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151.
Planetary protection is NASA's term for the practice of protecting solar system bodies from Earth life while protecting Earth from life that may be brought back from other solar system bodies. Spacefaring nations will soon begin retrieving samples from Mars and other solar system bodies. For these samples, planetary protection is in order, and measures are already in place to prevent the forward contamination of Mars and other bodies by Earth microbes and the backward contamination of Earth by possible extraterrestrial life. A major goal of planetary protection controls on forward contamination is to preserve the planetary record of natural processes by preventing human-caused microbial introductions. 相似文献
152.
153.
Thérèse Encrenaz 《Space Science Reviews》1992,61(1-2):13-17
The ISO mission is expected to allow significant progress in the study of Solar-System objects, especially concerning planetary and cometary atmospheres. Beyond ISO, future Solar-System studies using infrared space missions will require an extension of the spectral coverage toward longer wavelengths and increased spatial capabilities for imaging spectroscopy. 相似文献
154.
Darrell F. Strobel 《Space Science Reviews》2005,116(1-2):155-170
The photochemistries of the H2-He atmospheres of the gas giants Jupiter, Saturn and ice giants Uranus and Neptune and Titan’s mildly reducing N2 atmosphere are reviewed in terms of general chemical and physical principles. The thermochemical furnace regions in the deep
atmospheres and the photochemical regions of the giant planets are coupled by vertical mixing to ensure efficient recyling
of photochemical products. On Titan,mass loss of hydrogen ensures photochemical evolution of methane into less saturated hydrocarbons.
A summary discussion of major dissociation paths and essential chemical reactions is given. The chapter ends with a overview
of vertical transport processes in planetary atmospheres. 相似文献
155.
J. Barengoltz J. Witte 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
In August 2005 NASA launched a large orbiting science observatory, the Mars Reconnaissance Orbiter (MRO), for what is scheduled to be a 5.4-year mission. High resolution imaging of the surface is a principal goal of the mission. One consequence of this goal however is the need for a low science orbit. Unfortunately this orbit fails the required 20-year orbit life set in NASA Planetary Protection (PP) requirements [NASA. Planetary protection provisions for robotic extraterrestrial missions, NASA procedural requirements NPR 8020.12C, NASA HQ, Washington, DC, April 2005.]. So rather than sacrifice the science goals of the mission by raising the science orbit, the MRO Project chose to be the first orbiter to pursue the bio-burden reduction approach. 相似文献
156.
Thér‘se Encrenaz 《Space Science Reviews》2005,116(1-2):99-119
Measurements of the chemical composition of the giant planets provide clues of their formation and evolution processes. According
to the currently accepted nucleation model, giant planets formed from the initial accretion of an icy core and the capture
of the protosolar gas, mosly composed of hydrogen and helium. In the case of Jupiter and Saturn (the gaseous giants), this
gaseous component dominates the composition of the planet, while for Uranus and Neptune (the icy giants) it is only a small
fraction of the total mass. The measurement of elemental and isotopic ratios in the giant planets provides key diagnostics
of this model, as it implies an enrichment in heavy elements (as well as deuterium) with respect to the cosmic composition.
Neutral atmospheric constituents in the giant planets have three possible sources: (1) internal (fromthe bulk composition
of the planet), (2) photochemical (fromthe photolysis ofmethane) and(3) external (from meteoritic impacts, of local or interplanetary
origin). This paper reviews our present knowledge about the atmospheric composition in the giant planets, and their elemental
and istopic composition. Measurements concerning key parameters, like C/H, D/H or rare gases in Jupiter, are analysed in detail.
The conclusion addresses open questions and observations to be performed in the future. 相似文献
157.
Yoav Yair 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
We present the latest observations from spacecraft and ground-based instruments in search for lightning activity in the atmospheres of planets in the solar system, and put them in context of previous research. Since the comprehensive book on planetary atmospheric electricity compiled by Leblanc et al. (2008), advances in remote sensing technology and telescopic optics enable detection of additional and new electromagnetic and optical emissions, respectively. Orbiting spacecraft such as Mars Express, Venus Express and Cassini yield new results, and we highlight the giant storm on Saturn of 2010/2011 that was probably the single most powerful thunderstorm ever observed in the solar system. We also describe theoretical models, laboratory spark experiments simulating conditions in planetary mixtures and map open issues. 相似文献
158.
