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281.
A quartz sensor of small accelerations with a capacitive transducer is designed and produced, allowing one to measure spacecraft accelerations with a resolution of 10–7 m/s2 in the range ±10–1 m/s2. The results of calibration of the sensor by the method of inclinations are presented.  相似文献   
282.
王程 《中国航天》2005,(8):10-12
气象卫星是对地球及其大气层进行气象观测的遥感卫星。气象卫星按轨道不同,分为太阳同步轨道气象卫星和地球静止轨道气象卫星。太阳同步轨道卫星可以获得全球气象信息,如我国的风云(FY)1号气象卫星:地球静止轨道气象卫星可以对目标区域进行连续气象观测,如我国的风云2号气象卫星。两种类型的气象卫星相互补充、协同观测。目前除中国外,美国、俄罗斯、欧洲、日本和印度都先后发射了气象卫星。  相似文献   
283.
Layers of dormant endospores of Bacillus subtilis HA101 were applied to eight different spacecraft materials and exposed to martian conditions of low pressure (8.5 mbar), low temperature (-10 degrees C), and high CO(2) gas composition and irradiated with a Mars-normal ultraviolet (UV-visible- near-infrared spectrum. Bacterial layers were exposed to either 1 min or 1 h of Mars-normal UV irradiation, which simulated clear-sky conditions on equatorial Mars (0.1 tau). When exposed to 1 min of Mars UV irradiation, the numbers of viable endospores of B. subtilis were reduced three to four orders of magnitude for two brands of aluminum (Al), stainless steel, chemfilm-treated Al, clear-anodized Al, and black-anodized Al coupons. In contrast, bacterial survival was reduced only one to two orders of magnitude for endospores on the non-metal materials astroquartz and graphite composite when bacterial endospores were exposed to 1 min of Mars UV irradiation. When bacterial monolayers were exposed to 1 h of Mars UV irradiation, no viable bacteria were recovered from the six metal coupons listed above. In contrast, bacterial survival was reduced only two to three orders of magnitude for spore layers on astroquartz and graphite composite exposed to 1 h of Mars UV irradiation. Scanning electron microscopy images of the bacterial monolayers on all eight spacecraft materials revealed that endospores of B. subtilis formed large aggregates of multilayered spores on astroquartz and graphite composite, but not on the other six spacecraft materials. It is likely that the formation of multilayered aggregates of endospores on astroquartz and graphite composite is responsible for the enhanced survival of bacterial cells on these materials.  相似文献   
284.
Anselmo  L.  Pardini  C. 《Space Debris》2000,2(2):67-82
The short- and long-term effects of spacecraft explosions, as a function of the end-of-life re-orbit altitude above the geostationary orbit (GEO), were analyzed in terms of their additional contribution to the debris flux in the GEO ring. The simulated debris clouds were propagated for 72yrs, taking into account all the relevant orbital perturbations.The results obtained show that 6–7 additional explosions in GEO would be sufficient, in the long term, to double the current collision risk with sizable objects in GEO. Unfortunately, even if spacecraft were to re-orbit between 300 and 500km above GEO, this would not significantly improve the situation. In fact, an altitude increase of at least 2000km would have to be adopted to reduce by one order of magnitude the long-term risk of collision among geostationary satellites and explosion fragments. The optimal debris mitigation strategy should be a compromise between the reliability and effectiveness of spacecraft end-of-life passivation, the re-orbit altitude and the acceptable debris background in the GEO ring. However, for as long as the re-orbit altitudes currently used are less than 500km above GEO, new spacecraft explosions must be avoided in order to preserve the geostationary environment over the long term.  相似文献   
285.
运动的破缺产生差异,导致涨落,造成对系统原有方向、轨道的偏离,致使事物发展与进化,由此带来一系列富有生机和活力的启示。作为系统内在机制的协同与竞争,也深深地楔人了我们的生活。  相似文献   
286.
K. Sweet 《Space Policy》1999,15(4):223-231
The Earth has been hit by NEOs many times in its history and there is always a risk that this will happen again. While we are beginning to acquire the technology that could warn of and divert a future collision, the legal instruments needed to facilitate a global response to the problem are lacking, especially given that the most likely means of diverting a NEO would involve nuclear weapons that could also be used on Earth. An analysis of the current legal situation is used to support the argument that new rules must be created. The author also discusses US Air Force policy on the subject and whether planetary defense is consistent with its goal of achieving and sustaining US superiority in space.  相似文献   
287.
In 1994–1995 Lavochkin Association (Russia) together with the other enterprises in accordance with technical requirements of the Russian Space agency, developed a new Russian communication satellite of a small class that will operate in both the geostationary (GSO) and high-elliptical (HEO) orbits. This satellite may be injected into operational orbits using a SOYUZ-2 launch vehicle (LV) and a FREGAT upper stage (US) from Plesetsk and Baykonur space launch sites (SLS).The main reason for creating such a satellite was to decrease the cost of the support and development of the Russian communication geostationary satellites group.Russian satellites Horizont, Express, Ekran and Gals, which operate in GSO, are the basis of the space segment for communications, radio and TV broadcasting. All of these satellites are injected into GSO by the PROTON LV. PROTON is a launch vehicle of a heavy class. The use of a middle class LV instead of a heavy class will allow to reduce considerably the launch cost. The change of a heavy class LV to a LV of middle class determined one economic reason for this project. Besides, the opportunity to launch S/C into GSO from Russian Plesetsk SLS increases the independence of Russia in the domain of space communications, despite the presence of the contract with Kazachstan about the rent of Baykonur SLS. Finally, use of small satellites with a rather small number of transponders is more effective than the use of big satellites. It will allow also to increase a satellite group (by the launch of additional satellites) precisely in accordance to the development of the ground segment.  相似文献   
288.
雷达与ESM相关算法综述   总被引:5,自引:0,他引:5  
在比较雷达和ESM(ElectronicSupportMeasurements)这两种传感器特点的基础上,分析了雷达与ESM相关的特点,介绍了统计方法、模糊方法和优化方法等五种雷达与ESH相关算法,并对这些算法进行了评述。  相似文献   
289.
GPCM控制气动伺服系统的理论分析与实验研究   总被引:3,自引:0,他引:3  
广义脉冲编码调制(GPCM)控制是针对脉冲编码调制(PCM)控制气动系统中控制精度与控制范围、稳定性与快速性之间的矛盾而提出的。本文建立了GPCM控制气动伺服系统的数学模型,并进行了详细的仿真和实验研究,结果证明了该方法的有效性。  相似文献   
290.
充液飞行器大角度操纵变结构控制   总被引:2,自引:1,他引:2  
  相似文献   
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