<datastore> <nextgroup><![CDATA[<a href="/module/jslib/jquery/jpage/dataproxy.jsp?page=1&appid=1&appid=1&webid=2&path='/'&columnid=1346&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/2015/10/8/art_1346_22202.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Progress of the Key Technologies in Human-Computer Interface in Space Teleoperation</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 improve the human performance of space teleoperation such as space station robotic arm operation task，it is an important technical method to improve the operators^ telepresence level. Therefore，ergonomic design of human-computer interface (HCI) should be carried out.</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/2015/10/8/art_1346_22201.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Changes of Contamination Deposition on Surface of Tiangong 1 Target 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 spacecraft surface and internal material can adsorb molecules and particles on the ground during material processing, and will quickly release them after entering into the vacuum space. The spacecraft will be contaminated by the deposition layer on its surface due to outgassing in the space environment.</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/2015/10/8/art_1346_22200.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Simulation Technique of Atomic Oxygen for Manned Spacecraft in Low Earth Orbit Space 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： Atomic oxygen( AO) is one of the most important environmental factors impacting spacecraft performance in LEO space environment. Materials used on the exterior of spacecraft can， in most cases，be eroded away through reaction with AO.</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/2015/10/8/art_1346_22199.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Growth of Rice Cells in Shenzhou 8 under Microgravity and Transcriptome Analysis</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: Culture system of rice cells under spatial microgravity conditions was successfully established in this study. Moreover，a real-time fixation of cultured cells was undertaken to get the RNA samples which reflected the gene expression pattern of rice cells under microgravity conditions.</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/2015/10/8/art_1346_22198.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Technical Summary and Conceptual Study of Propellant Cross Feed Technology</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 classification and concepts of propellant cross feed technology of liquid rocket was introduced in this paper. Commonly used foreign propellant cross feed technology solutions were compared ，and the technical advantages and applications were analyzed.</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/2015/10/8/art_1346_22197.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Review of Microbiological Control Technologies in Space and Development Proposals</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: Microbiological risk is a major concern in long-term manned missions， threatening the safety and health of astronauts and integrity of spacecrafts. Microbial contamination in manned spacecrafts may pollute the cabin environment，cause infection or sickness in crews，and induce biodegradation of critical materials which may result in system failure.</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/2015/10/8/art_1346_22196.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Thermal Comfort Assessment in Manned Spaceship Cabin</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: Based on flight data, thermal comfort of the airtight cabin in manned spaceship was assessed using PMV - PPD model. The effects of cabin temperature, humidity and wall temperature on thermal comfort were presented in detail.</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/2015/10/8/art_1346_22195.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Research on Impact Point Prediction Methods of CZ-2F Rocket Fairing Debris</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 realize the rapid searching the CZ-2F Rocket's fairing debris, an impact point prediction model based on the correction of high altitude wind was proposed after in-depth study of the debris' falling down rule and the distribution of the impact point.</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/2015/10/8/art_1346_22194.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Study on Biosafety Engineering Technology Architecture for Space Application Payload in Manned Space...</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 biohazard problem of scientific experiment payload in the space application system of the manned space project, a complete biosafety engineering architecture for space application science experiment payload in manned space project was 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/2015/10/8/art_1346_22193.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Skip Entry Corridor Design for Lunar Module Considering Multiple Constraints</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 lunar module with low lift-to-drag ratio, skip entry trajectory must be flown to achieve long downrange. In this paper, skip entry corridor was designed considering multi-constraints.</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/2015/10/8/art_1346_22192.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">Conceptual Study on Crew-Robot Coordinated Exploration on Lunar Surface</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: Crew-Robot coordinated exploration is not only the basis of manned lunar exploration, but also the precondition for designing mission modes and spacecraft systems of manned lunar exploration.</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/2015/10/8/art_1346_22191.html' target="_blank" style="line-height:20px;font-weight:bold; font-size: 15px; color:#015198;">The LOX/Kerosene Rocket Engine for Chinese New-generation 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 development status and the trend of foreign and Chinese manned launch vehicles main power system were analyzed，and the research history，system composition，working principle， performance parameters，key technology and application prediction of the engines were introduced.</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>