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There is a lot of factors in satellite launch vehicle design which determined strongly successfulness of launch mission. The two of them are each stages rocket mass configuration and pitch program. An optimum rocket configuration will produce maximum ideal velocity. Pitch program determine maximum p...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/17108 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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