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11.
Clays form on Earth by near-surface weathering, precipitation in water bodies within basins, hydrothermal alteration (volcanic- or impact-induced), diagenesis, metamorphism, and magmatic precipitation. Diverse clay minerals have been detected from orbital investigation of terrains on Mars and are globally distributed, indicating geographically widespread aqueous alteration. Clay assemblages within deep stratigraphic units in the Martian crust include Fe/Mg smectites, chlorites and higher temperature hydrated silicates. Sedimentary clay mineral assemblages include Fe/Mg smectites, kaolinite, and sulfate, carbonate, and chloride salts. Stratigraphic sequences with multiple clay-bearing units have an upper unit with Al-clays and a lower unit with Fe/Mg-clays. The typical restriction of clay minerals to the oldest, Noachian terrains indicates a distinctive set of processes involving water-rock interaction that was prevalent early in Mars history and may have profoundly influenced the evolution of Martian geochemical systems. Current analyses of orbital data have led to the proposition of multiple clay-formation mechanisms, varying in space and time in their relative importance. These include near-surface weathering, formation in ice-dominated near-surface groundwaters, and formation by subsurface hydrothermal fluids. Near-surface, open system formation of clays would lead to fractionation of Mars’ crustal reservoir into an altered crustal reservoir and a sedimentary reservoir, potentially involving changes in the composition of Mars’ atmosphere. In contrast, formation of clays in the subsurface by either aqueous alteration or magmatic cooling would result in comparatively little geochemical fractionation or interaction of Mars’ atmospheric, crustal, and magmatic reservoirs, with the exception of long-term sequestration of water. Formation of clays within ice would have geochemical consequences intermediate between these endmembers. We outline the future analyses of orbital data, in situ measurements acquired within clay-bearing terrains, and analyses of Mars samples that are needed to more fully elucidate the mechanisms of martian clay formation and to determine the consequences for the geochemical evolution of the planet.  相似文献   
12.
The MICROSCOPE space mission aims at testing the Equivalence Principle (EP) with an accuracy of 10?15. The test is based on the precise measurement delivered by a differential electrostatic accelerometer on-board a drag-free microsatellite which includes two cylindrical test masses submitted to the same gravitational field and made of different materials. The experiment consists in testing the equality of the electrostatic acceleration applied to the masses to maintain them relatively motionless at a well-known frequency. This high precision experiment is compatible with only very little perturbations. However, aliasing arises from the finite time span of the measurement, and is amplified by measurement losses. These effects perturb the measurement analysis. Numerical simulations have been run to estimate the contribution of a perturbation at any frequency on the EP violation frequency and to test its compatibility with the mission specifications. Moreover, different data analysis procedures have been considered to select the one minimizing these effects taking into account the uncertainty about the frequencies of the implicated signals.  相似文献   
13.
Significant advances have been made during the last decade in several fields of solid propulsion: the advances have enabled new savings in the motor development phase and recurring costs, because they help limit the number of prototypes and tests.The purpose of the paper is to describe the improvements achieved by SNPE in solid grain technologies, making these technologies available for new developments in more efficient and reliable future SRMs: new energetic molecules, new solid propellants, new processes for grain manufacturing, quick response grain design tools associated with advanced models for grain performance predictions.Using its expertise in chemical synthesis, SNPE develops new molecules to fit new energetic material requirements.Tests based on new propellant formulations have produced good results in the propellant performance/safety behavior ratio. New processes have been developed simultaneously to reduce the manufacturing costs of the new propellants.In addition, the grain design has been optimized by using the latest generation of predictive theoretical tools supported by a large data bank of experimental parameters resulting from over 30 years' experience in solid propulsion:
• Computer-aided method for the preliminary grain design
• Advanced models for SRM operating and performance predictions

References

A Davenas, D Boury, M Calabro, B D'Andrea and A Mc Donald, Solid Propulsion for Space Applications: A Roadmap, 51st IAF Congress, Rio de Janeiro, Brazil (2000).
H Austruy, M Biagioni and Y Pelipenko, Improvement in Propellant and Process for Ariane 5 Boosters (1998) AIAA 98-35588.
Y Longevialle, M Golfier, H Graindorge and G Jacob, The use of new molecules in high performances energetic materials, NDIA Insensible munitions and energetic materials technology symposium, Tampa, Florida (1999).
A.T. Nielsen, J. Org. Chem. 55 (1990), pp. 1459–1466 US Patent 5 693 794, 30/09/1998. Full Text via CrossRef | View Record in Scopus | Cited By in Scopus (58)
Bescond P, Graindorge H, Mace H, EP 913374, 6/05/1999.
G Jacob, G Lacroix and V Destombes, Identification and analysis of impurities of HNIW, 31st Annual Conference of ICT (2000).
B D'Andrea, F Lillo, A Faure and C Perut, A New Generation of Solid Propellants for Space Launchers, 50th IAF Congress, Amsterdam, The Netherlands (1999).
D.W. Doll and G.K. Lund, Magnesium neutralized clean propellant (1991) AIAA 91-2560.
