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31.
Senior political and space agency personnel joined representatives of industry and other space-related institutions for a conference, held in Budapest in January 2009, on how best to structure national and European space governance. Four sessions examined the subject of the conference from a top-down European, a bottom-up national, a theoretical and actor-based and a discursive–participative perspective. The themes and outcomes of the conference are reported below.  相似文献   
32.
For the first time, empirical model of daytime vertical E×B drift based on Empirical Orthogonal functions (EOF) decomposition technique is presented. Day-to-day variability of E×B drift inferred from horizontal (H) geomagnetic field data around dip latitude for the period of 2008–2013 is used to both develop and validate the model. Results show that the EOF technique is promising with modelled values and data giving correlation coefficient values of at least 0.90 for geomagnetic conditions of both Kp?3 and Kp>3 within 2008–2013. Independent model validation shows that in situ E×B values from ion velocity meter (IVM) instrument on-board C/NOFS satellite are closer to model E×B estimates than the climatological Scherliess-Fejer (SF) model incorporated within the International Reference Ionosphere (IRI).  相似文献   
33.
As a result of increasing public and political interest in ‘space’ (i.e. solar system) exploration at the global scale, the Space Advisory Group of the European Commission has evaluated the situation in Europe with regard to its potential to participate in this ambitious global enterprise. Aspects of science, technology, environment and safety, society, spin-offs and international cooperation were all considered. The group concluded that Europe possesses sufficient key technologies and scientific expertise to play a major role in international space exploration and has recommended that the EU take a central role to ensure the success of future European space exploration, not only to give a clear political signal for the way forward but also to ensure an appropriate financial framework. In this way Europe would embrace the spirit of the European Space Policy and contribute to the knowledge-based society by investing significantly in space-based science and technology, thereby playing a strong role in international space exploration.  相似文献   
34.
35.
The Integrated Services Digital Network (ISDN) is currently evolving from its conceptualization by the CCITT international standards body to specification and implementation by network providers and equipment vendors. This paper provides an overview of ISDN standards that were approved by the CCITT in 1984, and identifies enhancements currently under study by the CCITT for 1988 approval.  相似文献   
36.
The propagation of radio signals in the Earth’s atmosphere is dominantly affected by the ionosphere due to its dispersive nature. Global Positioning System (GPS) data provides relevant information that leads to the derivation of total electron content (TEC) which can be considered as the ionosphere’s measure of ionisation. This paper presents part of a feasibility study for the development of a Neural Network (NN) based model for the prediction of South African GPS derived TEC. The South African GPS receiver network is operated and maintained by the Chief Directorate Surveys and Mapping (CDSM) in Cape Town, South Africa. Vertical total electron content (VTEC) was calculated for four GPS receiver stations using the Adjusted Spherical Harmonic (ASHA) model. Factors that influence TEC were then identified and used to derive input parameters for the NN. The well established factors used are seasonal variation, diurnal variation, solar activity and magnetic activity. Comparison of diurnal predicted TEC values from both the NN model and the International Reference Ionosphere (IRI-2001) with GPS TEC revealed that the IRI provides more accurate predictions than the NN model during the spring equinoxes. However, on average the NN model predicts GPS TEC more accurately than the IRI model over the GPS locations considered within South Africa.  相似文献   
37.
Key drivers of solar weather and mid-term solar weather are reviewed by considering a selection of relevant physics- and statistics-based scientific models as well as a selection of related prediction models, in order to provide an updated operational scenario for space weather applications. The characteristics and outcomes of the considered scientific and prediction models indicate that they only partially cope with the complex nature of solar activity for the lack of a detailed knowledge of the underlying physics. This is indicated by the fact that, on one hand, scientific models based on chaos theory and non-linear dynamics reproduce better the observed features, and, on the other hand, that prediction models based on statistics and artificial neural networks perform better. To date, the solar weather prediction success at most time and spatial scales is far from being satisfactory, but the forthcoming ground- and space-based high-resolution observations can add fundamental tiles to the modelling and predicting frameworks as well as the application of advanced mathematical approaches in the analysis of diachronic solar observations, that are a must to provide comprehensive and homogeneous data sets.  相似文献   
38.
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

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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).
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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   
39.
The ultimate objective of this paper is the estimation of rainfall over an area in Algeria using data from the SEVIRI radiometer (Spinning Enhanced Visible and Infrared Imager). To achieve this aim, we use a new Convective/Stratiform Rain Area Delineation Technique (CS-RADT). The satellite rainfall retrieval technique is based on various spectral parameters of SEVIRI that express microphysical and optical cloud properties. It uses a multispectral thresholding technique to distinguish between stratiform and convective clouds. This technique (CS-RADT) is applied to the complex situation of the Mediterranean climate of this region. The tests have been conducted during the rainy seasons of 2006/2007 and 2010/2011 where stratiform and convective precipitation is recorded. The developed scheme (CS-RADT) is calibrated by instantaneous meteorological radar data to determine thresholds, and then rain rates are assigned to each cloud type by using radar and rain gauge data. These calibration data are collocated with SEVIRI data in time and space.  相似文献   
40.
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   
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