<datastore> <nextgroup><![CDATA[<a href="/module/jslib/jquery/jpage/dataproxy.jsp?page=1&appid=1&appid=1&webid=2&path='/'&columnid=1348&unitid=3691&webname='China Manned Space Engineering'&permissiontype=0"></a>]]></nextgroup> <recordset> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22222.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Advancement in Space Human Factors Engineering</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract ： Space Human Factors Engineering ( SHFE ) is the application of Human Factors Engineering (HFE) in the manned space field , which adheres to the philosophy of astronaut-centered design , focuses on the best match and systematic integration of human , machine and environment in manned space missions in order to ensure the safety , comfortability and performance of astronauts.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22223.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Unified Modeling and Calculation of Aerodynamics Characteristics during Low-Orbit Flying Control of ...</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract ： The surface analytical method，considering surface shielding effect of the complex structure and the modified Boettcher/Legge nonsymmetric bridge correction function， was proposed to computationally model aerodynamic characteristics of the large-scale Tiangong spacecraft of irregular plate-capsule assembly.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22224.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Application of Virtual Reality in Spatial Orientation Training for Space Station</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract： During manned spaceflight，weightless environment has great influence on astronauts spatial orientation ability，especially in the complicated configuration of space station，which often results in astronaut spatial disorientation.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22225.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on High Pressure Water Electrolysis with Proton Exchange Membrane</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: This paper outlined the development states of solid polymer electrolyte membrane water electrolysis technology. The influences of anode catalyst and membrane thickness, as well as the current density on electrode properties were examined. The properties and working stabilities of high pressure and high power water electrolysis stack were tested on high pressure water electrolysis testing system.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22226.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Inactivation of Microbe Contaminants via Corona Discharge Radical Shower</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: The control of microbe contaminants is an important part of the life support system during long term manned flight. DC corona discharge technique was adopted to inhibit the microbes grow rate and further inactivate it.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22227.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">The Virtual ARQ Mechanism for Satellite Communications</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract： With the development of manned space technology, more and more space flight missions require information transmission via satellite communication. The existing research results mainly use ARQ mechanism to decrease the data loss probability of satellite channel. However, the acknowledgment mechanism of ARQ will highly increase the transmission delay of satellite channel.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22228.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Feasibility Analysis for Space Station Attitude Measurement Based on BeiDou Navigation Satellite Sys...</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract： To investigate the technical feasibility of determining the attitude of space station using BeiDou Navigation Satellite System (BDS) , the authors first reviewed the constellation situation of the global BDS during the operation phase of the forthcoming Chinese Space Station, and presented the service ability of BDS for Chinese Space Station.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22229.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on High-Voltage Special DC/DC Converter Applied in Lunar Survey Radar</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: For the rigorous demand of DC/DC Converter that its over shoot should be within 1% and the problem of discharge to high voltage output in detectors at lunar environment， the output soft start up and multistep boost circuits were designed.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22230.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Safety Certification Technology for Space Utilization Payloads in Space Station Program</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract ： Aiming at safety requirements of the large-scale space utilization in China’s space station program, the definition and concept of on-board safety certification for space utilization payloads of space station were presented.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22231.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Architecture Design and Key Technology of Communication Network in Manned Launch Vehicle</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: The communication network in Manned Launch Vehicle was developed for long-range testing， launch and control of launch vehicle， in which hot-standby route and retransmission validation protocol were used to build the information interchange platform with high efficiency and high reliability.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22232.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on Site Selection of Manned Lunar Base</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract ： The site selection strategy of manned lunar base is a complex system selection process and many factors should be considered including the project mission objective，science objective，Engineering capacity constraints and resource utilization.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> <record><![CDATA[ <table width="705" height="110" border="0" cellspacing="0" cellpadding="8" style=" margin-bottom:10px;"> <tr> <td align="left" valign="top"><table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td height="40"> <a href='/art/2015/10/9/art_1348_22233.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Review of Force limiting Technique in Aerospace Products Vibration Tests</a></td> </tr> </table> <table width="100%" border="0" cellspacing="0" cellpadding="0"> <tr> <td valign="top"><span style="line-height:22px; font-size: 15px; color:#313131">Abstract: Among the ground vibration tests of space products， traditional acceleration control method generally result in overtesting especially in the low order resonance frequency of the test item. The force limiting uses a method of dual control of the acceleration and force input from the shaker， which can alleviates the overtesting problem by reduce the input acceleration real time.</span></td> </tr> </table></td> </tr></table><table width="100%" border="0" cellspacing="0" cellpadding="0" style=" margin-bottom:10px" height="0"> <tr> <td style="border-bottom: dotted 1px #cbcbcb;" ></td> </tr></table>]]></record> </recordset> </datastore>