Apollo Rocket Propulsion Development

Total Page:16

File Type:pdf, Size:1020Kb

Apollo Rocket Propulsion Development REMEMBERING THE GIANTS APOLLO ROCKET PROPULSION DEVELOPMENT Editors: Steven C. Fisher Shamim A. Rahman John C. Stennis Space Center The NASA History Series National Aeronautics and Space Administration NASA History Division Office of External Relations Washington, DC December 2009 NASA SP-2009-4545 Library of Congress Cataloging-in-Publication Data Remembering the Giants: Apollo Rocket Propulsion Development / editors, Steven C. Fisher, Shamim A. Rahman. p. cm. -- (The NASA history series) Papers from a lecture series held April 25, 2006 at the John C. Stennis Space Center. Includes bibliographical references. 1. Saturn Project (U.S.)--Congresses. 2. Saturn launch vehicles--Congresses. 3. Project Apollo (U.S.)--Congresses. 4. Rocketry--Research--United States--History--20th century-- Congresses. I. Fisher, Steven C., 1949- II. Rahman, Shamim A., 1963- TL781.5.S3R46 2009 629.47’52--dc22 2009054178 Table of Contents Foreword ...............................................................................................................................7 Acknowledgments .................................................................................................................9 Welcome Remarks Richard Gilbrech ..........................................................................................................11 Steve Fisher ...................................................................................................................13 Chapter One - Robert Biggs, Rocketdyne - F-1 Saturn V First Stage Engine .......................15 Chapter Two - Paul Coffman, Rocketdyne - J-2 Saturn V 2nd & 3rd Stage Engine .............27 Chapter Three - Gerald R. Pfeifer, Aerojet - Attitude Control Engines ................................39 Chapter Four - Tim Harmon, Rocketdyne - SE-7 & SE-8 Engines .....................................51 Chapter Five - Clay Boyce, Aerojet - AJ10-137 Apollo Service Module Engine ...................59 Chapter Six - Gerard Elverum, TRW - Lunar Descent Engine.............................................73 Chapter Seven - Tim Harmon, Rocketdyne - Lunar Ascent Engine ....................................87 Appendix A - Event Program ...............................................................................................97 Appendix B - Speakers’ Group Photograph .......................................................................101 Appendix C - Robert Biggs’ Presentation Viewgraphs ........................................................103 Appendix D - Paul Coffman’s Presentation Viewgraphs .....................................................113 Appendix E - G. R. “Jerry” Pfeifer’s Presentation Viewgraphs ............................................123 Appendix F - Tim Harmon’s SE-7 & SE-8 Presentation Viewgraphs .................................133 Appendix G - Clay Boyce’s Presentation Viewgraphs .........................................................143 Appendix H - Jerry Elverum’s Presentation Viewgraphs .....................................................151 Appendix I - Tim Harmon’s Lunar Ascent Engine Presentation Viewgraphs ......................171 Appendix J - Event Photos and Highlights ........................................................................179 Further Reading ................................................................................................................191 Glossary ............................................................................................................................193 The NASA History Series ..................................................................................................197 Apollo Rocket Propulsion Development 3 On April 25, 2006, NASA’s John C. Stennis Space Center hosted a series of lectures on Apollo Propulsion development. This monograph is a transcript of the event, held as part of the cel- ebration to mark the 40th anniversary of the first rocket engine test conducted at the site then known as the Mississippi Test Facility. On April 23, 1966, engineers tested a cluster of five J-2 engines that powered the second stage of the Saturn V moon rocket. This transcript has been edited for readability and clarity. The opinions expressed are solely those of the individuals presented. The report does not in any way promulgate policies or state the official opinions of the