Résumé
L’étude porte sur les trajectoires de retour s’étendant depuis une orbite initiale quelconque jusqu’éu sommet de l’atmosphére. La phase propulsive est réduite à une impulsion; les trajectoires étudiées se trouvent dans le plan de l’orbite initiale; la Terre, fixe et sphérique, est le seul centre d’attraction.
Абстрактный
Требования, предъявляемы е к точност и трактори й возвращАнализируютс я траектори и возврата, начина я с данно й начаорбит ы и до верхни х слое в атмосферы. Двигател ь работае тпульсно м режиме. Рассмотренны е траектори и лежа т в’плоскосначально й орбиты. Сферическа я невращающаяс я Земл я являетединственны м центро м притяжения.
Abstract
Accuracy Requirements for Recovery Trajectories. Recovery trajectories, extending from a given initial orbit to the top of the atmosphere, are analyzed. The propulsion is reduced to an impulse; the trajectories considered lie in the plane of the initial orbit; the spherical non-rotat-ing earth is the only center of attraction.
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Références
Chapman, D. R., “An approximate method for studying entry into planetary atmosphere,” NASA TR R-11 (1959).
Chapman, D. R., “An analysis of the corridor and guidance requirements for supercircular entry into planetary atmospheres,” NASA TR R-55 (1960).
Lees, L., Hartwig, F. N., and Cohen, C. B., “The use of aerodynamic lift during entry into the earth’s atmosphere, ” ARS J. (Septem - ber 1959 ).
Allen, H. J., “Hypersonic aerodynamic problems of the future,” pre–sented to the Fluid Dynamics Panel of AGARD, Brussels, April 3–6, 1962.
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© 1964 Springer-Verlag Wien
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Moulin, L. (1964). Precisions Requises Pour Les Trajectoires de Retour D’engins Spatiaux. In: Boneff, N., Hersey, I. (eds) XIIIth International Astronautical Congress Varna 1962 / XIIIe Congrès International D’astronautique / XIII MeждyhapoдhbiЙ ҚohГpecc Пo ActpohabtИқe. Springer, Vienna. https://doi.org/10.1007/978-3-7091-4687-3_3
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DOI: https://doi.org/10.1007/978-3-7091-4687-3_3
Publisher Name: Springer, Vienna
Print ISBN: 978-3-7091-4541-8
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