ABSTRACT. Following con stru ction of a g lacial ice runwa y o n th e R oss Ice Shelf, Antarcti ca, and prior to fli g ht operations, th e runway was proof-rolled. Th e proof exercise was d es igned to simulate typica l heavy aircraft. Initia l tes ting produ ced num erous brittle surface failures in the runway ice. Thin sectio ns of ice co res taken from th e fail ed a reas showed large crystals (c ax is ve rti ca l) of cl ear , blu e ice with lon g, verti ca l bubbl es, indicative of ic e form ed direc tl y from meltwater. Uniaxialunconfined compression tes ts on core sample. were used to compare runway ice strength with published data for polyc rys talline la bora tory ice. Since the freq u e n t failure of surface ice had not bee n expec ted , it was criti cal to und e rsta nd the form a tion and mechani ca l properti es of th e weak ice to pre\'e nt its occ urrence in the future a nd to strengthen th e existing problem a reas. We discuss th e likely sce narios for devel o pment of weak ice o n the airstrip and the physical properti es of this typ e of ice. Also, the procedure used LO repa ir success full y th e runway surface is desc ribed , whi ch culminated in tes t fli ghts, followed by full fli ght opera tions.
INTRODUCTIONa n a lternating ta ll-a nd short-tooth pattern to assist In cleaning the surface of all debris. Th e includ ed a ng le of the cutting tee th w as 42° and sid e-relief a ngles were 41°. A laser-gu id ance sys tem assisted in producing a n acc ura te g rade even when th e g rader operator had great dif1icu lty seeing well enou g h to drive in a stra ig ht lin e. Snow and ice debris were r emoved from th e runway surface with a Rolb a rota ry sn ow -blo\\·er. (For a more co mpl e te