LEADER 03036nam 2200601 a 450 001 9910438114003321 005 20200520144314.0 010 $a3-642-32430-4 024 7 $a10.1007/978-3-642-32430-7 035 $a(CKB)2670000000279613 035 $a(EBL)1082546 035 $a(OCoLC)818827942 035 $a(SSID)ssj0000798967 035 $a(PQKBManifestationID)11462948 035 $a(PQKBTitleCode)TC0000798967 035 $a(PQKBWorkID)10757344 035 $a(PQKB)11450820 035 $a(DE-He213)978-3-642-32430-7 035 $a(MiAaPQ)EBC1082546 035 $a(PPN)168321785 035 $a(EXLCZ)992670000000279613 100 $a20121108d2013 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aNuclear rocket engine reactor /$fAnatoly Lanin 205 $a1st ed. 2013. 210 $aHeidelberg $cSpringer$d2013 215 $a1 online resource (114 p.) 225 0$aSpringer series in materials science,$x0933-033X ;$vv. 170 300 $aDescription based upon print version of record. 311 $a3-642-44263-3 311 $a3-642-32429-0 320 $aIncludes bibliographical references and index. 327 $aPreface -- History creation of a nuclear rocket engine reactor (NRER) -- Design of a NRER -- Methods of modeling tests -- Materials of the reactor core -- Radiation durability of NRE elements -- Corrosion of materials in a working environment -- Bearing ability of NRE elements -- Prospects of the NRER development for space. 330 $aThe development of a nuclear rocket engine reactor (NRER ) is presented in this book. The working capacity of an active zone NRER under mechanical and thermal load, intensive neutron fluxes, high energy generation (up to 30 MBT/l) in a working medium (hydrogen) at temperatures up to 3100 K is displayed. Design principles and bearing capacity of reactors area discussed on the basis of simulation experiments and test data of a prototype reactor. Property data of dense constructional, porous thermal insulating and fuel materials like carbide and uranium carbide compounds in the temperatures interval 300 - 3000 K are presented. Technological aspects of strength and thermal strength resistance of materials are considered. The design procedure of possible emergency processes in the NRER is developed and risks for their origination are evaluated. Prospects of the NRER development for pilotless space devices and piloted interplanetary ships are viewed. 410 0$aSpringer Series in Materials Science,$x0933-033X ;$v170 606 $aNuclear rocket engines 606 $aNuclear propulsion 615 0$aNuclear rocket engines. 615 0$aNuclear propulsion. 676 $a629.47 676 $a629.4753 700 $aLanin$b A$g(Anatoly)$01758776 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910438114003321 996 $aNuclear rocket engine reactor$94197029 997 $aUNINA