排序方式： 共有9条查询结果，搜索用时 296 毫秒
1
1.
Glazachev D. O. Popova O. P. Podobnaya E. D. Artemieva N. A. Shuvalov V. V. Svetsov V. V. 《Izvestiya Physics of the Solid Earth》2021,57(5):698-709
Izvestiya, Physics of the Solid Earth - Abstract—Destruction on the Earth’s surface caused by a shock wave is one of the most important and dangerous effects from asteroid and comet... 相似文献
2.
Assessment of Kinetic Energy of Meteoroids Detected by Satellite-Based Light Sensors 总被引：1，自引：0，他引：1
I.V. Nemtchinov V.V. Svetsov I.B. Kosarev A.P. Golub' O.P. Popova V.V. Shuvalov R.E. Spalding C. Jacobs E. Tagliaferri 《Icarus》1997,130(2):259-274
Radiation energies of bright flashes caused by disintegration of large meteoroids in the atmosphere have been measured using optical sensors on board geostationary satellites. Light curves versus time are available for some of the events. We have worked out several numerical techniques to derive the kinetic energy of the meteoroids that produced the flashes. Spectral opacities of vapor of various types of meteoroids were calculated for a wide range of possible temperatures and densities. Coefficients of conversion of kinetic energy to radiation energy were computed for chondritic and iron meteoroids 10 cm to 10 m in size using radiation–hydrodynamics numerical simulations. Luminous efficiency increases with body size and initial velocity. Some analytical approximations are presented for average conversion coefficients for irons and H-chondrites. A mean value of this coefficient for large meteoroids (1–10 m in size) is about 5–10%. The theory was tested by analyzing the light curves of several events in detail.Kinetic energies of impactors and energy–frequency distribution of 51 bolides, detected during 22 months of systematic observations in 1994–1996, are determined using theoretical values of luminous efficiencies and heat-transfer coefficients. The number of impacts in the energy range from 0.25 to 4 kt TNT is 25 per year and per total surface of the Earth.The energy–frequency distribution is in a rather good agreement with that derived from acoustic observations and the lunar crater record. Acoustic systems have registered one 1 Mt event in 12 years of observation. Optical systems have not detected such an event as yet due to a shorter time of observation. The probability of a 1 Mt impact was estimated by extrapolation of the observational data. 相似文献
3.
A mechanism through which water could be buried inside the Moon is found. If an icy comet strikes the planetary surface and a thin natural crack exists at the site of the impact, some amount of cometary material can penetrate deep into the ground. This happens due to peculiar features of hydrodynamic flow along the crack. Numerical simulations based on the free-Lagrangian method show that the amount of water buried under the crater is several percent of the original mass of the projectile. 相似文献
4.
V. V. Svetsov 《Solar System Research》2007,41(1):28-41
The atmospheric erosion induced by impacts of cosmic bodies with sizes from ～100 m to 10 km is calculated for the Earth with its present atmosphere and for Mars with a dense carbon dioxide atmosphere that could be at the early stages of planetary evolution. Numerical results are compared to simple analytic models and calculations performed by other authors; approximate formulas are suggested. The evolutions of early atmospheres, which could exist at the late stage of the planetary accumulation, are numerically simulated using an integral model of impact-induced atmospheric erosion and replenishment in the approximation of a one-component atmosphere with a composition determined by the basic atmosphile component of the bodies falling onto the planet. 相似文献
5.
Libyan Desert Glass contains meteoritic material and, therefore, its origin is most likely associated with an impact event. However, the impact crater has not been found. We performed numerical simulations of impacts of stony and cometary bodies in order to confirm the version that this glass was formed from silica heated by radiation from aerial bursts near the ground. Asteroids were treated as strengthless bodies from dunite with a density of 3.3 g cm?3, and comets as icy bodies with a density of 1 g cm?3. The simulations based on hydrodynamic equations included the equations of radiation transfer. Melting and vaporization of a silica target under action of radiation incident on a planar surface were modeled using a one‐dimensional hydrodynamic equation of energy and equations of radiation transfer in two‐flux approximation. We selected those variants of simulations in which a crater is not formed, a fireball touches the earth surface, and the area of a molten target corresponds to the area of the Libyan Desert Glass strewn field. Appropriate options include the impact of an asteroid with a diameter of 300 m, an entry speed of 35 km s?1, and an entry angle of 8°, and cometary bodies with diameters from 150 to 300 m, speeds of 50–70 km s?1, and entry angles from 15° to 45°. Impact options with crater formation are also discussed. The maximum depth of molten silica at ground zero reaches 10 cm with the cometary impacts and 3–4 cm with the asteroidal impact. Melting occurs during a period of time from 50 to 400 s. 相似文献
6.
