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Investigation Of Landing Point Control Of Re Entry Vehicles Utilizing Variable Area Aerodynamic Decelerators Incorporating Lift
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Book Synopsis Investigation of Landing Point Control of Re-entry Vehicles Utilizing Variable Area Aerodynamic Decelerators Incorporating Lift by : Avco-Everett Research Laboratory
Download or read book Investigation of Landing Point Control of Re-entry Vehicles Utilizing Variable Area Aerodynamic Decelerators Incorporating Lift written by Avco-Everett Research Laboratory and published by . This book was released on 1962 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Plasma Physics and Magnetohydrodynamics by :
Download or read book Plasma Physics and Magnetohydrodynamics written by and published by . This book was released on 1963 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Astronautics Information Abstracts by : Jet Propulsion Laboratory (U.S.)
Download or read book Astronautics Information Abstracts written by Jet Propulsion Laboratory (U.S.) and published by . This book was released on 1962 with total page 734 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Study of a Drag Brake Satellite Recovery System by :
Download or read book Study of a Drag Brake Satellite Recovery System written by and published by . This book was released on 1962 with total page 386 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of and Design Criteria for Deployable Aerodynamic Decelerators by : George Chernowitz
Download or read book Performance of and Design Criteria for Deployable Aerodynamic Decelerators written by George Chernowitz and published by . This book was released on 1964 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present state-of-the-art, technology, and theory applicable to deployable aerodynamic decelerators, especially textile parachute canopies, are presented. Major types of decelerators are described, and their aerodynamic and operational characteristics, as well as applications, are discussed. Detailed coverage is given to decelerator materials, design and construction, hardware, test methods and vehicles, and test instrumentation. Decelerator design procedures and performance prediction techniques are demonstrated by sample calculations.
Book Synopsis Investigation of Control-surface Instabilities on Lifting-body Reentry Vehicles at a Mach Number of 15.4 by : Robert Charles Goetz
Download or read book Investigation of Control-surface Instabilities on Lifting-body Reentry Vehicles at a Mach Number of 15.4 written by Robert Charles Goetz and published by . This book was released on 1971 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Use of Lift for Deceleration and Range Control for Re-entry of Space Vehicles by : Arthur J. Schwaniger
Download or read book Use of Lift for Deceleration and Range Control for Re-entry of Space Vehicles written by Arthur J. Schwaniger and published by . This book was released on 1960 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: This memorandum presents the results to date of a study of the problem of re-entry into the earth's atmosphere, by a vehicle returning from a space flight mission. Various re-entry conditions are studied using aerodynamic lift for deceleration and range control. Particular attention is given to cases where re-entry velocity is equal to escape velocity. The report shows that for non-lifting trajectories with re-entry velocity of 11,000 m/s (approximately escape velocity) only 0.4 degree variation in re-entry path angle is allowable if peak deceleration is to be held less than 10 g's. Range from re-entry to impact is shown to be variable up to 10,000 km for re-entry with escape velocity. (Author).
Book Synopsis A Flight Study of a Power-off Landing Technique Applicable to Re-entry Vehicles by : Richard S. Bray
Download or read book A Flight Study of a Power-off Landing Technique Applicable to Re-entry Vehicles written by Richard S. Bray and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of Retardation and Recovery Symposium by :
Download or read book Proceedings of Retardation and Recovery Symposium written by and published by . This book was released on 1963 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains the proceedings of the Retardation and Recovery Symposium sponsored by the Aeronautical Systems Division on 13 and 14 November 1962. The Introductory Session was opened with the Keynote Address which reviewed the use and applications of deployable aerodynamic decelerators throughout the past fifty (50) years and noted the areas in which additional work had to be accomplished. The four Technical Sessions deal with the latest significant developments in the retardation and recovery area. The Technical Sessions begin with presentations and discussions of investigations in the hypersonic and supersonic flight regimes followed by a technical analysis of transonic and supersonic flow phenomena. In addition, new aerodynamic decelerator designs and discussion of the wind tunnel tests pertaining to these designs, as well as overall reliability of recovery systems, are presented. The final Technical Session concludes with a discussion of the military, scientific, and general objectives for decelerators intended for future use.
