02093oam 2200577 450 991071410100332120201030152919.0(CKB)5470000002506658(OCoLC)761456718(OCoLC)995470000002506658(EXLCZ)99547000000250665820111115j196903 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierCold performance evaluation of 4.97-inch radial-inflow turbine designed for single-shaft Brayton cycle space-power system /William J. Nusbaum and Milton G. KofskeyWashington, D.C. :National Aeronautics and Space Administration,March 1969.1 online resource (ii, 22 pages) illustrationsNASA technical note. ;TN D-5090"March 1969."Includes bibliographical references (page 22).TurbinesAerodynamicsBrayton cycleSpace vehiclesAuxiliary power supplyBrayton cycleBrayton cyclefastSpace vehiclesAuxiliary power supplyBrayton cyclefastTurbinesAerodynamicsfastTurbinesAerodynamics.Brayton cycle.Space vehiclesAuxiliary power supplyBrayton cycle.Brayton cycle.Space vehiclesAuxiliary power supplyBrayton cycle.TurbinesAerodynamics.Nusbaum William J.1413835Kofskey Milton G.United States.National Aeronautics and Space Administration,Lewis Research Center.OCLCEOCLCEOCLCQOCLCOOCLCFOCLCQCOPGPOBOOK9910714101003321Cold performance evaluation of 4.97-inch radial-inflow turbine designed for single-shaft Brayton cycle space-power system3511253UNINA