Determination of trajectory of rocket with constant acceleration assuming radial thrust of motor and based on initial conditions; deduced differential equation represents generalization of Binet's equation; finite equations of trajectory are determined by means of elliptic integrals of first and second kind.
Considerations on rocket trajectories
Considerations sur la trajectoire des fusees
Revue de Mecanique Appliquee ; 6 , n 4
1961
13 pages
Aufsatz (Zeitschrift)
Französisch
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Engineering Index Backfile | 1950
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|Some optimum rocket trajectories
Engineering Index Backfile | 1961
|Some optimum rocket trajectories
Engineering Index Backfile | 1961
|