National Aeronautics and Space Administration or the U.S. government. John C. Stennis Space Center History Office B-1100 Stennis Space Center, MS 39529 228.688.2646 2006 Event Title “On the Shoulders of Giants,” Apollo Propulsion Development Seminars. Moderator: Steve Fisher, Rocketdyne Speakers: Robert Biggs, Paul Coffman, Gerald Pfeifer, Clay Boyce, Gerard Elverum, and Tim Harmon Initial Transcription: Michele Beisler, Transcription/Technical Writing: B. Nicole Wells (Jacobs Technology Facility Operating Services Contract) Editors: Mr. Steve Fisher, P&W Rocketdyne, and Dr. Shamim Rahman, NASA Event Coordinator: Rebecca Strecker, NASA About the Cover – At left, the Apollo Saturn launch vehicle; middle, a J-2 engine on a static test stand operating on oxygen and hydrogen; and at right, lunar surface photographed from approaching spacecraft. Dr. Shamim Rahman began his professional career at The Aerospace Corporation in El Segundo, CA, in 1985 as an aerospace engineer on launch vehicle and spacecraft flight programs for the Air Force Space and Missile Command. He later joined the TRW Propulsion Research Center to work on innovative rocket propulsion devices for civil and military space applications. Dr. Rahman joined NASA in 1998. At Stennis Space Center (SSC), Dr. Rahman has provided technical leadership and oversight on national rocket propulsion test facilities, and over a variety of research and development test activities for advanced rocket propulsion development. Dr. Rahman assumed his current position in November, 2007, as the Deputy Director for the Engineering & Test Directorate at NASA SSC. Mr. Steve Fisher has spent 37 years at Rocketdyne in the design, development, testing, and evaluation of liquid rocket engines, and recently retired as a Technical Fellow from Pratt & Whitney Rocketdyne. He initially joined North American Aviation of El Segundo to work on the original B-1 Bomber, and later transferred to the original Rocketdyne Division of the company. During his tenure, he was integrally involved in the development of the Space Shuttle Main Engine components at the Coca 1 and Coca 4 test facilities of Rocketdyne, and has further contributed to a wide variety of propulsion activities including advanced research and development projects with storable and cryogenic propellants, as well as flight engine projects such as the RS-68 engine design and development. Mr. Fisher served as a Boeing Technical Fellow prior to the Rocketdyne division being sold to Pratt & Whitney. 6 Remembering the Giants Foreword It gives us great pleasure to provide this historical compendium of what will likely be remembered as one of the most remarkable achievements in the evolution of rocket propulsion. This achievement was the simultaneous development, testing, and flight use of a series of first- ever propulsive devices that delivered Apollo 11 astronauts safely to the surface of the moon and back to Earth. These devices helped assure three individuals, Armstrong, Aldrin, and Collins a place in the history of humankind. From the F-1 booster engine to the lunar module ascent engine of the Apollo vehicle stack – all built and delivered by the new United States space industrial base – these individual rocket propulsion development stories provide a glimpse of how technical ingenuity rose to meet the challenge of the race to the moon. The development histories and lessons learned about the various engines are told by the engineers and project managers, and were recorded on DVD so that the lecture series held at NASA’s John C. Stennis Space Center near Bay St. Louis, Mississippi, could be replayed again and thus live on. Remarkably, to those who attended, it was apparent that these speakers recalled their Apollo challenges as if they had happened “just yesterday.” It was clear in their voices that the engines carried not just the hardware but also the hope of the nation that this “moon shot” could even be done at all. Although this monograph comes some years after the actual date of the lectures, and describes work from decades ago, the lessons will continue to carry space exploration forward. The story told within is not how one particular engine was built, but rather how ordinary people persisted and were driven to do extraordinary work. The country owes these resourceful and dedicated engineers a debt of gratitude for giving us the technical precedents upon which today’s space programs rest in a continuing story of human