Sounding Rocket Delta Velocity System PDF Download
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Author: Edward F. McKenna
Publisher:
ISBN:
Category : Payloads (Aerospace engineering)
Languages : en
Pages : 20
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Book Description
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: Edward F. McKenna
Publisher:
ISBN:
Category : Payloads (Aerospace engineering)
Languages : en
Pages : 20
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Book Description
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:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 328
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautical instruments
Languages : en
Pages : 328
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Book Description
Author: Air Force Cambridge Research Laboratories (U.S.)
Publisher:
ISBN:
Category : Geophysics
Languages : en
Pages : 228
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Book Description
Author: Edward F. McKenna
Publisher:
ISBN:
Category : Payloads (Aerospace engineering)
Languages : en
Pages : 20
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Book Description
Research has been conducted into the problems of avoiding collision between separated payloads and spent rocket motors due to post burnout thrust and into the problem of contamination of scientific instrumentation due to outgassing of the smoldering insulation. In order to measure this post burnout thrust, a payload instrument module was separated from an instrumented Black Brant VC Rocket in the exoatmosphere. In addition to measuring accelerations and velocities, the spent motor was observed by a TV camera on board the command attitude controlled payload module. Analysis shows that the payload separated cleanly from the vehicle at a relative separation velocity of 2.25 ft/sec (0.69 m/sec). However, the residual thrust of the spent motor overcame this differential, catching up to the payload 37 sec after separation and continuing on a parallel velocity vector at about 3.37 ft/sec (1.03 m/sec). (Author).
Author: DP Mishra
Publisher: CRC Press
ISBN: 1351708414
Category : Technology & Engineering
Languages : en
Pages : 364
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Book Description
The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Author: Mike Tooley
Publisher: Butterworth-Heinemann
ISBN: 1856175766
Category : Technology & Engineering
Languages : en
Pages : 1187
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Book Description
A one-stop Desk Reference, for engineers involved in all aspects of aerospace; this is a book that will not gather dust on the shelf. It brings together the essential professional reference content from leading international contributors in the field. Material covers a broad topic range from Structural Components of Aircraft, Design and Airworthiness to Aerodynamics and Modelling * A fully searchable Mega Reference Ebook, providing all the essential material needed by Aerospace Engineers on a day-to-day basis. * Fundamentals, key techniques, engineering best practice and rules-of-thumb together in one quick-reference.* Over 2,500 pages of reference material, including over 1,500 pages not included in the print edition
Author: Howard D. Curtis
Publisher: Butterworth-Heinemann
ISBN: 0323853455
Category : Science
Languages : en
Pages : 782
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Book Description
Orbital Mechanics for Engineering Students, Fourth Edition, is a key text for students of aerospace engineering. While this latest edition has been updated with new content and included sample problems, it also retains its teach-by-example approach that emphasizes analytical procedures, computer-implemented algorithms, and the most comprehensive support package available, including fully worked solutions, PPT lecture slides, and animations of selected topics. Highly illustrated and fully supported with downloadable MATLAB algorithms for project and practical work, this book provides all the tools needed to fully understand the subject. - Provides a new chapter on the circular restricted 3-body problem, including low-energy trajectories - Presents the latest on interplanetary mission design, including non-Hohmann transfers and lunar missions - Includes new and revised examples and sample problems
Author: Ashley Chandler Karp
Publisher: Academic Press
ISBN: 0128165936
Category : Technology & Engineering
Languages : en
Pages : 344
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Book Description
Hybrid Rocket Propulsion Design Handbook provides system scaling laws, design methodologies, and a summary of available test data, giving engineers all the tools they need to develop realistic hybrid system designs.Important supporting theory from chemistry, thermodynamics, and rocket propulsion is addressed, helping readers from a variety of backgrounds to understand this interdisciplinary subject. This book also suggests guidelines for standardized reporting of test data, in response to difficulties researchers have in working with results from different research institutes. - Covers general theory, recent advances and current fragmented experimental results of hybrid rocket engines - Outlines testing standards for hybrid researchers - Provides guidance on how to use a freely available online code from NASA
Author: Goddard Space Flight Center
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 1048
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Book Description
