全文获取类型
收费全文 | 2602篇 |
免费 | 5篇 |
国内免费 | 5篇 |
专业分类
航空 | 1345篇 |
航天技术 | 890篇 |
综合类 | 16篇 |
航天 | 361篇 |
出版年
2018年 | 29篇 |
2017年 | 24篇 |
2014年 | 32篇 |
2013年 | 61篇 |
2012年 | 35篇 |
2011年 | 86篇 |
2010年 | 60篇 |
2009年 | 86篇 |
2008年 | 137篇 |
2007年 | 54篇 |
2006年 | 49篇 |
2005年 | 52篇 |
2004年 | 73篇 |
2003年 | 85篇 |
2002年 | 46篇 |
2001年 | 60篇 |
2000年 | 63篇 |
1999年 | 33篇 |
1998年 | 83篇 |
1997年 | 58篇 |
1996年 | 69篇 |
1995年 | 72篇 |
1994年 | 89篇 |
1993年 | 53篇 |
1992年 | 70篇 |
1991年 | 33篇 |
1990年 | 34篇 |
1989年 | 73篇 |
1988年 | 29篇 |
1987年 | 33篇 |
1986年 | 58篇 |
1985年 | 103篇 |
1984年 | 56篇 |
1983年 | 62篇 |
1982年 | 58篇 |
1981年 | 72篇 |
1980年 | 37篇 |
1979年 | 29篇 |
1978年 | 27篇 |
1977年 | 25篇 |
1975年 | 25篇 |
1974年 | 26篇 |
1973年 | 26篇 |
1972年 | 21篇 |
1971年 | 32篇 |
1970年 | 18篇 |
1969年 | 25篇 |
1968年 | 23篇 |
1967年 | 26篇 |
1966年 | 22篇 |
排序方式: 共有2612条查询结果,搜索用时 15 毫秒
951.
952.
John Caldwell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1981,1(9):199-213
A discussion is given of the various capabilities and advantages of the Space Telescope observatory, scheduled for launch into Earth-orbit in 1984. The first generation instruments are described, and a detailed example for one specific observing program, an intercomparison of Uranus and Neptune, is made. The importance of an extra-solar planet search is emphasized. 相似文献
953.
A Comparison of Complementary and Kalman Filtering 总被引:1,自引:0,他引:1
A technique used in the flight control industry for estimation when combining measurements is the complementary filter. This filter is usually designed without any reference to Wiener or Kalman filters, although it is related to them. This paper, which is mainly tutorial, reviews complementary filtering and shows its relationship to Kalman and Wiener filtering. 相似文献
954.
955.
956.
Maurer RH Roth DR Kinnison JD Goldsten JO Gold RE Fainchtein R 《Acta Astronautica》2003,52(2-6):405-410
We describe the instrument design and detector development for MANES which has been selected to fly on the Mars 2003 Lander. Section 1 explains the need for the spectrometer in determining the increased risk of carcinogenesis for astronauts. Section 2 presents the instrument design including an outline drawing, a cross-sectional view and a detailed block diagram. Sections 3 and 4 describe the low and high energy detector components of the spectrometer and present responses to monoenergetic neutron beams. Sections 5 and 6 explain the design approaches to charged particle discrimination and instrument transfer function modeling. 相似文献
957.
958.
H. O. Funsten R. M. Skoug A. A. Guthrie E. A. MacDonald J. R. Baldonado R. W. Harper K. C. Henderson K. H. Kihara J. E. Lake B. A. Larsen A. D. Puckett V. J. Vigil R. H. Friedel M. G. Henderson J. T. Niehof G. D. Reeves M. F. Thomsen J. J. Hanley D. E. George J.-M. Jahn S. Cortinas A. De Los Santos G. Dunn E. Edlund M. Ferris M. Freeman M. Maple C. Nunez T. Taylor W. Toczynski C. Urdiales H. E. Spence J. A. Cravens L. L. Suther J. Chen 《Space Science Reviews》2013,179(1-4):423-484
The HOPE mass spectrometer of the Radiation Belt Storm Probes (RBSP) mission (renamed the Van Allen Probes) is designed to measure the in situ plasma ion and electron fluxes over 4π sr at each RBSP spacecraft within the terrestrial radiation belts. The scientific goal is to understand the underlying physical processes that govern the radiation belt structure and dynamics. Spectral measurements for both ions and electrons are acquired over 1 eV to 50 keV in 36 log-spaced steps at an energy resolution ΔE FWHM/E≈15 %. The dominant ion species (H+, He+, and O+) of the magnetosphere are identified using foil-based time-of-flight (TOF) mass spectrometry with channel electron multiplier (CEM) detectors. Angular measurements are derived using five polar pixels coplanar with the spacecraft spin axis, and up to 16 azimuthal bins are acquired for each polar pixel over time as the spacecraft spins. Ion and electron measurements are acquired on alternate spacecraft spins. HOPE incorporates several new methods to minimize and monitor the background induced by penetrating particles in the harsh environment of the radiation belts. The absolute efficiencies of detection are continuously monitored, enabling precise, quantitative measurements of electron and ion fluxes and ion species abundances throughout the mission. We describe the engineering approaches for plasma measurements in the radiation belts and present summaries of HOPE measurement strategy and performance. 相似文献
959.
Gale Paulsen Kris Zacny Christopher B. Dreyer Attila Szucs Matt Szczesiak Chris Santoro Jack Craft Magnus Hedlund John Skok 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
We have developed a rock grinding and polishing mechanism for in situ planetary exploration based on abrasive disks, called Grinding Rocks Into Thin Sections (GRITS). Performance characteristics and design considerations of GRITS are presented. GRITS was developed as part of a broader effort to develop an in situ automated rock thin section (ISARTS) instrument. The objective of IS-ARTS was to develop an instrument capable of producing petrographic rock thin sections on a planetary science spacecraft. GRITS may also be useful to other planetary science missions with in situ instruments in which rock surface preparation are necessary. 相似文献
960.
Steven A. Walker Lawrence W. Townsend John W. Norbury 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Estimates of organ dose equivalents for the skin, eye lens, blood forming organs, central nervous system, and heart of female astronauts from exposures to the 1977 solar minimum galactic cosmic radiation spectrum for various shielding geometries involving simple spheres and locations within the Space Transportation System (space shuttle) and the International Space Station (ISS) are made using the HZETRN 2010 space radiation transport code. The dose equivalent contributions are broken down by charge groups in order to better understand the sources of the exposures to these organs. For thin shields, contributions from ions heavier than alpha particles comprise at least half of the organ dose equivalent. For thick shields, such as the ISS locations, heavy ions contribute less than 30% and in some cases less than 10% of the organ dose equivalent. Secondary neutron production contributions in thick shields also tend to be as large, or larger, than the heavy ion contributions to the organ dose equivalents. 相似文献