C. Beckman, Clean propellants for space launch boosters, Propulsion and Energetic Panel, 84th Symposium held in Aalesund, Norway (2921994).
B. D'Andrea, B. Lillo, A. Volpi, C. Zanotti and P. Giuliani, Advanced solid propellant composition for low environmental impact and negligible erosive effect, ISTS (1998) 98-a-1-12.
J.C Chastenet and A Mobuchon, Prediction of Air Bag Performance, 5 ISCP, Stresa, Italy (2000).
J. Thépénier, D. Ribereau and E. Giraud, Grain Design for thrust trace shaping in segmented solids for the SRBs IAF-99-S.2.09, 50th IAF Congress, Amsterdam, The Netherlands (1999).
J. Thépénier, D. Ribereau and E. Giraud, Application of advanced computational softwares in propellant grain analysis : a major contribution to future SRM development for space application IAF-97-S.4.06, 48th IAF Congress, Torino, Italy (97).
A. Davenas and J. Thépénier, Recent Progress in the prediction and analysis of the operation of Solid Rocket Motors IAF-98-S2.06, 49th IAF Congress, Melbourne, Australia (1998).
D. Ribéreau, P. Le Breton and E. Giraud, SRM 3D surface burnback computation using mixes stratification deduced from 3D grain filling simulation, AIAA 99-2802, 35th AIAA JPC Conference, Los Angeles, USA (1999).
Mary. Y; “Simulation de coulée gravitaire, validation du code MONTREAL.”, DEA mechanics report, 1995.
P. Le Breton, D. Ribéreau, F. Godfroy, R. Abgrall and S. Augoula, SRM Performance Analysis by coupling bidimensional surface burnback and Pressure field computations AIAA 98-3968, 34th AIAA JPC Conference, Cleveland, USA (1998).
P. Durand, B. Vieille, H. Lambare, P. Vuillermoz, G. Bourit and P. Steinfeld, A three dimensional CFD numerical Code dedicated to space propulsive flows AIAA 00-3864, 36th AIAA JPC Conference, Huntsville, USA (2000).
  相似文献   
14.
This paper aims at investigating the stability over 150 years of a very large number of trajectories in the Medium Earth Orbit (MEO) region, near the orbits devoted to radionavigation such as the Global Navigation Satellite Systems (GNSS like GPS, Glonass, Galileo, COMPASS).  相似文献   
15.
We present the first public database of high-energy observations of all known Galactic supernova remnants (SNRs). In Section 1 we introduce the rationale for this work motivated primarily by studying particle acceleration in SNRs, and which aims at bridging the already existing census of Galactic SNRs (primarily made at radio wavelengths) with the ever-growing but diverse observations of these objects at high-energies (in the X-ray and γγ-ray regimes). In Section 2 we show how users can browse the database using a dedicated web front–end (http://www.physics.umanitoba.ca/snr/SNRcat). In Section 3 we give some basic statistics about the records we have collected so far, which provides a summary of our current view of Galactic SNRs. Finally, in Section 4, we discuss some possible extensions of this work. We believe that this catalogue will be useful to both observers and theorists, and timely with the synergy in radio/high-energy SNR studies as well as the upcoming new high-energy missions. A feedback form provided on the website will allow users to provide comments or input, thus helping us keep the database up-to-date with the latest observations.  相似文献   
16.
This paper proposes an approach for a complex and innovative project requiring international contributions from different communities of knowledge and expertise. Designing a safe and reliable architecture for a manned mission to Mars or the Asteroids necessitates strong cooperation during the early stages of design to prevent and reduce risks for the astronauts at each step of the mission. The stake during design is to deal with the contradictions, antagonisms and paradoxes of the involved partners for the definition and modeling of a shared project of reference. As we see in our research which analyses the cognitive and social aspects of technological risks in major accidents, in such a project, the complexity of the global organization (during design and use) and the integration of a wide and varie d range of sciences and innovative technologies is likely to increase systemic risks as follows: human and cultural mistakes, potential defaults, failures and accidents. We identify as the main danger antiquated centralized models of organization and the operational limits of interdisciplinarity in the sciences. Beyond this, we can see that we need to take carefully into account human cooperation and the quality of relations between heterogeneous partners. Designing an open, self-learning and reliable exploration system able to self-adapt in dangerous and unforeseen situations implies a collective networked intelligence led by a safe process that organizes interaction between the actors and the aims of the project. Our work, supported by the CNES (French Space Agency), proposes an innovative approach to the coordination of a complex project.  相似文献   
17.
18.
The Pioneer anomaly refers to the difference between the computed trajectories of the Pioneer 10 and 11 spacecrafts and their actual trajectories as observed through Doppler tracking. This difference has been described by the Jet Propulsion Laboratory (JPL) as a constant anomalous acceleration. In order to perform an independent analysis, specific trajectography software, named ODYSSEY, has been developed. The paper will focus on the models implemented in this software and on the results obtained. The existence of a constant anomalous acceleration is confirmed with properties similar to those reported by JPL. Time dependent components of the anomaly are also found and discussed.  相似文献   
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