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by ateng
1585 days ago
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If you just model rocket science as a point mass with variable m then yes… But it’s more than that. To name a few:
* How does one raise the thrust temperature as high as possible without melting the engine to maximise thrust? (The burning temperature IS already higher than the engine material melting point)
* how does one reduce the redundancy (both system wise and material wise) to minimise weight while ensuring the rocket won’t fail? |
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