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Author : Leslie G. Smith
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (377 download)
Download or read book A Simple Method of Trajectory Determination for Sounding Rockets written by Leslie G. Smith and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ernesto Gismondi
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
Download or read book A New Method of Approaching the Design of Sounding Rockets written by Ernesto Gismondi and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert M. Howe
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.L/5 ( download)
Download or read book Trajectory calculations for sounding rockets written by Robert M. Howe and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Edward F. McKenna
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.3/5 (91 download)
Download or read book Sounding Rocket Delta Velocity System written by Edward F. McKenna and published by . This book was released on 1976 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: A sounding rocket tumble system to enhance deceleration and redirect the flight path angle of a vehicle can be an effective means of accomplishing large spacial separation between a separated payload and the spent final stage rocket motor. The design and implementation of two such systems, for 9-in. - and 17-in. -diam payloads, is presented. Flight test results show that separation distances between payload and vehicle in the order of 10 percent of vehicle apogee can be achieved. (Author).
Author : K. A. Steele
Publisher :
ISBN 13 :
Total Pages : 7 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Single Station Doppler Range Technique for Sounding Rocket Trajectories written by K. A. Steele and published by . This book was released on 1968 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt: A doppler ranging technique for determining the height and horizontal range-time histories of flight of a sounding rocket is described. Two stable oscillators operating at the same frequency are employed. One oscillator is carried in the rocket and its output is telemetered to the ground. The other oscillator is used as a ground-based reference located at the telemetry receiving station at the launch site. The method is primarily of interest for use at remote launching sites where normal range tracking facilities do not exist. The results of a number of trials of the method with Black Brant II rockets launched at the Churchill Research Range are discussed. They indicate that an accuracy of plus or minus 1 km for apogee height can be obtained. (Author).
Author : Charles F. Miller (Jr)
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Graphic Method for Determining the Absolute Attitude of Sounding Rocket Vehicles written by Charles F. Miller (Jr) and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Charles H. Whitlock
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)
Download or read book Comparison of Steady-state and Six-degree-of-freedom Analyses of Pitch-roll Resonance Conditions for a Long Slender Sounding Rocket written by Charles H. Whitlock and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Allen B. Henning
Publisher :
ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Wind-compensation Method and Results of Its Application to Flight Tests of Twelve Trailblazer Rocket Vehicles written by Allen B. Henning and published by . This book was released on 1964 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ph Uyttendaele
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (12 download)
Download or read book The Accuracy of Determination of the Upper Reaches of a Sounding Rocket Trajectory Using Tracking Angles from a Single Station written by Ph Uyttendaele and published by . This book was released on 1966 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : CAgodi Onwumechikli
Publisher : Routledge
ISBN 13 : 1351449931
Total Pages : 650 pages
Book Rating : 4.3/5 (514 download)
Download or read book Equatorial Electrojet written by CAgodi Onwumechikli and published by Routledge. This book was released on 2019-03-04 with total page 650 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is the first book to review all the fields of equatorial electrojet phenomena and their relevant theories in one volume. In certain relevant sections, the book discusses both the equatorial electrojet and the world-wide parts of the Sq current systems. Onwumwchili is an internationally known and highly respected expert in the equatorial electrojet field- a brand of geomagnetism.
Author : International Telemetering Conference
Publisher :
ISBN 13 :
Total Pages : 856 pages
Book Rating : 4.0/5 ( download)
Download or read book Proceedings written by International Telemetering Conference and published by . This book was released on 1965 with total page 856 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Keith E. Hennigh
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)
Download or read book Field Wind Weighting and Impact Prediction for Unguided Rockets written by Keith E. Hennigh and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert L. James
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (31 download)
Download or read book Calculation of Wind Compensation for Launching of Unguided Rockets written by Robert L. James and published by . This book was released on 1961 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 826 pages
Book Rating : 4.3/5 (91 download)
Download or read book Proceedings written by and published by . This book was released on 1965 with total page 826 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher :
ISBN 13 :
Total Pages : 1152 pages
Book Rating : 4.F/5 ( download)
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1965 with total page 1152 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 556 pages
Book Rating : 4.F/5 ( download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John D. Bird
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
Download or read book An Investigation of the Optimum Design and Flight of Rockets written by John D. Bird and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis using classical variational methods was made whereby significant physical characteristics of rockets were determined in an optimal sense. A two-point boundary-value problem was formulated which, when solved, provided the significant physical parameters and flight path for a two-stage rocket which would deliver a given payload to orbit with minimum total initial mass. Numerical solutions were carried out for nine cases by an iterative method. The results show how the stage masses and thrusts should be proportioned for various structural efficiencies in the fuel tanks and rocket motors. Analyses of the type carried out for this investigation should be useful in the sizing and, generally, in the design of rockets.
