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In the beginning of its use, missile is growth was from rocket that already optimized with technology that expanded at this time until become a weapon that applicable to defence need and security. At that moment speed, lethality has been limited and aparted its not so far. For that needed developmen...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/15353 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
| Summary: | In the beginning of its use, missile is growth was from rocket that already optimized with technology that expanded at this time until become a weapon that applicable to defence need and security. At that moment speed, lethality has been limited and aparted its not so far. For that needed developments to close over existing insuffiency at missile referred. Ramjet is one of usage solution propulsion rocket substitution to improve distance and speed missile. Relate to that then needed study hits design missile ramjet-powered. <br />
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At this final projects will give knowledge hits conceptual design and analysis missile ramjet-powered. This condition are expected become step early for development missile-powered furthermore ramjet. <br />
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This design is focus on aerodynamics analysis. Analysis is conducted by using steps that conducted by Fleeman and simulated uses ANSYS 11.0 ICEM CART 3D and some supportive analysises missile conceptual design. |
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