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1.
Jones EG  Lineweaver CH  Clarke JD 《Astrobiology》2011,11(10):1017-1033
We present a comprehensive model of martian pressure-temperature (P-T) phase space and compare it with that of Earth. Martian P-T conditions compatible with liquid water extend to a depth of ~310?km. We use our phase space model of Mars and of terrestrial life to estimate the depths and extent of the water on Mars that is habitable for terrestrial life. We find an extensive overlap between inhabited terrestrial phase space and martian phase space. The lower martian surface temperatures and shallower martian geotherm suggest that, if there is a hot deep biosphere on Mars, it could extend 7 times deeper than the ~5?km depth of the hot deep terrestrial biosphere in the crust inhabited by hyperthermophilic chemolithotrophs. This corresponds to ~3.2% of the volume of present-day Mars being potentially habitable for terrestrial-like life.  相似文献   

2.
Apollo should not serve as a model for the many programs for lunar and planetary exploration currently making headway: it was a unilateral effort whose generous budget would be inconceivable today. Yet President Kennedy was an advocate of cooperation in major space missions, an attitude that makes perfect sense today, when so many agencies have ambitious exploration plans. The importance of President G.W. Bush's ‘Vision for Space Exploration’, by providing a focus for NASA and others, has been underestimated. It should give us a chance to find out whether a long-term objective of moving humans off the home planet is really feasible—surely the point of exploration.  相似文献   

3.
The project STEPS (Sistemi e Tecnologie per l'EsPlorazione Spaziale) is a joint development of technologies and systems for Space Exploration supported by Regione Piemonte, the European Regional Development Fund (E.R.D.F.) 2007-2013, Thales Alenia Space Italia (TAS-I), SMEs, Universities and public Research Centres belonging to the network “Comitato Distretto Aerospaziale del Piemonte” the Piedmont Aerospace District (PAD) in Italy. The project first part terminated in May 2012 with a final demonstration event that summarizes the technological results of research activities carried-out during a period the three years and half. The project developed virtual and hardware demonstrators for a range of technologies for the descent, soft landing and surface mobility of robotic and manned equipment for Moon and Mars exploration. The two key hardware demonstrators—a Mars Lander and a Lunar Rover—fit in a context of international cooperation for the exploration of Moon and Mars, as envisaged by Space Agencies worldwide. The STEPS project included also the development and utilization of a system of laboratories equipped for technology validation, teleoperations, concurrent design environments, and virtual reality simulation of the Exploration Systems in typical Moon and Mars environments. This paper presents the reached results in several technology domains like: vision-based GNC for the last portion of Mars Entry, Descent and Landing sequence, Hazard avoidance and complete spacecraft autonomy; Autonomous Rover Navigation, based on the determination of the terrain morphology by a stereo camera; Mobility and Mechanisms providing an Integrated Ground Mobility System, Rendezvous and Docking equipment, and protection from Environment effects; innovative Structures such as Inflatable, Smart and Multifunction Structures, an Active Shock Absorber for safe landing, balance restoring and walking; Composite materials Modelling and Monitoring; Human-machine interface features of a predictive Command and Control System; Energy Management systems based on Regenerative Fuel Cells; aerothermodynamic solutions for Atmospheric Re-entry of Commercial Transportation Systems; novel Design and Development Tools, such as a Rover S/W simulator and prototypes of the DEM viewer and of a S/W Rock Creator/visualizator.The paper also provides perspectives on the proposed STEPS 2 project that will likely continue the development of a subset of the above technologies in view of their possible in-flight validation within next five years.  相似文献   

4.
深空探测对航天器热控技术的推动   总被引:1,自引:0,他引:1  
工程热物理学广泛应用于航天领域,一方面解决了具体航天工程问题,另一方面逐步发展成为交叉学科——空间热物理。随着我国在深空探测领域不断拓展,以深空探测器研制中的工程热物理问题为需求背景,推动着航天器热控制技术、防热技术等取得新的发展。文章在介绍深空探测器技术体系的基础上,分析了热设计、热分析、热试验、热控硬件、防热等方面的技术进步,并就深空探测领域进一步拓展对工程热物理发展的牵引进行了展望,分析了工程热物理学与航天技术间相互促进、相互推动的关系。  相似文献   