exploration. It would not have been possible without the sanction and enthusiastic support of NASA Stennis Space Center’s “front office” (center director, deputy director, and associate director), and the excellent support and facilitation of the local NASA public affairs staff. The 2006 event was officially designated at NASA SSC as “On the Shoulders of Giants”, and in this monograph is more aptly designated by the title, “Remembering the Giants.” Shamim A. Rahman, PhD, NASA Stennis Space Center Steven C. Fisher, Technical Fellow, Boeing and Pratt & Whitney Retired Apollo Rocket Propulsion Development 7 8 Remembering the Giants Acknowledgments The initial transcription of these seminars was done by Michele Beisler and Shelia Reed,
Recommended publications
  • Victor Or Villain? Wernher Von Braun and the Space Race
    The Social Studies (2011) 102, 59–64 Copyright C Taylor & Francis Group, LLC ISSN: 0037-7996 print / 2152-405X online DOI: 10.1080/00377996.2010.484444 Victor or Villain? Wernher von Braun and the Space Race JASON L. O’BRIEN1 and CHRISTINE E. SEARS2 1Education Department, University of Alabama in Huntsville, Huntsville, Alabama, USA 2History Department, University of Alabama in Huntsville, Huntsville, Alabama, USA Set during the Cold War and space race, this historical role-play focuses on Wernher von Braun’s involvement in and culpability for the use of slave laborers to produce V-2 rockets for Nazi Germany. Students will grapple with two central questions. Should von Braun have been allowed to emigrate to the United States given his affiliation with the Nazis and use of slave laborers? Should the U.S. government and military have put Braun in powerful positions in NASA and military programs? This activity encourages students to hone their critical thinking skills as they consider and debate a complex, multi-layered historical scenario. Students also have opportunity to articulate persuasive arguments either for or against von Braun. Each character sketch includes basic information, but additional references are included for teachers and students who want a more in depth background. Keywords: role-play, Wernher von Braun, Space Race, active learning Victor or Villain? Wernher von Braun and the Space Role-Playing as an Instructional Strategy Race By engaging in historical role-plays, students can explore In 2009, the United States celebrated the fortieth anniver- different viewpoints regarding controversial topics (Clegg sary of the Apollo 11 crew’s landing on the moon.
    [Show full text]
  • Mission to Jupiter
    This book attempts to convey the creativity, Project A History of the Galileo Jupiter: To Mission The Galileo mission to Jupiter explored leadership, and vision that were necessary for the an exciting new frontier, had a major impact mission’s success. It is a book about dedicated people on planetary science, and provided invaluable and their scientific and engineering achievements. lessons for the design of spacecraft. This The Galileo mission faced many significant problems. mission amassed so many scientific firsts and Some of the most brilliant accomplishments and key discoveries that it can truly be called one of “work-arounds” of the Galileo staff occurred the most impressive feats of exploration of the precisely when these challenges arose. Throughout 20th century. In the words of John Casani, the the mission, engineers and scientists found ways to original project manager of the mission, “Galileo keep the spacecraft operational from a distance of was a way of demonstrating . just what U.S. nearly half a billion miles, enabling one of the most technology was capable of doing.” An engineer impressive voyages of scientific discovery. on the Galileo team expressed more personal * * * * * sentiments when she said, “I had never been a Michael Meltzer is an environmental part of something with such great scope . To scientist who has been writing about science know that the whole world was watching and and technology for nearly 30 years. His books hoping with us that this would work. We were and articles have investigated topics that include doing something for all mankind.” designing solar houses, preventing pollution in When Galileo lifted off from Kennedy electroplating shops, catching salmon with sonar and Space Center on 18 October 1989, it began an radar, and developing a sensor for examining Space interplanetary voyage that took it to Venus, to Michael Meltzer Michael Shuttle engines.
