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History of Rocket Technology
CHAPTER 1 History of Rockets 1. 1. INTRODUCTION Action-Reaction Principle Take any technology and you always find that its practical demonstration had been realized much before the theory was established. However, you may note that the fast and effective refinement of a technology begins only after its theory, explaining the underlying basic principles, has been established. The action-reaction principle that is fundamental to jet propulsion, which includes airbreathing- as well as rocket-propulsion, was theoretically explained only in 1687 by the English scientist Sir Isaac Newton by his famous publication “Philosophiae Naturalis Principia Mathematica (“Mathematical Principles of Natural Philosophy”). But, approximately 2100 years before this, Archytas, a Greek philosopher, mathematician, astronomer, statesman, and strategist, had demonstrated the action-reaction principle by his toy pigeon in the city of Tarentum, Fig. 1. 1. Archytas suspended on a wire his wooden pigeon that contained hot steam at an elevated pressure in its belly cavity. The other end of the wire was hooked on to the top of a tall pole. On releasing a plug, a jet of steam escaped through a hole from the rear of the pigeon to produce a thrust that made the toy pigeon fly in circles around the pole. Thus Archytas mystified and amused the citizens of Tarentum by his flying toy- pigeon and demonstrated the fundamental principle of propulsion: “every force has an equal and opposite reaction”. The second recorded-demonstration of the action-reaction principle was in the first century B.C. Hero of Alexandria, a Greek mathematician 1 and scientist, constructed a device known as aeolipile. -
Quantitative Planetary Image Analysis Via Machine Learning
Tina Memo No. 2013-008 External, PhD Thesis, University of Manchester Quantitative Planetary Image Analysis via Machine Learning. Paul Tar Last updated 25 / 09 / 2014 Centre for Imaging Sciences, Medical School, University of Manchester, Stopford Building, Oxford Road, Manchester, M13 9PT. Quantitative Planetary Image Analysis via Machine Learning A thesis submitted to the University of Manchester for the degree of PhD in the faculty of Engineering and Physical Sciences 2014 Paul D. Tar School of Earth, Atmospheric and Environmental Sciences 2 Contents 1 Introduction 19 1.1 Theriseofimagingfromspace. ...... 19 1.1.1 Historicalimages ............................... 20 1.1.2 Contemporaryimages . 20 1.1.3 Futureimages.................................. 21 1.2 Sciencecase ..................................... .. 22 1.2.1 Lunarscience .................................. 22 1.2.2 Martianscience ................................ 22 1.3 Imageinterpretation ............................. ..... 23 1.3.1 Manualanalysis................................ 24 1.3.2 Automatedanalysis.............................. 24 1.4 Measurements.................................... .. 25 1.4.1 Quantitative measurements and The Scientific Method . .......... 26 1.4.2 Theroleofstatistics . ... 27 1.4.3 Assumptionsandapproximations . .... 29 1.5 Argumentforquantitativeautomation . ........ 30 1.6 Criteriaforaquantitativesystem . ......... 31 1.7 Thesisoutline ................................... ... 32 2 Literature Review 35 2.1 Representations ................................ -
Lunar Orbiter Photographic Atlas of the Near Side of the Moon Charles J
Lunar Orbiter Photographic Atlas of the Near Side of the Moon Charles J. Byrne Lunar Orbiter Photographic Atlas of the Near Side of the Moon Charles J. Byrne Image Again Middletown, NJ USA Cover illustration: Earth-based photograph of the full Moon from the “Consolidated Lunar Atlas” on the Website of the Lunar and Planetary Institute. British Library Cataloging-in-Publication Data Byrne, Charles J., 1935– Lunar Orbiter photographic atlas of the near side of the Moon 1. Lunar Orbiter (Artificial satellite) 2. Moon–Maps 3. Moon–Photographs from space I. Title 523.3 0223 ISBN 1852338865 Library of Congress Cataloging-in-Publication Data Byrne, Charles J., 1935– Lunar Orbiter photographic atlas of the near side of the Moon : with 619 figures / Charles J. Byrne. p. cm. Includes bibliographical references and index. ISBN 1-85233-886-5 (acid-free paper) 1. Moon–Maps. 2. Moon–Photographs from space. 3. Moon–Remote-sensing images. 4. Lunar Orbiter (Artificial satellite) I. Title. G1000.3.B9 2005 523.3 022 3–dc22 2004045006 Additional material to this book can be downloaded from http://extras.springer.com. ISBN 1-85233-886-5 Printed on acid-free paper. © 2005 Springer-Verlag London Limited Apart from any fair dealing for the purposes of research or private study, or criticism, or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be repro- duced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licenses issued by the Copyright Licensing Agency. -
PEENEMUENDE, NATIONAL SOCIALISM, and the V-2 MISSILE, 1924-1945 Michael