5.
The release and oxidation of ferrous iron during aqueous alteration of the mineral olivine is known to reduce aqueous solutions to such extent that molecular hydrogen, H2, forms. H2 is an efficient energy carrier and is considered basal to the deep subsurface biosphere. Knowledge of the potential for H2 generation is therefore vital to understanding the deep biosphere on Earth and on extraterrestrial bodies. Here, we provide a review of factors that may reduce the potential for H2 generation with a focus on systems in the core temperature region for thermophilic to hyperthermophilic microbial life. We show that aqueous sulfate may inhibit the formation of H2, whereas redox-sensitive compounds of carbon and nitrogen are unlikely to have significant effect at low temperatures. In addition, we suggest that the rate of H2 generation is proportional to the dissolution rate of olivine and, hence, limited by factors such as reactive surface areas and the access of water to fresh surfaces. We furthermore suggest that the availability of water and pore/fracture space are the most important factors that limit the generation of H2. Our study implies that, because of large heat flows, abundant olivine-bearing rocks, large thermodynamic gradients, and reduced atmospheres, young Earth and Mars probably offered abundant systems where microbial life could possibly have emerged.  相似文献   

6.
The space elevator in the context of current space exploration policy   总被引:2,自引:1,他引:1  
Mark S. Avnet 《Space Policy》2006,22(2):133-139
The space elevator is an advanced space transportation system that someday could replace chemical rockets as humanity's primary means of reaching Earth's orbit. However, before this can occur, a number of enabling technologies will need to be developed, and a variety of economic and policy questions must be addressed. The goal of this paper is to examine the feasibility of the space elevator in the context of current space exploration policy. The paper reviews the space elevator's critical enabling technologies and presents their wide variety of applications. The challenges of funding the space elevator and of building support for the program are discussed. The potential for international cooperation is considered, and the role of the space elevator in the Vision for Space Exploration is examined. The paper argues that each of the space elevator's component technologies ought to be developed independently to meet separate nearer-term objectives. The space elevator should be just one of many applications considered in making decisions to pursue research and development related to each component technology. The enabling technologies, once mature, might eventually be integrated in the construction of a full-scale space elevator from the Earth's surface to geosynchronous orbit and beyond.  相似文献   

7.
A Mars manned space mission would be characterized by long-lasting psycho-social stress for its human participants. Based on the results of our and other authors' experiments with small human groups under simulated space stress conditions, and bearing in mind historical evidence of the changing role of women in human society, the differences of feminine and masculine cognitive patterns should be taken into greater account. Participation of women in astronautics should be reconsidered from the point of view of the roles of women as members of a space ship crew, as members of a space control centre and in relation to the family life of male astronauts on long-term space missions.  相似文献   

8.
As NASA struggles to fund and execute its ambitious Space Station Freedom and Mission to Planet Earth programmes, President Bush has pledge the nation to a programme to return humans to the Moon to stay and to explore Mars. While not predicted on scientific grounds, this Space Exploration Initiative welcomes the support and participation of the scientific community. Success in establishing this relationship will depend on how the initiative is structured, sold and managed within the context of scientists' past experience with large, manned flight programmes.  相似文献   

9.
国外深空探测推进技术发展及启示   总被引:1,自引:0,他引:1  
推进系统为探测器的飞行提供所需的控制力和控制力矩,一定程度上决定了探测器的规模、最远飞行距离,乃至任务的成败,是探测器的重要分系统之一。为满足不同的深空探测任务需求,国外发展了多种形式的推进技术,但总体上仍以化学推进为主,部分采用了电推进系统,并在发展高性能低温推进技术等。对国外典型探测器推进系统进行了叙述,分析了其技术特点和发展趋势,并分别针对无人探测和载人探测应用探讨了对我国开展深空探测推进技术研究的启示。  相似文献   

10.
论航天型号项目的协作及项目群的管理   总被引:1,自引:0,他引:1  
文章主要针对我国航天型号项目管理中存在的问题进行分析和研究。例如在大型环境试验和总装过程中,单一项目的管理已经日臻完善;但面对更加繁重的任务和巨大的发展机遇,单一项目的管理所暴露出的问题也越发明显。文章拟用项目群的管理思路来完善和丰富项目管理体系,从而促进环境试验和总装的项目管理水平。  相似文献   

11.
未来的深空探测与空间环境模拟   总被引:2,自引:1,他引:1  
文章介绍了国内外有代表性的深空探测计划的内容、特点和意义,包括:欧空局的Exo Mars火星车、美国"2020火星车"以及中国的2020火星探测计划;金星着陆探测进展情况;欧空局木星系统探测计划"木星冰月亮探索者(JUICE)"和美国的"木卫二飞越任务(Europa Clipper)";"蜻蜓号(Dragonfly)"土卫六探测项目;美国的"彗星天体生物学探索取样返回(CAESAR)"项目;月球探测计划等。还分析了未来深空探测对空间环境模拟的具体要求,空间环境模拟对推动深空探测发展的重要意义;提出了对我国未来开展空间环境模拟试验的建议。  相似文献   

