Solution to problem of optimum thrust programming deduced for rocket which is required to reach given altitude with given pay load (rather than given burnt mass) and minimum fuel expenditure, i.e. effect of rocket deadweight is taken into account; in particular, case of rocket with disposable booster is considered and necessary conditions for minimum initial mass are found.
Stationary trajectories for high-altitude rocket with dropaway booster
Astronautica Acta
Astronautica Acta ; 2 , n 3
1956
6 pages
Article (Journal)
English
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