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Old August 23rd 03, 05:36 PM
Ian Woollard
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Default inefficient turbo-pumps and Isp

Zoltan Szakaly wrote:

The optimum thrust to weight at takeoff for a rocket is around 1.5,


Actually no, it depends on the rocket, mainly on the staging scheme;
some rockets (especially two or more stage rockets) can optimise at
around 3g takeoff.

Zoltan