12.
This article discusses the outcomes of an April 2005 workshop held at ISU in Strasbourg. Experts sought to tailor an international co-ordination mechanism that would achieve the classical benefits of international co-operation for the unique venture of space exploration. The mechanism they developed provides a permanent forum for those with vested interests in exploration (currently space agencies in key spacefaring nations) to exchange information about national plans and activities so as to build confidence in one another's programs and, to the extent they choose, to develop beneficial interdependencies. The product of this co-ordination effort would be a consolidated international exploration roadmap that would both inform and reflect national program decisions. The co-ordination mechanism would simultaneously involve, but in less central roles, other important interested parties (industry, the science community, other countries without current exploration programs), whose advice is important to the development of a consolidated roadmap. Recognizing that the stakeholders in exploration will almost certainly evolve over time, the mechanism also presents the flexibility to accommodate new players (e.g. companies and countries not yet with investments in exploration) in more central roles as they become stakeholders with vested interests in exploration.  相似文献   

13.
14.
15.
载人深空探测任务航天医学工程问题研究   总被引:2,自引:1,他引:1  
航天医学工程问题关系到载人深空探测任务中的人员生存及健康。文章从人员长期生存的生命保障、变重力生理效应及防护、地外环境效应与防护、人员生理健康监测与维护、人员心理健康等方面的问题入手,分析了问题产生的原因及解决的必要性,并提出了解决思路,为后续深入开展相关关键技术的攻关提供参考。最后,以载人月球基地任务为案例,提出了生命保障、变重力防护、辐射及月尘防护、生理及心理健康监测及维护等问题的解决方案。  相似文献   

16.
After a large consultation with the scientific and industrial communities in Europe, the Aurora Space Exploration Programme was unanimously approved at the European Space Agency (ESA) Council at ministerial level in Edinburgh in 2001. This marked the start of the programme's preparation phase that was due to finish by the end of 2004. Aurora features technology development robotic and crewed rehearsal missions aimed at preparing a human mission to Mars by 2033. Due to the evolving context, both international and European, ESA has undertaken a review of the goals and approach of its exploration programme. While maintaining the main robotic missions that had been conceived during Aurora, the European Space Exploration Programme that is currently being proposed to the Aurora participating states and other ESA Member States has a reviewed approach and will feature a greater synergy with other ESA programmes. The paper will present the process that led to the revision of ESA's plans in the field of exploration and will give the current status of the programme.  相似文献   

17.
As well as providing practical information on Earth-besetting problems, space science and exploration are vital tools for capturing the public imagination and encouraging young people's interest in space. The relatively small scale of some scientific instruments also allows mission participation by developing countries. Citing the work of the UN and various NGOs in promoting study and distribution of space science data, the authors recommend that it be given a higher profile and suggest a number of projects -- the Mars drill study in Egypt, refurbishment of a telescope facility in Sri Lanka -- involving developing countries that should be followed up, as well as listing ongoing successful projects. The UN is urged to continue its annual workshops on space science (apparently under threat) and to ensure its inclusion in the forthcoming UNISPACE III Conference.  相似文献   

18.
M D Ross 《Acta Astronautica》2001,49(3-10):441-445
Safety of astronauts during long-term space exploration is a priority for NASA. This paper describes efforts to produce Earth-based models for providing expert medical advice when unforeseen medical emergencies occur on spacecraft. These models are Virtual Collaborative Clinics that reach into remote sites using telecommunications and emerging stereo-imaging and sensor technologies.  相似文献   

19.
Stephen J. Pyne   《Space Policy》2007,23(3):147-149
The polar regions have often been suggested as surrogates for the exploration and colonization of space. In particular, Antarctica's greater isolation makes it a useful analogue. Its features—abiotic, acultural, alien to human habitation—all echo the regions of interest to contemporary exploration, notably the solar system and the deep oceans. But more than a century of Antarctic experience also suggests that exploration will likely resemble the Renaissance's Great Voyages and their outposts rather than become portals for wholesale colonization. These sites will traffic mostly in information—the spices and luxury goods of interest to their sustaining societies.  相似文献   

20.
全相位快速傅里叶变换(all phase Fast Fourier Transform,apFFT)相位一致性特点使正弦信号相位估计不受频率估计影响,但由于频谱泄露和栅栏效应,apFFT相位估计性能受信号频率位置影响。针对该问题,提出了一种基于高精度频率估计和补偿的apFFT相位估计方法。首先,对信号进行高精度频率估计,并以此对信号进行频移补偿,然后对补偿信号进行apFFT,最后求解信号相位。蒙特卡洛仿真结果表明:所提算法的相位估计性能不受信号频率位置影响,相位估计误差性能与理论值一致,受两参数克拉美罗界(CRLB2)约束,约为1.158 2倍的CRLB2;相位估计性能和抗噪声能力明显优于经典apFFT算法和其他对比算法。更进一步,利用我国首次火星探测器TW-1(天问一号)近火捕获段干涉测量数据进行算法验证,结果表明:相位估计精度约4 mrad,干涉测量时延估计精度约50 ps。  相似文献   

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