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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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/20839 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |