflitto sociale /$cStefano Quintarelli 260 $aTorino :$bBollati Boringhieri,$c2019 300 $a198 p. ;$c22 cm 490 0 $aSaggi. Scienze sociali 650 $aCapitalismo$xInternet$xEffetti dannosi 650 4$aCapitalismo$xRuolo [dell'] Innovazione tecnologica$xEffetti sociali 907 $a.b14389010$b31-07-20$c16-04-20 912 $a991003796499707536 945 $aLE023 330.122 QUI 1 1$g1$i2023000184523$lle023$op$pE16.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i15930920$z15-07-20 996 $aCapitalismo immateriale$91754454 997 $aUNISALENTO 998 $ale023$b16-04-20$cm$da $e-$fita$git $h0$i0 LEADER 04825nam 22006853u 450 001 9910781404503321 005 20230422050636.0 010 $a1-60086-497-X 010 $a1-60086-278-0 035 $a(CKB)2550000000072655 035 $a(EBL)3111529 035 $a(SSID)ssj0000786813 035 $a(PQKBManifestationID)11407264 035 $a(PQKBTitleCode)TC0000786813 035 $a(PQKBWorkID)10803431 035 $a(PQKB)10008459 035 $a(MiAaPQ)EBC3111529 035 $a(EXLCZ)992550000000072655 100 $a20151005d2000|||| u|| | 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aThermophysics$b[electronic resource] $eApplications to Thermal Design of Spacecraft 210 $aReston $cAmerican Institute of Aeronautics and Astronautics$d2000 215 $a1 online resource (599 p.) 225 0 $aProgress in astronautics and aeronautics Thermophysics 300 $aDescription based upon print version of record. 311 $a1-56347-872-2 327 $a""Cover ""; ""Title ""; ""Copyright ""; ""Preface ""; ""The Thermophysics Committee of the American Institute of Aeronautics and Astronautics""; ""Editorial Committee for Volume 23""; ""Table of Contents ""; ""I. Experimental Thermophysical Properties""; ""Conduction""; ""Thermal Isolation with Low-Conductance Interstitial Materials under Compressive Loads ""; ""Thermal Contact Resistance Measurements at Ambient Pressures of One Atmosphere to 3 X 10 ~12 mm Hg and Comparison with Theoretical Predictions "" 327 $a""Column Method of Measuring Thermal Conductivity of Gases: Results on Carbon Monoxide and Oxygen """"Radiation""; ""Portable Reflectometer ""; ""Investigation of a Model for Bidirectional Reflectance of Rough Surfaces ""; ""Solar Absorptance and Hemispherical Emittance of Various Metals at Space Conditions ""; ""Combined Radiation, Convection, and/or Conduction""; ""A Study of Heat-Transfer Processes in Multilayer Insulations ""; ""Opacified Fibrous Insulations ""; ""Techniques for Improving the Thermal Performance of Low-Density Fibrous Insulation ""; ""Phase Change"" 327 $a""Microscopic Observation of Interfacial Phenomena """"Space Environmental Effects upon Radiation Properties""; ""Radiation-Induced Absorption Bands in Spacecraft Thermal Control Coating Pigments ""; ""Electron Energy Dependance for In-Vacuum Degradation and Recovery in Thermal Control Surfaces ""; ""Results from the ATS-3 Reflectometer Experiment ""; ""II. Analytical Predictions Of Thermophysical Properties""; ""Radiation from a Bounded Medium""; ""Distribution of Solar Energy Reflected from Earth by a Scattering Atmosphere "" 327 $a""Radiative Equilibrium of a Gray Medium Bounded by Nonisothermal Walls """"Directional Emittance from Emitting, Absorbing, and Scattering Media ""; ""Surface Radiation Properties""; ""Apparent Radiation Properties of a Rough Surface ""; ""Effect of Thin Surface Films on the Radiative Properties of Metal Surfaces ""; ""III. Thermal Design Of Spacecraft Systems""; ""Thermal Design Techniques""; ""Distributed Parameter Space Radiator Dynamic Analysis ""; ""An ATS-E Solar Cell Space Radiator Utilizing Heat Pipes ""; ""Two-Component Heat Pipes "" 327 $a""Scale Modeling of a Multilayer Insulated Spacecraft for Use in a Preliminary Design Study """"Parametric Thermal Control Requirements for Future Manned Spacecraft ""; ""Planetary Landers""; ""Thermal Considerations of a Landed Vehicle on the Surface of Mars ""; ""Mars Lander Thermal Control System Parametric Studies ""; ""Thermal Design, Analysis, and Testing of a Full-Size Planetary Lander Model ""; ""Index of Contributors "" 606 $aMaterials -- Thermal properties -- Congresses 606 $aSpace vehicles -- Thermodynamics -- Congresses 606 $aSpace vehicles$xThermodynamics$xCongresses 606 $aMaterials$xCongresses$xThermal properties 606 $aMechanical Engineering$2HILCC 606 $aEngineering & Applied Sciences$2HILCC 606 $aAeronautics Engineering & Astronautics$2HILCC 615 4$aMaterials -- Thermal properties -- Congresses. 615 4$aSpace vehicles -- Thermodynamics -- Congresses. 615 0$aSpace vehicles$xThermodynamics$xCongresses 615 0$aMaterials$xCongresses$xThermal properties 615 7$aMechanical Engineering 615 7$aEngineering & Applied Sciences 615 7$aAeronautics Engineering & Astronautics 676 $a629.47/1 700 $aBevans$b Jerry T$01478330 702 $aBevans$b Jerry T 702 $aBevans$b Jerry T 801 0$bAU-PeEL 801 1$bAU-PeEL 801 2$bAU-PeEL 906 $aBOOK 912 $a9910781404503321 996 $aThermophysics$93748490 997 $aUNINA