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941.
G. Boscheri M. Kacira L. Patterson G. Giacomelli P. Sadler R. Furfaro C. Lobascio M. Lamantea L. Grizzaffi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Models are required to accurately predict mass and energy balances in a bioregenerative life support system. A modified energy cascade model was used to predict outputs of a multi-crop (tomatoes, potatoes, lettuce and strawberries) Lunar greenhouse prototype. The model performance was evaluated against measured data obtained from several system closure experiments. The model predictions corresponded well to those obtained from experimental measurements for the overall system closure test period (five months), especially for biomass produced (0.7% underestimated), water consumption (0.3% overestimated) and condensate production (0.5% overestimated). However, the model was less accurate when the results were compared with data obtained from a shorter experimental time period, with 31%, 48% and 51% error for biomass uptake, water consumption, and condensate production, respectively, which were obtained under more complex crop production patterns (e.g. tall tomato plants covering part of the lettuce production zones). These results, together with a model sensitivity analysis highlighted the necessity of periodic characterization of the environmental parameters (e.g. light levels, air leakage) in the Lunar greenhouse. 相似文献
942.
为了提高短距离定位精度,消除采用平行入射假定所引入的计算误差,分析和研究了近似误差对角度估计和解相位模糊的影响;得出了满足平行入射近似的前提条件,为干涉仪的波长、基线长度等参数设计提供了指导依据;提出了实际入射角的相位差估计和相应的角度计算方法,提高了角度估计精度。文章提出的高精度相位干涉仪测角方法,适用于多个运动平台(如卫星、飞行器)的互相定位、航天器交会对接、地面短距离目标定位等测角精度要求高的工程应用。 相似文献
943.
Soybean cultivar selection for Bioregenerative Life Support Systems (BLSSs) – Hydroponic cultivation
R. Paradiso R. Buonomo V. De Micco G. Aronne M. Palermo G. Barbieri S. De Pascale 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Four soybean cultivars (‘Atlantic’, ‘Cresir’, ‘Pr91m10’ and ‘Regir’), selected through a theoretical procedure as suitable for cultivation in BLSS, were evaluated in terms of growth and production. Germination percentage and Mean Germination Time (MGT) were measured. Plants were cultivated in a growth chamber equipped with a recirculating hydroponic system (Nutrient Film Technique). Cultivation was performed under controlled environmental conditions (12 h photoperiod, light intensity 350 μmol m−2 s−1, temperature regime 26/20 °C light/dark, relative humidity 65–75%). Fertigation was performed with a standard Hoagland solution, modified for soybean specific requirements, and EC and pH were kept at 2.0 dS m−1 and 5.5 respectively. 相似文献
944.
945.
非对称喷管超声速流场的PIV实验与数值模拟 总被引:1,自引:1,他引:0
选取了跟随性能以及散射性能都上佳的二氧化钛粒子,利用了粒子图像测速仪(particle image velocimetry,PIV)对不同落压比下的非对称喷管(single expansion ramp nozzle,SERN)流场进行了测量,成功获取了相应流动结构,以及沿程上壁面压力分布和速度场等.在测得的图像中,可以清晰地观察到由于过膨胀产生的激波与膨胀波系,并进一步获得出口速度分布.运用计算流体动力学数值模拟方法,对实验状态下的非对称喷管进行了模拟.对比结果发现:PIV实验测得流场结构能很好地与其吻合,这互相验证了CFD计算和PIV实验的正确性及可靠性. 相似文献
946.
SPH方法对气液两相流自由界面运动的追踪模拟 总被引:2,自引:0,他引:2
气液两相流动是自然界中常见的流动现象,对其进行数值模拟时要求必须能够准确跟踪界面运动变形。本文利用光滑粒子流体动力学方法,结合微可压缩模型(SCM),引入界面控制方法XSPH速度修正以及Van Derwaals状态方程修正,对典型的气液两相流动如二维溃坝、气泡上浮等问题进行了数值模拟,分析了空气和水相互作用机理以及界面运动规律,并同实验结果和其他数值计算结果进行了比较。结果表明,该方法在模拟多相介质界面运动问题准确有效,可用于处理更为复杂的多相流动工程问题。 相似文献
947.
948.
基于气动热力模型的FADEC系统FHA方法 总被引:1,自引:1,他引:0
从适航规章对全权限数字发动机控制(full authority digital engine control,简称FADEC)系统的安全要求出发,结合功能危险分析(functional hazard assessment,简称FHA)的一般原则和FADEC系统的特点,得到了FADEC系统FHA的分析要素.根据分析要素中的工具与数据需求,将航空发动机气动热力模型用于可调放气活门(variable bleed valve,简称VBV)控制功能失效危险分析,结果表明:①该模型能够辅助确定FADEC系统功能失效的发动机影响;②FADEC系统功能危险的模型分析方法通过定量分析确定发动机影响的危险等级,为FHA提供直观的参考依据,可作为对专家经验的补充. 相似文献
949.
J. Klokočník A. Bezděk J. Kostelecký 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Small changes in semimajor axis of the orbits selected for the GNSS-R [R as Reflectometry] satellites, so-called fine orbit tuning, known from the ESA’s Gravity and steady-state Ocean Circulation Explorer mission, can dramatically increase the number of nadir and off-nadir reflecting points and, in turn, can enhance the capability of the concept of bistatic altimetry (GNSS Reflectometry) without additional costs. The application of our suggestion is feasible for a satellite which will be equipped by thrusters for the orbit keeping. During the mission lifetime several orbit tunings are feasible, just to transfer from one to another orbit. Then we can study short-periodic or longer-periodic features, according to scientific goals defined for the mission. The shortest cycles (few days), corresponding to the required revisit time (defined by ESA), may be subcycles of much longer cycles (repeat periods). 相似文献
950.
Bérangère Farges David Duchez Claude-Gilles Dussap Jean-François Cornet 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
In microgravity, one of the major challenge encountered in biological life support systems (BLSS) is the gas–liquid transfer with, for instance, the necessity to provide CO2 (carbon source, pH control) and to recover the evolved O2 in photobioreactors used as atmosphere bioregenerative systems. 相似文献