ABSTRACT Title of Dissertation: ENGINEERING CONSENT: PEENEMUENDE, NATIONAL SOCIALISM, AND THE V-2 MISSILE, 1924-1945 Michael Brian Petersen, Doctor of Philosophy, 2005 Dissertation Directed By: Professor Jeffrey Herf Departmen t of History This dissertation is the story of the German scientists and engineers who developed, tested, and produced the V-2 missile, the world’s first liquid -fueled ballistic missile. It examines the social, political, and cultural roots of the prog ram in the Weimar Republic, the professional world of the Peenemünde missile base, and the results of the specialists’ decision to use concentration camp slave labor to produce the missile. Previous studies of this subject have been the domain of either of sensationalistic journalists or the unabashed admirers of the German missile pioneers. Only rarely have historians ventured into this area of inquiry, fruitfully examining the history of the German missile program from the top down while noting its admi nistrative battles and technical development. However, this work has been done at the expense of a detailed examination of the mid and lower -level employees who formed the backbone of the research and production effort. This work addresses that shortcomi ng by investigating the daily lives of these employees and the social, cultural, and political environment in which they existed. It focuses on the key questions of dedication, motivation, and criminality in the Nazi regime by asking “How did Nazi authori ties in charge of the missile program enlist the support of their employees in their effort?” “How did their work translate into political consent for the regime?” “How did these employees come to view slave labor as a viable option for completing their work?” This study is informed by traditions in European intellectual and social history while borrowing from different methods of sociology and anthropology. -
Apollo 13 Mission Review
APOLLO 13 MISSION REVIEW HEAR& BEFORE THE COMMITTEE ON AERONAUTICAL AND SPACE SCIENCES UNITED STATES SENATE NINETY-FIRST CONGRESS SECOR’D SESSION JUR’E 30, 1970 Printed for the use of the Committee on Aeronautical and Space Sciences U.S. GOVERNMENT PRINTING OFFICE 47476 0 WASHINGTON : 1970 COMMITTEE ON AEROKAUTICAL AND SPACE SCIENCES CLINTON P. ANDERSON, New Mexico, Chairman RICHARD B. RUSSELL, Georgia MARGARET CHASE SMITH, Maine WARREN G. MAGNUSON, Washington CARL T. CURTIS, Nebraska STUART SYMINGTON, bfissouri MARK 0. HATFIELD, Oregon JOHN STENNIS, Mississippi BARRY GOLDWATER, Arizona STEPHEN M.YOUNG, Ohio WILLIAM B. SAXBE, Ohio THOJfAS J. DODD, Connecticut RALPH T. SMITH, Illinois HOWARD W. CANNON, Nevada SPESSARD L. HOLLAND, Florida J4MES J. GEHRIG,Stad Director EVERARDH. SMITH, Jr., Professional staffMember Dr. GLENP. WILSOS,Professional #tad Member CRAIGVOORHEES, Professional Staff Nember WILLIAMPARKER, Professional Staff Member SAMBOUCHARD, Assistant Chief Clerk DONALDH. BRESNAS,Research Assistant (11) CONTENTS Tuesday, June 30, 1970 : Page Opening statement by the chairman, Senator Clinton P. Anderson-__- 1 Review Board Findings, Determinations and Recommendations-----_ 2 Testimony of- Dr. Thomas 0. Paine, Administrator of NASA, accompanied by Edgar M. Cortright, Director, Langley Research Center and Chairman of the dpollo 13 Review Board ; Dr. Charles D. Har- rington, Chairman, Aerospace Safety Advisory Panel ; Dr. Dale D. Myers, Associate Administrator for Manned Space Flight, and Dr. Rocco A. Petrone, hpollo Director -___________ 21, 30 Edgar 11. Cortright, Chairman, hpollo 13 Review Board-------- 21,27 Dr. Dale D. Mvers. Associate Administrator for Manned SDace 68 69 105 109 LIST OF ILLUSTRATIOSS 1. Internal coinponents of oxygen tank So. 2 ---_____-_________________ 22 2. -
Apollo 11 Lunar Landing Mission Press Kit, Part 2
-lOl- The ascent stage engine compartment is formed by two beams running across the lower midsection deck and mated to the fore and aft bulkheads. Systems located in the midsection include the LM guidance computer, the power and servo assembly, ascent engine propellant tanks, RCS pro- pellant tanks, the environmental control system, and the waste management section. A tunnel ring atop the ascent stage meshes with the command module docking latch assemblies. During docking, the CM docking ring and latches are aligned by the LM drogue and the CSM probe. The dockingtunnel extends downward into the midsection 16 inches (40 cm). The tunnel is B2 inches (0.81 cm) in dia- meter and Is used for crew transfer between the CSM and LM. The upper hatch on the inboard end of the docking tunnel hinges downward and cannot be opened with the LM pressurized and u_docked. A thermal and mlcrometeoroid shield of multiple layers of mylar and a single thickness of thin aluminum skin encases the entire ascent stage structure. Descent Stase The descent stage consists of a cruciform load-carrylng structure of two pairs of parallel beams, upper and lower decks, and enclosure bulkheads -- all of conventional skln-and-strlnger aluminum alloy construction. The center compartment houses the descent engine, and descent propellant tanks are housed in the four square bays around the engine. The descent stage measures i0 feet 7 inches high by 14 feet 1 inch in diameter. Four-legged truss outriggers mounted on the ends of each pair of beams serve as SLA attach points and as "knees" for the landing gear main struts. -
