{"id":1503,"date":"2016-08-03T14:12:52","date_gmt":"2016-08-03T14:12:52","guid":{"rendered":"http:\/\/www.inspirenignite.com\/jntuk\/?p=1503"},"modified":"2016-08-03T14:12:52","modified_gmt":"2016-08-03T14:12:52","slug":"jntuk-b-tech-space-mechanics-for-r13-batch","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/jntuk\/jntuk-b-tech-space-mechanics-for-r13-batch\/","title":{"rendered":"JNTUK B. Tech Space Mechanics for R13 Batch."},"content":{"rendered":"<p>JNTUK B.Tech Space Mechanics gives you detail information of Space Mechanics R13 syllabus It will be help full to understand you complete curriculum of the year.<\/p><div class=\"a9916ad81d5189659b0bfae0b37c143c\" data-index=\"1\" style=\"float: none; margin:10px 0 10px 0; text-align:center;\">\n<ins class=\"adsbygoogle\"\r\n     style=\"display:block; text-align:center;\"\r\n     data-ad-layout=\"in-article\"\r\n     data-ad-format=\"fluid\"\r\n     data-ad-client=\"ca-pub-1181153414625576\"\r\n     data-ad-slot=\"9648548092\"><\/ins>\r\n<script>\r\n     (adsbygoogle = window.adsbygoogle || []).push({});\r\n<\/script>\n<\/div>\n\n<p><strong>Course Objective<\/strong><\/p>\n<p>This course is designed with an objective to provide a comprehensive overview of spaceflight mechanics, including both orbit and attitude dynamics. The two-body problem will be solved from first principles to allow the solution of the two-body position-time problem. This analysis will then be used to investigate various modes of orbit transfer. Attitude stabilization will be investigated for both spin- and 3-axis stabilized spacecraft. Finally, the various elements of the class will be brought together to illustrate the mission analysis and design process.<\/p>\n<p><strong>UNIT-I : Basic Concepts:<\/strong>The solar system-Reference frames and coordinate systems-The celestial sphere- The ecliptic-Motion of vernal equinox-Sidereal time-Solar Time-Standard Time-The earths atmosphere<br \/>\n<strong>The General N-Body Problem:<\/strong> The many body problem-Lagrange-Jacobi identity-The circular restricted three- body problem-Libration points- Relative Motion in the N-body problem.<\/p>\n<p><strong>UNIT-II : The Two-Body Problem:<\/strong> Equations of motion-General characteristics of motion for different orbits-Relations between position and time for different orbits-Expansions in elliptic motion-Orbital Elements-Relation between orbital elements and position and velocity.<\/p>\n<p><strong>UNIT-III : The Launching Of A Satellite:<\/strong> Launch vehicle ascent trajectories-General aspects of satellite injection-Dependence of orbital parameters on in-plane injection parameters-Launch vehicle performances- Orbit deviations due to injection errors<\/p>\n<p><strong>UNIT-IV : Perturbed Satellite Orbits:<\/strong> Special and general perturbations- Cowell\u2019s Method-Encke\u2019s method-Method of variations of orbital elements- General perturbations approach<\/p>\n<p><strong>UNIT-V : Interplanetary Trajectories:\u00a0<\/strong>Two-dimensional interplanetary trajectories-Fast interplanetary trajectories-Three-dimensional interplanetary trajectories- Launch of interplanetary spacecraft-Trajectory about the target planet<\/p>\n<p><strong>UNIT-VI : Ballistic Missile Trajectories:<\/strong> The boost phase-The ballistic phase-Trajectory geometry-Optimal flights-Time of flight-Re-entry phase-The position of the impact point-Influence coefficients.<\/p>\n<p><strong>Low-Thrust Trajectories :<\/strong> Equations of Motion-Constant radial thrust acceleration-Constant tangential thrust (Characteristics of the motion, Linearization of the equations of motion- Performance analysis.<\/p>\n<p><strong>TEXT BOOKS<\/strong><\/p>\n<ul>\n<li>\u201dRocket Propulsion and Spaceflight Dynamics\u201d, J.W.Cornelisse, H.F.R. Schoyer, and K.F. Wakker, Pitman, 1979<\/li>\n<li>\u201dSpaceflight Dynamics\u201d, William E.Wiesel, McGraw-Hill, 1997<\/li>\n<\/ul>\n<p>REFERENCE BOOKS<\/p>\n<ul>\n<li>Spacecraft Mission Design\u201d, Charles D.Brown, AIAA Education Series, Published by AIAA, 1998<\/li>\n<li>\u201cOrbital Mechanics\u201d, Vladimir A. Chobotov, AIAA Education Series, AIAA Education Series, Published by AIAA, 2002<\/li>\n<li>\u201dFundamentals of Astrodynamics and Applications\u201d, David.A. Vellado, Microcosm and Kluwer, 2001<\/li>\n<\/ul>\n<p><strong>Course Outcomes<\/strong><br \/>\nUpon completion of the module the student is expected to be able to<\/p>\n<ul>\n<li>An understanding of the methods employed in spaceflight mechanics.<\/li>\n<li>The ability to solve the two-body problem and two-body orbit transfer problems.<\/li>\n<li>The ability to analyse the dynamics and control of spin- and 3-axis stabilised spacecraft.<\/li>\n<li>An appreciation of the importance of spaceflight mechanics in space systems engineering.<\/li>\n<\/ul>\n<p>For more information about all JNTU updates please stay connected to us on FB and don\u2019t hesitate to ask any questions in the comment.<\/p>\n<div class=\"a9916ad81d5189659b0bfae0b37c143c\" data-index=\"2\" style=\"float: none; margin:10px 0 10px 0; text-align:center;\">\n<ins class=\"adsbygoogle\"\r\n     style=\"display:block; text-align:center;\"\r\n     data-ad-layout=\"in-article\"\r\n     data-ad-format=\"fluid\"\r\n     data-ad-client=\"ca-pub-1181153414625576\"\r\n     data-ad-slot=\"8060844699\"><\/ins>\r\n<script>\r\n     (adsbygoogle = window.adsbygoogle || []).push({});\r\n<\/script>\n<\/div>\n\n<div style=\"font-size: 0px; height: 0px; line-height: 0px; margin: 0; padding: 0; clear: both;\"><\/div>","protected":false},"excerpt":{"rendered":"<p>JNTUK B.Tech Space Mechanics gives you detail information of Space Mechanics R13 syllabus It will be help full to understand you complete curriculum of the year. Course Objective This course [&hellip;]<\/p>\n","protected":false},"author":2259,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"_bbp_topic_count":0,"_bbp_reply_count":0,"_bbp_total_topic_count":0,"_bbp_total_reply_count":0,"_bbp_voice_count":0,"_bbp_anonymous_reply_count":0,"_bbp_topic_count_hidden":0,"_bbp_reply_count_hidden":0,"_bbp_forum_subforum_count":0,"footnotes":""},"categories":[2],"tags":[],"class_list":["post-1503","post","type-post","status-publish","format-standard","hentry","category-syllabus"],"_links":{"self":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts\/1503","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/users\/2259"}],"replies":[{"embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/comments?post=1503"}],"version-history":[{"count":1,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts\/1503\/revisions"}],"predecessor-version":[{"id":1504,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/posts\/1503\/revisions\/1504"}],"wp:attachment":[{"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/media?parent=1503"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/categories?post=1503"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.inspirenignite.com\/jntuk\/wp-json\/wp\/v2\/tags?post=1503"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}