Coplanar Air Launch With Gravity Turn Launch Trajectories
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Coplanar Air Launch With Gravity Turn Launch Trajectories
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Author : David W. Callaway
language : en
Publisher:
Release Date : 2004-03-01
Coplanar Air Launch With Gravity Turn Launch Trajectories written by David W. Callaway and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2004-03-01 with Rockets (Aeronautics) categories.
The purpose of this study was to determine the feasibility of launching a vehicle based on the Boeing AirLaunch System in a coplanar, direct to rendezvous trajectory with gravity-turn. The focus of the research was to model the launch trajectory and determine the ability to reach different coplanar orbits. The launch trajectory was modeled using two-dimensional equations of motion and a boundary value problem was posed and solved for the gravity-turn trajectory. Trajectories were then created in an attempt to reach different altitudes through coasting and transfer orbits. Finally a specific orbital altitude was chosen and the trajectories were analyzed to find the most efficient route to the target orbit for fuel and time.
Simulation Of Gravity Turn Trajectories For Two Stage Launch Vehicles
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Author : Steven Roy Walker
language : en
Publisher:
Release Date : 2006
Simulation Of Gravity Turn Trajectories For Two Stage Launch Vehicles written by Steven Roy Walker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2006 with Launch vehicles (Astronautics) categories.
A study of the design and validation of a software program for simulating gravity turn trajectories for two-stage launch vehicles.
Optimal Non Coplanar Launch To Quick Rendezvous
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Author : Gregory B. Sears
language : en
Publisher:
Release Date : 1997-12-01
Optimal Non Coplanar Launch To Quick Rendezvous written by Gregory B. Sears and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997-12-01 with Delta launch vehicles categories.
The purpose of this study was to determine the feasibility of launching a Delta Clipper-like vehicle on an optimal, non-coplanar trajectory to rendezvous with an earth orbiting object in one orbit or less. The focus of the research was to determine what such a trajectory would look like, and to determine the cost, in payload mass, of flying such a trajectory. A model for the ascent trajectory was developed using the dynamics equations of motion, an atmosphere model, and an aerodynamic model for the DC-Y concept vehicle. A boundary value problem was posed and solved for a coplanar rendezvous. The non- coplanar solutions were obtained through extrapolation from the coplanar solution.
Launch Vehicle Dynamics
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Author : Harry L. Runyan
language : en
Publisher:
Release Date : 1961
Launch Vehicle Dynamics written by Harry L. Runyan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Launch vehicles (Astronautics) categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1996
International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Aeronautics categories.
Orbital Mechanics For Engineering Students
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Author : Howard D Curtis
language : en
Publisher: Elsevier
Release Date : 2009-10-26
Orbital Mechanics For Engineering Students written by Howard D Curtis and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2009-10-26 with Technology & Engineering categories.
Orbital Mechanics for Engineering Students, Second Edition, provides an introduction to the basic concepts of space mechanics. These include vector kinematics in three dimensions; Newton’s laws of motion and gravitation; relative motion; the vector-based solution of the classical two-body problem; derivation of Kepler’s equations; orbits in three dimensions; preliminary orbit determination; and orbital maneuvers. The book also covers relative motion and the two-impulse rendezvous problem; interplanetary mission design using patched conics; rigid-body dynamics used to characterize the attitude of a space vehicle; satellite attitude dynamics; and the characteristics and design of multi-stage launch vehicles. Each chapter begins with an outline of key concepts and concludes with problems that are based on the material covered. This text is written for undergraduates who are studying orbital mechanics for the first time and have completed courses in physics, dynamics, and mathematics, including differential equations and applied linear algebra. Graduate students, researchers, and experienced practitioners will also find useful review materials in the book. NEW: Reorganized and improved discusions of coordinate systems, new discussion on perturbations and quarternions NEW: Increased coverage of attitude dynamics, including new Matlab algorithms and examples in chapter 10 New examples and homework problems
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1991
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Rocket And Spacecraft Propulsion
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Author : Martin J. L. Turner
language : en
Publisher: Springer Science & Business Media
Release Date : 2006-08-29
Rocket And Spacecraft Propulsion written by Martin J. L. Turner and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2006-08-29 with Technology & Engineering categories.
The revised edition of this practical, hands-on book discusses the launch vehicles in use today throughout the world, and includes the latest details on advanced systems being developed, such as electric and nuclear propulsion. The author covers the fundamentals, from the basic principles of rocket propulsion and vehicle dynamics through the theory and practice of liquid and solid propellant motors, to new and future developments. He provides a serious exposition of the principles and practice of rocket propulsion, from the point of view of the user who is not an engineering specialist.
Planetary Flight Handbook
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Author :
language : en
Publisher:
Release Date : 1963
Planetary Flight Handbook written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Astronautics categories.
Fundamentals Of Astrodynamics
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Author : Roger R. Bate
language : en
Publisher: Courier Corporation
Release Date : 1971-01-01
Fundamentals Of Astrodynamics written by Roger R. Bate and has been published by Courier Corporation this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971-01-01 with Technology & Engineering categories.
Teaching text developed by U.S. Air Force Academy and designed as a first course emphasizes the universal variable formulation. Develops the basic two-body and n-body equations of motion; orbit determination; classical orbital elements, coordinate transformations; differential correction; more. Includes specialized applications to lunar and interplanetary flight, example problems, exercises. 1971 edition.