<datastore> <nextgroup><![CDATA[<a href="/module/jslib/jquery/jpage/dataproxy.jsp?page=1&appid=1&appid=1&webid=2&path='/'&columnid=1350&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_1350_22257.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research Progress of Novel Lightweight Thermal Protection Composites</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 ： According to the requirements on novel lightweight aerospace composites in the field of deep space exploration，this paper summarized the latest research progress of thermal protection aerospace composites at home and abroad.</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_1350_22258.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Conceptual Design of Human-Robot System for On-orbit Service of 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: In the field of manned spaceflight, astronauts and space robot have formed a complementary relationship. Astronauts, robot and environment are interrelated, inter-restricted and interacted with each other. Human-robot system aims at solving the problem of robot operation and human-robot interaction, according to the environment of the robot and 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_1350_22259.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Conceptual Study of System Schemes of Manned Asteroid Exploration Spacecraft</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 ： On the basis of the mission mode of human asteroid exploration, the manned asteroid exploration spacecraft was designed, which was comprised of a crew module, a landing module, a reentry module and a propulsion module. The functions and main parameters of these modules in asteroid exploration were described.</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_1350_22260.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Ascent Assist Capability of Crew Launch Tower Escape System</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: In a normal flight of a manned launch vehicle，the escape system is not activated and is abandoned at a predetermined time，which results in a waste of escape fuel. To improve the utilization rate of the escape fuel，the escape system could be started at the end of its responsible time interval to provide extra thrust for the manned launch vehicle.</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_1350_22261.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on Buckling Load Analysis and Test of Solar Array Deployable Mechanism in 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 ： Buckling load analysis of deployable mechanism was a key factor in the stability design of large flexible solar array in space station. Three span coiled deployable mechanism with tension served as the object of study.</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_1350_22262.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">The Effect of Duplex Annealing on Microstructure and Mechanical Properties of Laser Deposited Ti60A ...</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 ： In this paper, laser deposited Ti60A alloy was annealed in the upper ( a + p) region at different temperatures, followed by low temperature annealing, “Tβ-30”( 1020℃/1h/AC + 700℃/ 2h/AC) and “Tβ-10”( 1040℃/1h/AC +700℃/2h/AC) heat treatments.</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_1350_22263.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Flame Retardants Study of Expandable Graphite in Semi-rigid Polyurethane Foams</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： Semi-rigid polyurethane foam (SPF) has a wide range of potential applications due to its outstanding cushioning performance. However，SPF is highly flammable owing to its low density and open-cell structure， which limits its greater use in many fields， especially in the aerospace and other special areas.</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_1350_22264.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Relative Positioning Based on Kinematic Method Using Single Difference GPS Observations</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 background of this paper is the formation flying of two satellites in the mode of two spacecraft equipped with dual-frequency receivers and in the mode of one spacecraft with dual-frequency receiver and the other with single-frequency receiver.</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_1350_22265.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Accelerated Life Test Research on Nickel-hydrogen Battery in Spacecraft</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 predict the cycle life of Ni-H2 batteries in spacecraft, the accelerated life test was conducted in 40Ah Ni-H= batteries under 40%, 60% and 80% DODs. Destructive physical analysis and performance test were then carried out after 1300 cycles.</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_1350_22266.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Electrical Performance Prediction of Space Station Lithium-Ion Batteries Base on Nerual Network</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: Predictions should be made for the electrical performance of Lithium-Ion batteries in the space station according to the changes of the tasks. A dynamic neural network model was established and the Lithium-Ion batteries charge and discharge cycles data were selected and categorized for the training, calibration and test of the open-loop and closed-loop dynamic neural network.</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_1350_22267.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Review of Fault Tolerant Techniques in COTS-based Devices in Space Station Environment</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 ： In the space station environment, the effect of total ionizing dose (TID) is usually not obvious. Therefore, the commercial off-the-shelf (COTS) devices may be used instead of the traditional anti-radiation ones as an effective method to decrease the cost.</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_1350_22268.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on the On-demand Service of Space Search in Space Station Stage</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: Aimed at the characteristics of space search in space station stage, the information system of the on-demand service of space search was studied. Firstly, the characteristics of space search and on-demand service of space search in space station stage were analyzed. Secondly, the on-demand service of space search based on the space-based information system and the infrastructure of the information system of the on-demand service of space search were established.</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>