Cermet-Bonding Mechanism in Cermets
openaire +2 more sources
PEGASUS: A multi-megawatt nuclear electric propulsion system [PDF]
A propulsion system (PEGASUS) consisting of an electric thruster driven by a multimegawatt nuclear power system is proposed for a manned Mars mission. Magnetoplasmadynamic and mercury-ion thrusters are considered, based on a mission profile containing a ...
Berkopec, Frank +5 more
core +1 more source
In situ high temperature X-ray diffraction and dilatometric analysis of CGO-Cu composites for solid oxide devices. [PDF]
Balaguer M +5 more
europepmc +1 more source
Corrosion Properties of Cold-Sprayed Cr3C2-25(Ni20Cr) Coatings After Heat Treatment. [PDF]
Scendo M, Żórawski W.
europepmc +1 more source
Evaluation of cermet materials suitable for lithium lubricated thrust bearings for high temperature operation [PDF]
Cerment materials (HfC - 10 wt% W; HfC - 10 wt% TaC - 10 wt%W; HfC - 2 wt% CbC - 8 wt% Mo;Hfn - 10 wt% W; Hfn - 10 wt% TaN - 10 wt% W; and ZrC - 17 wt% W) were evaluated for possible use as lithium-lubricated bearings in the control system of a nuclear ...
Hendrixson, W. H., Sinclair, J. H.
core +1 more source
Effects of Mo2C on Microstructures and Comprehensive Properties of Ti(C, N)-Based Cermets Prepared Using Spark Plasma Sintering. [PDF]
Qiao M, Zhao Z, Zhang G, Zheng H.
europepmc +1 more source
Syngas Production via Oxidative Reforming of Propane Using a CO2- and O2-Permeating Membrane. [PDF]
Fabián-Anguiano JA +6 more
europepmc +1 more source
Selective Laser Melting of TiC-Fe via Laser Pulse Shaping: Microstructure and Mechanical Properties. [PDF]
Maurya HS +5 more
europepmc +1 more source
Scalable and shapable nacre-like ceramic-metal composites based on deformable microspheres. [PDF]
Lu YJ +10 more
europepmc +1 more source
Direct current plasma spraying of mechanofused alumina-steel particles
Stainless steel particles (60 $\mu$m in mean diameter) cladded with an alumina shell (2 $\mu$m thick and manufactured by mechanofusion) were sprayed with an Ar-H2 (53-7 slm) d.c. plasma jet (I = 500 A, P = 28 kW, \rho_th = 56 %).
Ageorges, Hélène +4 more
core +1 more source

