Methods for determining optimum stage-weight distribution and ascending trajectory of multistage rockets have individually been described; these two problems are inherently inseparable and are not independent of each other; unified numerical method integrating these two optimization problems for satellite laucching vehicles is explained; also, numerical examples concerning finding of optimum vehicle to place 150 kg weight satellite into circular orbit at height of 1000 km are given. (In Japanese with English abstract) (Rec'd 1968)
Optimization of staging and trajectory for satellite launching vehicles
Mitsubishi Heavy Industries, Ltd -- Tech Bul
1966
18 pages
Report
Japanisch
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Method of weight prediction of satellite launching vehicles
Engineering Index Backfile | 1967
|Online Contents | 1995