Lunar Orbiter Ii
NASA CONTRACTOR NASA CR-883 REPORT LUNAR ORBITER II Photographic Mission Summary Prepared by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAl AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • OCTOBER 1967 THE CRATER COPERNICUS - Photo taken by NASA-Boeing Lunar Orbiter II, November 23, 1966,00:05:42 GMT, from a distance of 150 miles. NASA CR-883 LUNAR ORBITER II Photographic Mission Summary Distribution of this report is provided in the interest of information exchange. Responsibility for the contents resides in the author or organization that prepared it. Issued by Originator as Document No. D2-100752-1 Prepared under Contract No. NAS 1-3800 by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sole by the Clearinghouse for Federal Scientific and Technical Information Springfield, Virginia 22151 - CFSTI price $3.00 CONTENTS Page No. 1.0 LUNAR ORBITER II MISSION SUMMARY 1 1.1 INTRODUCTION 4 1.1.1 Program Description 4 1.1.2 Program Management 5 1.1.3 Program Objectives 6 1.1.3.1 Mission II Objectives 6 1.1.4 Mission Design 8 1.1.5 Flight Vehicle Description 12 1.2 LAUNCH PREPARATION AND OPERATIONS 19 1.2.1 Launch Vehicle Preparation 19 1.2.2 Spacecraft Preparation 21 1.2.3 Launch Countdown 21 1.2.4 Launch Phase 22 1.2.4.1 Flight Vehicle Performance 22 1.2.5 Data Acquisition 24 1.3 MISSION OPERATIONS 29 1.3.1 Mission Profile 29 1.3.2 Spacecraft Performance 31 1.3.2.1 Photo Subsystem Performance 32 1.3.2.2 Power Subsystem Performance 34 1.3.2.3 Communications -
NASA and Planetary Exploration
**EU5 Chap 2(263-300) 2/20/03 1:16 PM Page 263 Chapter Two NASA and Planetary Exploration by Amy Paige Snyder Prelude to NASA’s Planetary Exploration Program Four and a half billion years ago, a rotating cloud of gaseous and dusty material on the fringes of the Milky Way galaxy flattened into a disk, forming a star from the inner- most matter. Collisions among dust particles orbiting the newly-formed star, which humans call the Sun, formed kilometer-sized bodies called planetesimals which in turn aggregated to form the present-day planets.1 On the third planet from the Sun, several billions of years of evolution gave rise to a species of living beings equipped with the intel- lectual capacity to speculate about the nature of the heavens above them. Long before the era of interplanetary travel using robotic spacecraft, Greeks observing the night skies with their eyes alone noticed that five objects above failed to move with the other pinpoints of light, and thus named them planets, for “wan- derers.”2 For the next six thousand years, humans living in regions of the Mediterranean and Europe strove to make sense of the physical characteristics of the enigmatic planets.3 Building on the work of the Babylonians, Chaldeans, and Hellenistic Greeks who had developed mathematical methods to predict planetary motion, Claudius Ptolemy of Alexandria put forth a theory in the second century A.D. that the planets moved in small circles, or epicycles, around a larger circle centered on Earth.4 Only partially explaining the planets’ motions, this theory dominated until Nicolaus Copernicus of present-day Poland became dissatisfied with the inadequacies of epicycle theory in the mid-sixteenth century; a more logical explanation of the observed motions, he found, was to consider the Sun the pivot of planetary orbits.5 1. -
Lunar Orbiter Iv
NASA CONTRACTOR NASA CR-1054 REPORT LUNAR ORBITER IV Photographic Mission Summary Prepared by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • JUNE 1968 First Detailed View of Orientale Basin Photo taken by NASA-Boeing Lunar Orbiter IV, May 25, 1967, 05:33:34 GMT, from an altitude o£2,721 kilometers. NASA CR-1054 LUNAR ORBITER IV Photographic Mission Summary Distribution of this report is provided in the interest of information exchange. Responsibility for the contents resides in the author or organization that prepared it. Issued by Originator as Boeing Document No. 02-100754-1 (Vol. 1) Prepared under Contract No. NAS 1-3800 by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sale by the Clearinghouse for Federal Scientific and Technical Information Springfield, Virginia 22151 - CFSTI price $3.00 Contents Page 1.0 INTRODUCTION . ........ ............ ............... ....... ............... 5 1.1 Program Description ....................................................... 5 1.2 Program Management ...................................................... 5 1.3 Program Objectives ........................................................ 6 1.3.1 Mission IV Objectives ................................................. 7 1.4 Mission Design ............................... ..... ....... .... ............ 8 1.5 Flight Vehicle Description ... ......... ............................. .... .. .. 11 2.0 LAUNCH PREPARATION -
