A Rayleigh quotient method for criticality eigenvalue problems in neutron transport
Not Available
Ortega, M. I.↗
Engineering topics
Brown, P. N.
Publications and source records attributed to Brown, P. N..
Composite engines for application to a single-stage-to-orbit vehicle
Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. The engine designs were variations of the supercharged ejector ramjet engine. The resulting performance, weight, and drawings of each engine form a data base for establishing a potential of this class of composite engine to various missions, including the single-stage-to-orbit application. The impact of advanced technology in the design of the critical fan turbine was established.
Bendot, J. G.↗