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871.
The purpose of the research is to develop a photo-bioreactor which may produce algae protein and oxygen for future astronauts in comparatively long-term exploration, and remove carbon dioxide in a controlled ecological life support system. Based on technical parameters and performance requirements, the project planning, design drafting, and manufacture were conducted. Finally, a demonstration test for producing algae was done. Its productivity for micro-algae and performance of the photo-bioreactor were evaluated. The facility has nine subsystems, including the reactor, the illuminating unit, the carbon dioxide (CO2) production unit and oxygen (O2) generation unit, etc. The demonstration results showed that the facility worked well, and the parameters, such as energy consumption, volume, and productivity for algae, met with the design requirement. The density of algae in the photo-bioreactor increased from 0.174 g (dry weight) L−1 to 4.064 g (dry weight) L−1 after 7 days growth. The principle of providing CO2 in the photo-bioreactor for algae and removing O2 from the culture medium was suitable for the demand of space conditions. The facility has reasonable technical indices, and smooth and dependable performances.  相似文献   
872.
We present the work of an international team at the International Space Science Institute (ISSI) in Bern that worked together to review the current observational and theoretical status of the non-virialised X-ray emission components in clusters of galaxies. The subject is important for the study of large-scale hierarchical structure formation and to shed light on the “missing baryon” problem. The topics of the team work include thermal emission and absorption from the warm-hot intergalactic medium, non-thermal X-ray emission in clusters of galaxies, physical processes and chemical enrichment of this medium and clusters of galaxies, and the relationship between all these processes. One of the main goals of the team is to write and discuss a series of review papers on this subject. These reviews are intended as introductory text and reference for scientists wishing to work actively in this field. The team consists of sixteen experts in observations, theory and numerical simulations.  相似文献   
873.
The New Horizons Spacecraft   总被引:1,自引:0,他引:1  
The New Horizons spacecraft was launched on 19 January 2006. The spacecraft was designed to provide a platform for seven instruments designated by the science team to collect and return data from Pluto in 2015. The design meets the requirements established by the National Aeronautics and Space Administration (NASA) Announcement of Opportunity AO-OSS-01. The design drew on heritage from previous missions developed at The Johns Hopkins University Applied Physics Laboratory (APL) and other missions such as Ulysses. The trajectory design imposed constraints on mass and structural strength to meet the high launch acceleration consistent with meeting the AO requirement of returning data prior to the year 2020. The spacecraft subsystems were designed to meet tight resource allocations (mass and power) yet provide the necessary control and data handling finesse to support data collection and return when the one-way light time during the Pluto fly-by is 4.5 hours. Missions to the outer regions of the solar system (where the solar irradiance is 1/1000 of the level near the Earth) require a radioisotope thermoelectric generator (RTG) to supply electrical power. One RTG was available for use by New Horizons. To accommodate this constraint, the spacecraft electronics were designed to operate on approximately 200 W. The travel time to Pluto put additional demands on system reliability. Only after a flight time of approximately 10 years would the desired data be collected and returned to Earth. This represents the longest flight duration prior to the return of primary science data for any mission by NASA. The spacecraft system architecture provides sufficient redundancy to meet this requirement with a probability of mission success of greater than 0.85. The spacecraft is now on its way to Pluto, with an arrival date of 14 July 2015. Initial in-flight tests have verified that the spacecraft will meet the design requirements.  相似文献   
874.
Using our new 3-D relativistic particle-in-cell (PIC) code parallelized with MPI, we investigated long-term particle acceleration associated with a relativistic electron–positron jet propagating in an unmagnetized ambient electron–positron plasma. The simulations were performed using a much longer simulation system than our previous simulations in order to investigate the full nonlinear stage of the Weibel instability and its particle acceleration mechanism. Cold jet electrons are thermalized and ambient electrons are accelerated in the resulting shocks. Acceleration of ambient electrons leads to a maximum ambient electron density three times larger than the original value as predicted by hydrodynamic shock compression. In the jet (reverse) shock behind the bow (forward) shock the strongest electromagnetic fields are generated. These fields may lead to time dependent afterglow emission. In order to calculate radiation from first principles that goes beyond the standard synchrotron model used in astrophysical objects we have used PIC simulations. Initially we calculated radiation from electrons propagating in a uniform parallel magnetic field to verify the technique. We then used the technique to calculate emission from electrons in a small simulation system. From these simulations we obtained spectra which are consistent with those generated from electrons propagating in turbulent magnetic fields with red noise. This turbulent magnetic field is similar to the magnetic field generated at an early nonlinear stage of the Weibel instability. A fully developed shock within a larger simulation system may generate a jitter/synchrotron spectrum.  相似文献   
875.
研究了圆锥运动情况下陀螺角增量采样量化对姿态误差的影响, 对比分析 了单子样算法、三子样扩展频率级数算法和三子样显式频率整形算法,理论推导给出陀 螺角增量分辨率造成的量化误差方差和圆锥算法姿态误差方差间关系的理论表达式。推 导公式及蒙特卡罗仿真结果表明,除通过脉冲细分提高陀螺角增量分辨率外,低通滤波 和提高姿态更新频率也可减小量化误差对姿态解算的误差影响。  相似文献   
876.
