Effect of body porosity on hypervelocity impact.
Body porosity effect on hypervelocity impact, computing pressure, velocity, density and specific internal energy profiles
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Body porosity effect on hypervelocity impact, computing pressure, velocity, density and specific internal energy profiles
We report here on the predicted impact of species such as ice-water, CO2, CH4, and NH3, on oxidized titanium, as well as HC species on diamond surfaces. These simulations provide the dynamics of product distributions during and after a hypervelocity impact event, ionization fractions, and dissociation probabilities for the various species of interest as a function of impact velocity (energy). We are using these results to determine the relevance of the fragmentation process to Cassini INMS results, and to quantify its effects on the observed spectra.
The use of carbon-fiber-reinforced polymer (CFRP) in modern satellites has led to a significant amount of space debris, including fragments of CFRP and high-density metals such as steel and copper, produced during catastrophic breakup events. To address this issue, NASA's White Sands Test Facility (WSTF) has been developing the capability to launch "flake-like" and long "needle-like" projectiles. WSTF tested projectiles with different length-to-diameter ratios (L/D), impacting aluminum Whipple shields with thermal blankets on the outer surface, at velocities exceeding 6 km/s. The results of the study suggest that launching and imaging shaped projectiles at high velocities is feasible. Ongoing research is now focused on improving the techniques for launching and imaging shaped projectiles under hypervelocity conditions.
Heat transfer problems with a ballistic vehicle entering into the atmospheres of near planets at hypervelocity entry conditions
Shock tube instrumentation to study convective and radiative heat transfer of hot gases simulating hypervelocity reentry
Velocity selector system for particle detector of electrostatic hypervelocity accelerator
Matched asymptotic expansion method applied to hypervelocity flight trajectories, obtaining solutions to flight dynamic equations
Hypervelocity heat protection, surface heat shielding, and internal temperature rise of Teflon, phenolic nylon, epoxy resin in glass honeycomb, and silicone elastomer
One dimensional analysis of hypervelocity impact of pellet onto thin bumper using finite difference techniques
Hypervelocity launcher designed for analyzing physical, chemical and aerodynamic problems associated with planetary entry and meteoroid impact
Hypervelocity impacts on silicates and polyethylene, noting highly irregular fragment shapes produced and relevance to lunar surface properties for similar meteor process
Hypervelocity impact effect on structural honeycomb spacecraft wall configurations, stressing design and wall thickness parameters
Sensors used in cosmic dust experiments studied for response to microparticle hypervelocity impacts, noting relationship to velocity
Reynolds number, viscosity and atom concentration in hypervelocity nozzles measured using stagnation point heat transfer
Theoretical prediction of crater size in Al alloy for hypervelocity impact by reduced density particles
Projectile shape effects on hypervelocity impact craters in aluminum
Response of infinite elastic plates to axisymmetric initial velocity distributions with application to hypervelocity impact
Initial hydrodynamic phase of hypervelocity impact analyzed by computer program using eigenvector approach