Marshall Space Flight Center
............__........ Marshall Space Flight Center Introduction This booklet, prepared by the Marshall Space Flight Center, is illustrative of the Center's support for the von Braun Celebration of the Arts and Sciences (VBCAS). Marshall is honored to be a participant in the celebration of this 50-year cultural and technological legacy of Dr. Wernher von Braun and the members of his famed German rocket team. The VBCAS features a year-long series of events, performances, exhibits and historical, cultural and educational programs. Special performances by internationally known artists and speakers, and commemorative events featuring an aerospace, German, or nostalgic theme will be held during this year-long celebration. More than 30 arts, technology, educational and community organizations have been working for almost three years to plan this series of events. In 1950, Dr. von Braun and approximately 100 of his team members came to Huntsville, Alabama, to begin work on what would later become America's historic space program. Dr. von Braun eventually served as the first director of the Marshall Center and led the development of the Saturn V launch vehicle that lofted three American astronauts on their journey to the moon in July 1969. music. In the 1920s, von Braun was accepted for led the piano lessons by the great composer Paul design for the most powerful rocket the world has Hindemith and had even composed some pieces of ever known and used it to launch the first humans his own by the age of 15. Von Braun also took cello to the surface of the moon in 1969. -
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Memorial Tributes: Volume 17 Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 17 ABE SILVERSTEIN 1908–2001 Elected in 1967 “For aeronautical and space systems.” BY ROBERT S. ARRIGHI SUBMITTED BY THE NAE HOME SECRETARY ABE SILVERSTEIN was a visionary engineer and leader whose accomplishments during his 40-year career continue to impact the aerospace community. He was instrumental in the design of a massive subsonic wind tunnel (the Full-Scale Tunnel), study of complete engine systems, development of the nation’s early jet engines and ramjets, creation of large supersonic wind tunnels, use of liquid hydrogen as a propellant, the foundation of NASA, formation of the Mercury and Apollo Programs, the success of the Centaur second- stage rocket, and a great deal more. He excelled at instantly grasping the essence of a problem, proposing a likely solution, and delegating the task to the experts to resolve. His off-the- cuff acumen and decisiveness inspired both fear and intense loyalty from staff and colleagues. Abe Silverstein died on June 1, 2001, at the age of 92. Abe was born on September 15, 1908, in Terre Haute, Indiana, to Joseph and Eva Silverstein. His father advised him at a young age to pursue engineering, and Abe claimed that his mother’s insistence on perfection in his school work provided him with the mindset required for future space engineering. Abe graduated from Terre Haute’s Rose Polytechnic Institute in 1929 with a BS in mechanical engineering. He returned to earn a degree as a mechanical engineering professional in 1934. -
Auburn University – Romance, Rocketry, and the Dannenberg Connection
Auburn University – Romance, Rocketry and the Dannenberg Connection Auburn University – Romance, Rocketry, and the Dannenberg Connection Dr. Joseph Majdalani, faculty advisor at Auburn University Auburn University is not only known for its campus beauty, college romance, and passion for football, but also for its celebrated history in aeronautics, its love for rocketry, its faithful devotion to the AIAA community, and its intimate connection with the Wright Brothers and the Dannenberg family. This year was particularly romantic as it seems to have started and ended with two totally unrelated events, which nonetheless involved Auburn‟s incoming Chair for Aerospace Engineering, Dr. Joe Majdalani, and two distinguished members of Konrad Dannenberg‟s immediate family, whose association with Auburn University dates back to the Apollo era: Dr. Klaus Dannenberg, „67 Auburn Aerospace Engineering and AIAA Deputy Executive Director, for the SciTech Award Banquet, and Jacquelyn (Jackie) Dannenberg, wife of Konrad Dannenberg, for the awarding of the Konrad Dannenberg Educator of the Year Award in Huntsville. LTR: Konrad and Klaus Dannenberg at the Auburn Alumni Engineering Council Meeting (April 2007). The year also encompassed a number of developments and recognitions, such as a record participation in the AIAA Region II Student Conference with 20 Auburn students, a first place award capture in both undergraduate and graduate divisions of the 65th AIAA Southeastern Regional Conference, a first place award ranking among all seven regions of AIAA