This paper considers the use of spatio-temporal adaptive array processing in over-the-horizon radar (OTHR) and airborne radar applications in order to remove nonstationary multipath interference, known as “hot clutter”. Since the spatio-temporal properties of hot clutter cannot be assumed constant over the coherent processing interval (CPI), conventional adaptive techniques fail to provide effective hot-clutter mitigation without simultaneously degrading the properties of the backscattered radar signals, known as “cold clutter”. The approach presented incorporates multiple “stochastic” (data-dependent) constraints to achieve effective hot-clutter suppression, while maintaining distortionless output cold-clutter post-processing stationarity  相似文献   
877.
We readily convince ourselves that most achievements can be credited to the construction of powerful jet engines, which enable a spaceship to escape gravity. The principle of jet propulsion seems to work perfectly; jet engines can accelerate a rocket up to an incredible speed of 11 km/sec. Looks like there is nothing left to desire. However, from the physical point of view, 11 km/sec is not such a large value compared, for instance, to the speed of light. Would it be possible to attain half of that speed using gas jets? Unfortunately, the answer is no. Nevertheless, that is not the end of the story. The purpose of this article is to show that it is still possible to use the same principle to remove limitations on attainable speed if instead of gas jets, we employ ultrafast electron beams. The basic idea of our construction was inspired by the paper by H. Morgan (ibid., vol. 13, pp. 5-10, 1998). In that article he experimentally refuted the common premise that nothing can go faster than light and gave some theoretical arguments supporting his experimental data. Although the nature and underlying principles of the Morgan phenomenon are yet to be understood, we can already start thinking of its practical applications  相似文献   
878.
Passive tracking scheme for a single stationary observer   总被引:1,自引:0,他引:1  
While there are many techniques for bearings-only tracking (BOT) in the ocean environment, they do not apply directly to the land situation. Generally, for tactical reasons, the land observer platform is stationary; but, it has two sensors, visible and infrared, for measuring bearings and a laser range finder (LRF) for measuring range. There is a requirement to develop a new BOT data fusion scheme that fuses the two sets of bearing readings, and together with a single LRF measurement, produces a unique track. This paper first develops a parameterized solution for the target speeds, and then heading, prior to the occurrence of the LRF measurement, when the track is unobservable. At, and after the LRF measurement, a BOT, formulated as a least squares (LS) estimator, then produces a unique LS estimate of the target states. Bearing readings from the other sensor serve as instrumental variables in a data fusion setting to eliminate the bias in the BOT estimator. The result is an unbiased and decentralized data fusion scheme. Results from two simulation experiments have corroborated the theoretical development and show also that the scheme is optimal.  相似文献   
879.
The effect of clinostat-simulated microgravity on SP-2/0 and 1D6 hybridoma cells was studied. Clinorotation during 4-5 days at 1.5 rounds per minute decreased dramatically their proliferating capacity: the rotated cells divided less than once while control cells performed 4-5 divisions. They decreased the non-specific adhesion to tissue culture plastic, but increased the number of cell-to-cell contacts. Such phenomenological changes were accompanied with the alterations in pericellular glycosaminoglycans: decreased accumulation of hyaluronic acid and increased accumulation of chondroitin/dermatan-sulfate, as well as with the increase of cytoplasmic Ca2+ concentration. Clinorotation resulted in hybridoma nicotinic receptor desensitization but not down-regulation. In contrast, both the quantity and quality (molecular isoforms, affinity and specificity) of the antibody produced by 1D6 hybridoma cells were not altered by clinorotation. It is concluded that simulated microgravity affected the proliferating and adhesive, but not biosynthetic properties of hybridoma cells.  相似文献   
880.
Single cells and cell culture are very good model for estimation of primary effects of gravitational changes. It is suggested that cell cytoskeleton plays a key role in mechanisms of adaptation to mechanical influences including gravitational ones. Our results demonstrated that cultured cells of human vascular endothelium (correction of endotheliun) are highly sensitive to hypogravity (clinorotation) and respond by significant decrease of cell proliferative activity. Simultaneously it was noted that the formation of confluent monolayer appeared early in cultures exposed to simulated microgravity due to accelerated cells spreading. Long-term hypogravity (several hours or days) leads to significant changes of cell cytoskeleton revealed as microfilament thinning and their redistribution within cell. Such changes were observed only in monolayer cells and not in cell suspensions. Gravitational forces as known to be modificators of cell adhesive ability and determine their mobility. Hypogravity environment stimulated endothelial cell migration in culture: 24-48 hrs pre-exposition to hypogravity significantly increased endothelial cell migration resulting in 2-3-fold acceleration of mechanically injured monolayer repair. Obtained results suggest that the effects of hypogravity on cultured human endothelial cells are, possibly, associated with protein kinase C and/or adenylate cyclase activity and are accompanied by noticeable functional cell changes.  相似文献   
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