Mounted Camera facing northeast for scene image collection (a1-level)
Mounted Camera facing northeast for scene image collection
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Mounted Camera facing northeast for scene image collection
Mounted Camera facing northeast for scene image collection
Mounted Camera facing southeast for scene image collection
Mounted Camera facing southeast for scene image collection, processed into a movie
This paper addresses the potential impact of liquid metal (LM) plasma facing components (PFCs) for the heating and current drive actuators (H&CD) on the Fusion Nuclear Science Facility (FNSF) fusion reactor. Fulfilling the high neutron fluence mission of the FSNF requires steady-state operation for extremely long pulses (months to years) between maintenance opportunities. The use of liquid metal as a surface material is one strategy for extending the lifetime of the PFCs for long pulse operation in a high heat flux, high neutron flux environment like that of the FNSF. Liquid metal PFCs provide possible pathways forward on many difficult aspects of a fusion reactor, however the LM PFCs also bring new challenges and unknowns with respect to the H&CD actuators needed to provide steady-state operation. The development of LM compatible materials for RF antennas will be critical, as well as strategies for minimizing contamination of antenna surfaces and the core plasma. Successful deployment of LM PFCs on the FNSF will require operational experience with RF in a liquid metal environment both on test stands and in an integrated toroidal environment.
Boronization is a Plasma Facing Component (PFC) conditioning technique widely used in tokamak machines. The National Spherical Torus Experiment-Upgrade (NSTX-U) applied this conditioning, using a plasma glow with a deuterated Trimethyl-boron (d-TMB) and He mixture. The use of boronization during the campaign improved the plasma performance, allowing longer plasma discharges and H-mode access. The chemical state of an ATJ graphite sample, used as a proxy for the NSTX-U PFCs, was monitored in-situ using the Materials Analysis Particle Probe (MAPP) diagnostic and X-ray Photoelectron Spectroscopy (XPS). The XPS data showed a progressive rise (from + fluence increased. Filterscopes were used to measure the light emitted by oxygen impurities in the plasma near the surface of the PFC. An increase in the registered magnitude of the OII line, normalized to the Dγ intensity, was observed as the concentration of O on the ATJ surface increased. The plasma performance was found to be strongly correlated to oxygen impurity concentrations at the plasma edge and on the PFC surface, as measured by the discharge length and access to the H-mode regime. In this work, we present a quantitative analysis of the evolution of the chemistry of the ATJ surface, and the oxygen presence in the plasma-material interface, and report relevant plasma parameters observed during the same period of time.
Formation energy for interstitials in a face- centered cubic crystal
Free flight aerodynamic heating data obtained from flat-faced cylinder at mach 10.9
Pressure and heat-transfer measurements of flat face of blunted 10 deg half-cone body or semidisk at mach 6.15
Effects of transverse barycenter displacement, conical afterbody, curved front face on mercury capsule supersonic aerodynamic characteristics
Effect of canted forward faces on static longitudinal stability characteristics of escape and exit configurations of Mercury capsule at Mach 2.01
Effect of face sheet flexural stiffness on buckling of elastic curved plates and cylindrical shells of sandwich construction in axial compression
Transonic tests of base pressures associated with shallow three-dimensional rearward-facing steps
Four-element dynamic face seal for positive separation of cryogenic coolant and hot gas in turbopump, using neutral gaseous nitrogen purge
Effect of face sheet stiffness on buckling of cylindrical shells of sandwich construction
Heat transfer and pressure distributions on flat face rounded-corner body of revolution with and without flap control at hypersonic speeds and angles of attack from 0 deg to 45 deg
Hypersonic aerodynamic stability and drag of ablating and nonablating models of blunt-faced reentry shape
Dynamic instability in undamped bellows face seals operating in cryogenic environment with torsional oscillation and diametrical rocking as primary motion