STUDY OF MULTI-STAGE SATELLITE LAUNCH VEHICLE PROPULSION SPECIFICATIONS DETERMINATION BASED ON ASCENT PROBLEM
In this final project, a study of ascent problems in the conceptual design of satellite launch vehicle was done. The sub-problems studied were about the selection of trajectories and the selection of rocket propulsion. The reference trajectory is the optimal trajectory, which is the solution of opti...
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| 主要作者: | |
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| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/20839 |
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| 機構: | Institut Teknologi Bandung |
| 語言: | Indonesia |