A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.
申请公布号
WO2011143642(A3)
申请公布日期
2012.01.12
申请号
WO2011US36561
申请日期
2011.05.14
申请人
PARAGON SPACE DEVELOPMENT CORPORATION;MORIN, THOMAS, WILLIAM;MACCALLUM, TABER, K.;HAHN, NORMAN, JACOB;MACCAGNANO, JOHN, ZANIEL