Conceptual Design of an Air- launched Multi-stage Launch Vehicle
In the present thesis, the objective was to find the maximum amount of payload mass that can be put into a 500 km polar orbit by a 1400 kg air-launched multi-stage rocket launched from a fighter jet platform. To fulfill the objective an algorithm incorporating several modules was developed. The modu...
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| Format: | Others |
| Language: | English |
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KTH, Fysik
2020
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-284355 |
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