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Space Flight and Re-Entry Trajectories

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Cover of 'Space Flight and Re-Entry Trajectories'

Table of Contents

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    Book Overview
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    Chapter 1 Possible Paths for Re-Entry Into the Earth’s Gravitational Field Avoiding the Radiation Belts
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    Chapter 2 Aerodynamics of Trajectory Control for Re-Entry at Escape Speed
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    Chapter 3 L’étagement optimum des groupes de fusées en fonctionnement parallèle
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    Chapter 4 Aspects analytiques du problème des perturbations d’un satellite artificiel
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    Chapter 5 The Effect of Atmospheric Oblateness on a Satellite Orbit
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    Chapter 6 Problems and Potentialities of Space Rendezvous
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    Chapter 7 Interplanetary Trajectories for Electrically-Propelled Space Vehicles
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    Chapter 8 The Stability of the 24-Hour Satellite
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    Chapter 9 Practical Aspects of Re-Entry Problems
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    Chapter 10 A Generalized Study of Two-dimensional Trajectories of a Vehicle in Earth-Moon Space
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    Chapter 11 Optimal Intermediate-Thrust Arcs in a Gravitational Field
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    Chapter 12 Factors Affecting the Accuracy of Impact Position of Satellites Re-Entered by Command
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    Chapter 13 Etude théorique des trajectoires optimales dans un champ de gravitation. Application au cas d’un centre d’attraction unique
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    Chapter 14 Astrodynamics and Planetary Research
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    Chapter 15 On Guidance and Landing Accuracy Requirements in Re-Entry Trajectories
Attention for Chapter 9: Practical Aspects of Re-Entry Problems
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Summary
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Chapter title
Practical Aspects of Re-Entry Problems
Chapter number 9
Book title
Space Flight and Re-Entry Trajectories
Published by
Springer, Vienna, January 1962
DOI 10.1007/978-3-7091-5470-0_9
Book ISBNs
978-3-70-915472-4, 978-3-70-915470-0
Authors

Antonio Ferri, Lu Ting, Ferri, Antonio, Ting, Lu

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