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[null,"1.","Record Nr.",null,"UNINA9910457249903321"]
[null,null,"Titolo",null,"Celestial mechanics and astrodynamics [[electronic resource] /] / edited by Victor G. Szebehely"]
[null,null,"Pubbl/distr/stampa",null,"New York, : Academic Press, 1964"]
[null,null,"ISBN",null,"1-60086-488-0"]
[{"$nulls":4},"1-60086-269-1"]
[null,null,"Descrizione fisica",null,"1 online resource (765 p.)"]
[null,null,"Collana",null,"Progress in astronautics and aeronautics ; ; v. 14"]
[null,null,"Disciplina",null,"521.1"]
[null,null,"Soggetti",null,"Astronautics"]
[{"$nulls":4},"Artificial satellites - Orbits"]
[{"$nulls":4},"Electronic books."]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","\"A selection of technical papers based mainly on the American Institute of Aeronautics and Astronautics Astrodynamics Conference held at New Haven, Connecticut, August 19-21, 1963.\""]
[null,null,null,"Nota di bibliografia","Includes bibliographical references and index."]
[null,null,"Nota di contenuto",null,"\"\"Cover\"\"; \"\"Title\"\"; \"\"Copyright\"\"; \"\"The ARS Astrodynamics Committee 1962\"\"; \"\"The AIAA Astrodynamics Committee 1963\"\"; \"\"The Astrodynamics Conference Committee 1963\"\"; \"\"Preface\"\"; \"\"Astrodynamics in the AIAA\"\"; \"\"Contents\"\"; \"\"I. Orbit Prediction and General Perturbations\"\"; \"\"Numerical Aspects of Uniformly Valid Asymptotic Approximations for a Class of Trajectories in the Restricted Three-Body Problem\"\"; \"\"A Group of Earth-to-Moon Trajectories with Consecutive Collisions\"\"; \"\"Two Fixed Center Approximations to the Restricted Problem\"\""]
[{"$nulls":4},"\"\"A High-Order Perturbation Theory Using Rectangular Coordinates\"\"\"\"Trajectories of Satellites under the Influence of Air Drag\"\"; \"\"II. Astronomical Constants and Physical Properties\"\"; \"\"System of Astronomical Constants\"\"; \"\"The Evaluation of Certain Astronomical Constants from the Radio Tracking of Mariner II\"\"; \"\"Atmospheric Density Determination from Satellite Observations\"\"; \"\"III. Orbit Selection\"\"; \"\"Probabilistic Evaluation of Satellite Missions Involving Ground Coverage\"\"; \"\"Orbital Aspects of Nonsynchronous Communication Satellite Systems\"\""]
[{"$nulls":4},"\"\"Guidance of Unmanned Lunar and Interplanetary Spacecraft\"\"\"\"An Approximate Method for Computing Error Coefficient Matrices for Lunar Trajectories\"\"; \"\"Minimum Lunar Orbit Inclination to Lunar Equatorial Plane for Earth-Launched Vehicle\"\"; \"\"General Characteristics "]
[{"$nulls":4},"of the Launch Window for Orbital Launch to the Moon\"\"; \"\"Launch Windows for Highly Eccentric Orbits\"\"; \"\"Moon-to-Earth Trajectories\"\"; \"\"An Analysis of Free Return Circumlunar Trajectories\"\"; \"\"Free Return Circumlunar Trajectories from Launch Windows with Fixed Launch Azimuths\"\""]
[{"$nulls":4},"\"\"IV. Orbit Mechanics of the Ranger and Mariner Missions\"\"\"\"Trajectory Design for Ranger and Mariner Missions\"\"; \"\"Boost Vehicle Trajectories for Ranger and Mariner Programs\"\"; \"\"Launch-to-Mission Completion Targeting for Ranger and Mariner Missions\"\"; \"\"V. Orbit Transfer and Trajectory Optimization\"\"; \"\"A Trajectory Optimization Technique Based upon the Theory of the Second Variation\"\"; \"\"Minimum Impulse Transfer\"\"; \"\"On Some Single-Impulse Transfer Problems\"\"; \"\"Analysis of the Orbital Transfer Problem in Three-Dimensional Space\"\"; \"\"VI. Orbit Determination\"\""]
[{"$nulls":4},"\"\"Position and Velocity Estimates by Trajectory Rectification\"\"\"\"Self-Contained Orbit Determination Techniques\"\"; \"\"Linearized Drag Analysis and Orbit Determination\"\"; \"\"Orbit Determination in the Presence of Systematic Errors\"\"; \"\"Contributors to Volume 14\"\""]