Book Synopsis Investigation of the Landing Characteristics of a Reentry Vehicle Having a Canted Multiple-air-bag Load-alleviation System by : Sandy M. Stubbs
Download or read book Investigation of the Landing Characteristics of a Reentry Vehicle Having a Canted Multiple-air-bag Load-alleviation System written by Sandy M. Stubbs and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Variation and Control of Range Traveled in the Atmosphere by a High-drag Variable-lift Entry Vehicle by : Donald C. Cheatham
Download or read book The Variation and Control of Range Traveled in the Atmosphere by a High-drag Variable-lift Entry Vehicle written by Donald C. Cheatham and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Control-surface Instabilities on Lifting-body Reentry Vehicles at a Mach Number of 15.4 by : Robert C. Goetz
Download or read book Investigation of Control-surface Instabilities on Lifting-body Reentry Vehicles at a Mach Number of 15.4 written by Robert C. Goetz and published by . This book was released on 1971 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Landing Characteristics of a Reentry Vehicle Having a Canted Multiple-air-bag Load-alleviation System by : Sandy M. Stubbs
Download or read book Investigation of the Landing Characteristics of a Reentry Vehicle Having a Canted Multiple-air-bag Load-alleviation System written by Sandy M. Stubbs and published by . This book was released on 1963 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Optimal Lifting Re-Entry by Reduced-Order Approximation by : W. O'Dwyer
Download or read book Optimal Lifting Re-Entry by Reduced-Order Approximation written by W. O'Dwyer and published by . This book was released on 1973 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt: A faster method for computing optimal three dimensional trajectories that maximize the landing footprint of a lifting re-entry vehicle has been developed. The method uses energy approximations based on the assumption that the flight path angle is small and the flight path angular rate is zero. Thus, the vertical component of lift is considered equal to the weight minus centrifugal relief, and the equation of motion are reduced in order from six to four. Because of this simplification, the classical indirect method of the calculus of variations is used to compute families of optimal solutions. Using data corresponding to one of the space shuttle configurations, computations have been carried out for both unconstrained trajectories and for solutions that have aerodynamic heating rates and lift coefficients limited to specified values. During the investigation, several interesting analytical finds were uncovered that could be used as a basis for an onboard guidance scheme. (Author).
Book Synopsis Stability and Control Characteristics of a Low-lift-drag-ratio Reentry Vehicle at Mach Numbers from 2.30 to 4.65 by :
Download or read book Stability and Control Characteristics of a Low-lift-drag-ratio Reentry Vehicle at Mach Numbers from 2.30 to 4.65 written by and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721103898 Total Pages :114 pages Book Rating :4.1/5 (38 download)
Book Synopsis Reentry Vehicle Flight Controls Design Guidelines by : National Aeronautics and Space Administration (NASA)
Download or read book Reentry Vehicle Flight Controls Design Guidelines written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-13 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report addresses issues in developing a flight control design for vehicles operating across a broad flight regime and with highly nonlinear physical descriptions of motion. Specifically it addresses the need for reentry vehicles that could operate through reentry from space to controlled touchdown on Earth. The latter part of controlled descent is achieved by parachute or paraglider - or by all automatic or a human-controlled landing similar to that of the Orbiter. Since this report addresses the specific needs of human-carrying (not necessarily piloted) reentry vehicles, it deals with highly nonlinear equations of motion, and then-generated control systems must be robust across a very wide range of physics. Thus, this report deals almost exclusively with some form of dynamic inversion (DI). Two vital aspects of control theory - noninteracting control laws and the transformation of nonlinear systems into equivalent linear systems - are embodied in DI. Though there is no doubt that the mathematical tools and underlying theory are widely available, there are open issues as to the practicality of using DI as the only or primary design approach for reentry articles. This report provides a set of guidelines that can be used to determine the practical usefulness of the technique. Ito, Daigoro and Georgie, Jennifer and Valasek, John and Ward, Donald T. Johnson Space Center
Book Synopsis The Capability of a Proportional-type Lateral Control System in Providing Aerodynamic Heading-angle Trajectory Control During Reentry by : Gene W. Sparrow
Download or read book The Capability of a Proportional-type Lateral Control System in Providing Aerodynamic Heading-angle Trajectory Control During Reentry written by Gene W. Sparrow and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