A. ElShafie V.F. Chevrier R. Ulrich L. Roe 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The Optical Probe for Regolith Analysis (OPRA) is a spike-shaped subsurface analytical probe that will be delivered to a planet, asteroid, or cometary body by a lander and/or rover. OPRA will be pushed down into the subsurface to record near infrared spectra as a function of depth down to maximum of 50 cm. Therefore, knowledge of the required penetration force to specific depths can be helpful in estimating the length of the probe. Test probes covering the anticipated diameter (2.5, 1.9, 1.2 and 0.9 cm diameter) and tip angle (T.A. = 30°, 60°, 90° and 120°) of OPRA were inserted mechanically into dry playground sand. The results showed that tip angle does not have a major effect, while probe diameter and density of the regolith are the most important parameters. Increasing probe diameter from 0.9 to 1.9 cm (i.e. a factor of 2) leads to an increase in penetration force from 200 to 1000 N (i.e. a factor of 5) at 20 cm depth. An increase in bulk density (B.D.) from 1550 to 1700 kg m−3 leads to an increase in penetration force from 10 to 200 N at 20 cm depth. Bearing capacity theory was used to explain the downward movement of the penetrometer through regolith and showed good agreement with the experimental results. This model was then used to take into account the effect of gravity on other planetary bodies. We observed a good agreement between the theoretical model and results from penetration testings on the Moon by the Apollo missions. Since the maximum allowed force for penetration is the weight of the lander/rover on their targeted planetary surface, our results put a strong constraint on the maximum reachable depth without endangering the whole mission. 相似文献
159.
F.C. Wasiak A. Luspay-Kuti W.D.D.P. Welivitiya L.A. Roe V.F. Chevrier D.G. Blackburn T. Cornet 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
As a result of measurements acquired by the Cassini–Huygens mission of Titan’s near surface atmospheric composition and temperature, Titan conditions can now be simulated in the laboratory and samples can subsequently be subjected to those conditions. Titan demonstrates an active hydrological-like cycle with its thick atmosphere, dynamic clouds, polar lakes of methane and ethane, moist regolith, and extensive fluvial erosive features. Unlike Earth, Titan’s hydrological-like cycle likely involves several constituents, primarily methane and ethane. Here the properties of a new Titan simulation facility are presented, including conceptual methodology, design, implementation, and performance results. The chamber maintains Titan’s surface temperature and pressure, and the sample cryogenic liquids undergoing experimentation are condensed within the chamber itself. During the experiments, the evaporation rates of the sample liquids are directly determined by continually measuring mass. Constituents are analyzed utilizing a Fourier Transform Infrared Spectroscopy (FTIR), and vapor concentrations are determined using a gas chromatograph fitted with a Flame Ionization Detector (FID). All pertinent data is logged via computer. Under laboratory conditions, the direct measurements of the evaporation rates of methane, ethane, and mixtures thereof can be achieved. Among the processes to be studied are the effects of regolith on transport from the subsurface to the atmosphere, the freezing point depression effects of dissolved nitrogen, and the solubility of various relevant organic compounds. 相似文献
160.
利用中国岢岚站(38.7°N,111.6°W)法布里-珀罗干涉仪2013年7月至2014年11月的水平风场数据,对87,97,250km风场长期变化和行星波特征进行了研究.通过分析年振荡(AO)和半年振荡(SAO)振幅相位,将午夜风场与HWM07数据对比发现:87km和97km处FPI纬向风变化趋势与HWM07相近,而经向风相位落后于HWM07,从振幅上看,HWM07振幅偏大;250km处风场月变化大,FPI与HWM07差异大,HWM07模式的准确性需进一步考虑太阳活动和行星际磁场的影响.利用Lomb-Scargle功率谱以及最小二乘谐波拟合提取了三个高度的行星波振幅,其特征表明87km和97km处纬向风16日波秋季及冬春季活动强,而6.5日波最强振幅出现在春季和秋季,在中间层顶附近两种行星波活动均较弱;250km处经向行星波活动略强于纬向,经向风不同周期带的行星波最强振幅主要出现在5-9月,与电离层f0F2振荡特性的研究结果一致. 相似文献