Plumes produced by the impacts of asteroids and comets consist of rock vapor and heated air. They emit visible light, ultraviolet, and infrared radiation, which can greatly affect the environment. We have carried out numerical simulations of the impacts of stony and cometary bodies with a diameter of 0.3, 1, and 3 km, which enter the atmosphere at various angles, using a hydrodynamic model supplemented by radiation transfer. We assumed that the cosmic object has no strength, and deforms, fragments, and vaporizes in the atmosphere. After the impact on the ground, the formation of craters and plumes was simulated, taking the internal friction of destroyed rocks and the trail formed in the atmosphere into account. The equation of radiative transfer, added to the equations of gas dynamics, was used in the approximation of radiative heat conduction or, if the Rosseland optical depth of a radiating volume of gas and vapor was less than unity, in the volume‐emission approximation. We used temperature and density distributions obtained in these simulations to calculate radiation fluxes on the Earth's surface by integrating the equation of radiative transfer along rays passing through a luminous region. We used tables of the equation of state of dunite and quartz (for stony impactors and a target) and air, as well as tables of absorption coefficients of air, vapor of ordinary chondrite, and vapor of cometary material. We have calculated the radiation impulse on the ground and the impact radiation efficiency (a ratio of thermal radiation energy incident on the ground to the kinetic energy of a body), which ranges from ~0.5% to ~9%, depending on the impactor size and the angle of entry into the atmosphere. Direct thermal radiation from fireballs and impact plumes, poses a great danger to people, animals, plants, and economic objects. After the impacts of asteroids at a speed of 20 km s?1 at an angle of 45°, a fire can occur at a distance of 250 km if the asteroid has a diameter of 0.3 km, and at a distance of 2000 km if the diameter is 3 km. 相似文献
7.
Vladimir Svetsov 《Icarus》2011,214(1):316-326
I have performed 3D numerical hydrodynamic simulations of impacts of stony projectiles on stony planar targets in a range of impact velocities from 1.25 to 60 km/s. The projectile and target masses ejected at speeds greater than some given values have been calculated. This provided a possibility to determine impact erosion of a target which undergoes bombardment with comparatively small bodies. The relative losses of target masses and masses of retained projectile material have been averaged over impact angles and approximated by analytical formulas as functions of impact and escape velocities. The balance between escaped material of a target and retained material of a projectile determines growth or reduction of a target mass. The target cratering erosion predominates over the projectile retention when the impacts have velocities of more than 3-5 times the escape velocity of a target. The results can be applied to collisions of planetary embryos with planetesimals, which have higher velocities than embryo-embryo impacts. Estimates for impact velocities 1-10 km/s show that while large embryos accrete planetesimals smaller embryos erode and can completely vanish or partly lose their silicate shells if they are differentiated. Application of calculated erosion efficiency to Mercury made it possible to test a hypothesis (Vityazev, A.V., Pechernikova, G.V., Safronov, V.S. [1988]. Formation of Mercury and removal of its silicate shell. In: Vilas, F., Chapman, C.R., Matthews, M.S. (Eds.), Mercury. Univ. Arizona Press., Tucson, pp. 667−669) that differentiated massive proto-Mercury has lost its mantle due to collisions with objects of moderate sizes. It turned out that in order for this to happen, relative collision velocities must exceed 25 km/s. As alternatives to the widely-known hypothesis of a giant impact on a massive proto-Mercury, other possibilities are considered, which do not require such high speeds. The first one is formation of a number of small-sized metal-rich embryos which lose their silicate shells due to cratering erosion. The second is that a small proto-Mercury was metallic and gained its mantle at the latest stage of its accumulation when it grew so large that the erosion became ineffective. 相似文献
8.
Izvestiya, Physics of the Solid Earth - Cometary impacts on Earth, as comets themselves, especially aperiodic ones, have been much less studied compared to asteroids. Nevertheless, despite the... 相似文献
9.
We present the results of numerical simulation for impacts of relatively small asteroids and ice bodies of 30–100 m in size, decelerated in the atmosphere and exploding before they reach the surface, but still producing seismic effects due to the impact wave reaching the surface. The calculated magnitudes fall within the range of 4 to 6, and average seismic efficiency of these events is 2.5 × 10–5. The results obtained allow the seismic hazard from impacts of cosmic bodies to be estimated.
相似文献
1