Technique of trajectory and stage propellant loading optimization for powered phase of multistage rocket carriers through atmosphere is presented; procedure is particularly suitable for large scale engineering analyses of vehicle trajectories and performance by means of digital computers; theoretical requirements and equations of motion are considered; basic computer program logic is described; technique is applied to hypothetical 2- and 3-stage vehicle in Saturn V class.
Technique for optimization of ascent trajectories and propellant loadings of multistage space vehicles
Raumfahrtforschung
Raumfahrtforschung ; 8 , n 3
1964
9 pages
Article (Journal)
English
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