Notice bibliographique
- Notice
Type(s) de contenu et mode(s) de consultation : Texte noté : électronique
Auteur(s) : Radiation Incorporated. Research Division
Titre(s) : Space trajectories [Texte électronique] : a symposium sponsored by the American Astronautical Society, the Advanced Research Projects Agency, and Radiation Incorporated / edited by the technical staff, Research Division, Radiation Incorporated, T.C. Helvey
Publication : New York : Academic Press, 1960
Description matérielle : 1 online resource (309 pages)
Note(s) : 3. Hypersonic Gasdynamic Problems of the Re-Entry Trajectories. - Includes bibliographical references. - REFERENCES FOR SECTION ON CLOSED-FORM ORBIT
DETERMINATION IN THE DISCOVERER PROGRAMChapter 7. Trajectory Computation in Systems
Design; Part I: General Discussion; Part II: Details of Computational Methods; REFERENCES;
Chapter 8. Computer Programs for Space Missions; Introduction; Simulation and Targeting
Programs; Satellite Tracking Methods; Summary; REFERENCES; Chapter 9. Space-Borne
Computer Design; Introduction; Computer Requirements; The Drum Memory; The Magnetic
Core Memory; Computer Organization; Computer Minimization; Targeting; Computer Check-Out;
Future Computers. - Print version record.
Autre(s) auteur(s) : Helvey, T. C.. Fonction indéterminée
American astronautical society. Fonction indéterminée
Sujet(s) : Trajectoires spatiales
Indice(s) Dewey :
629.435 (23e éd.) = Vols astronautiques d'exploration et de collecte de données
Identifiants, prix et caractéristiques : ISBN 9781483227368
Identifiant de la notice : ark:/12148/cb446670000
Notice n° :
FRBNF44667000
(notice reprise d'un réservoir extérieur)
Table des matières : Front Cover; Space Trajectories; Copyright Page; CONTRIBUTORS; PREFACE; Table of Contents;
Chapter 1. Military Space: Taking the High Ground; Review of Recent Accomplishments;
Comparison of Space Effort; Future Prospects; Future USSR Satellites; Direction of
Effort; ARPA; Conclusion; Chapter 2. Satellite and Probe Orbit Determination: Past,
Present, and Future; Chapter 3. General Survey of the Field; Introduction; Theoretical
Problems; The Computational Problem; Operational Problems; Contributions of Satellite
Observations; Conclusion; REFERENCE; DISCUSSION; Chapter 4. Astrodynamics.
Determination of the Physical Constants of the MoonConclusions; Effect of Uncertainties
on Lunar Trajectories; Recent Improvements in Constants; Solar Parallax; Planetary
Masses; Planetary Diameters and Flattening; Geocentric Constants; REFERENCES; Chapter
6. Trajectory Computation and Optimization; Introduction; Classical Methods of Orbital
Computation; Direct Numerical Integration; New Methods; DISCUSSION; ACKNOWLEDGMENTS;
REFERENCES ON TRAJECTORY COMPUTATION AND OPTIMIZATION; COMMENTS; REFERENCE; BREAKWELL:
CLOSED-FORM ORBIT DETERMINATION IN THE DISCOVERER PROGRAM.
Chapter 10. Space ManeuversIntroduction; Correctional Maneuvers; Terminal Maneuvers;
The Systems Problem; Propulsion Requirement Analysis; Other Approaches; Solar Sail
Concept; Satellite Rendezvous; Conclusion; REFERENCES; Chapter 11. Space Maneuvers:
Optimization; Optimal Transfer between Coplanar Ellipses; Transfer between Non-Coplanar
Orbits; Escape and Entry into Circular Orbits; Entry; Theory of Correctional Maneuvers;
REFERENCES; Chapter 12. Re-Entry Trajectories and Problems of Hypersonic Flow; Introduction;
1. Environment; 2. Trajectory Types as Related to Various Vehicles.
SECTION I IntroductionSECTION II Introduction to Astrodynamics; SECTION III Application
to Lunar Orbits; REFERENCES; Chapter 5. Trajectory Constants; Introduction; Heliocentric
Constants; The Solar Parallax and the Astronomical Unit; Methods for Determining the
Solar Parallax; Effect of the Uncertainty on Interplanetary Orbits; Universal Gravitational
Constant; Masses of the Planets; Diameter of the Planets; Flattening of α Planet;
Geocentric Constants; Determination of Constants; Effects of Uncertainties in Ke and
J on α Trajectory; Selenocentric Constants.