    [Show full text]
  • Space Administration
    https://ntrs.nasa.gov/search.jsp?R=19700024651 2020-03-23T18:20:34+00:00Z TO THE CONGRESSOF THE UNITEDSTATES : Transmitted herewith is the Twenty-first Semiannual Repol* of the National Aeronautics and Space Administration. Twen~-first SEMIANNUAL REPORT TO CONGRESS JANUARY 1 - JUNE 30, 1969 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. 20546 Editors: G. B. DeGennaro, H. H. Milton, W. E. Boardman, Office of Public Affairs; Art work: A. Jordan, T. L. Lindsey, Office of Organiza- tion and Management. For sale by the Superintendent of Documents, U.S. Government Printing Office Washington, D.C. 20402-Price $1.25 THE PRESIDENT May 27,1970 The White House I submit this Twenty-First Semiannual Report of the National Aeronautics and Space Aldministration to you for transmitttal to Congress in accordance with section 206(a) of the National Aero- nautics and Space Act of 1958. It reports on aotivities which took place betiween January 1 and June 30, 1969. During this time, the Nation's space program moved forward on schedule. ApolIo 9 and 10 demonstrated the ability of ;the man- ned Lunar Module to operate in earth and lunar orbit and its 'eadi- ness to attempt the lunar landing. Unmanned observatory and ex- plorer class satellites carried on scientific studies of the regions surrounding the Earth, the Moon, and the Sun; a Biosatellite oarwing complex biological science experiment was orbited; and sophisticated weather satellites and advanced commercial com- munications spacecraft became operational. Advanced research projects expanded knowledge of space flighk and spacecraft engi- neering as well as of aeronautics.
    [Show full text]
  • Back to the the Future? 07> Probing the Kuiper Belt
    SpaceFlight A British Interplanetary Society publication Volume 62 No.7 July 2020 £5.25 SPACE PLANES: back to the the future? 07> Probing the Kuiper Belt 634089 The man behind the ISS 770038 Remembering Dr Fred Singer 9 CONTENTS Features 16 Multiple stations pledge We look at a critical assessment of the way science is conducted at the International Space Station and finds it wanting. 18 The man behind the ISS 16 The Editor reflects on the life of recently Letter from the Editor deceased Jim Beggs, the NASA Administrator for whom the building of the ISS was his We are particularly pleased this supreme achievement. month to have two features which cover the spectrum of 22 Why don’t we just wing it? astronautical activities. Nick Spall Nick Spall FBIS examines the balance between gives us his critical assessment of winged lifting vehicles and semi-ballistic both winged and blunt-body re-entry vehicles for human space capsules, arguing that the former have been flight and Alan Stern reports on his grossly overlooked. research at the very edge of the 26 Parallels with Apollo 18 connected solar system – the Kuiper Belt. David Baker looks beyond the initial return to the We think of the internet and Moon by astronauts and examines the plan for a how it helps us communicate and sustained presence on the lunar surface. stay in touch, especially in these times of difficulty. But the fact that 28 Probing further in the Kuiper Belt in less than a lifetime we have Alan Stern provides another update on the gone from a tiny bleeping ball in pioneering work of New Horizons.
    [Show full text]
  • Space Transportation Association Roundtable "An Engineering Assessment of the Way-Forward in Human Spaceflight” September 9, 2010 Rayburn Building
    Space Transportation Association Roundtable "An Engineering Assessment of the Way-Forward in Human Spaceflight” September 9, 2010 Rayburn Building Thank you, Rich, for the opportunity to get together on this important topic with this group. Please let me begin with a disclaimer. While I am the Executive Director of the American Institute of Aeronautics and Astronautics, by no means do I speak for the Institute. We have some 36,000 student and professional members – including all four of us on the panel. Our volunteer leadership establishes our policy positions, and to be candid, it is an extremely difficult process to get consensus on almost any subject. With a topic as filled with options and differing views as what we are talking about this morning, we consider our role to be to provide opportunities to debate issues and bring out technically sound perspectives rather than advocate positions. So, I’m afraid I will have to use the standard disclaimer that the views expressed are my own. 1 Over the past few years Mike and I have discussed various aspects of the space exploration portfolio. On some we have agreed, on some we have agreed to disagree. Mike will be on the AIAA election Ballot in a few months to run for the same position he had to resign when he was confirmed as Administrator of NASA – President‐Elect of AIAA. I think it is both a characteristic and strength of AIAA that the senior staff person and the person who was a month away from being my boss, and may be again, can engage in debate on issues and agree to disagree.
    [Show full text]
  • Progress Report on Apollo Program
    PROGRESS REPORT ON APOLLO PROGRAM Michael Collins, LCol. USAF (M) Astronaut NASA-MANNED SPACECRAFT CENTER It is a great pleasure to be here today and to greet you hardy suMvors of the pool party. I will do my best to avoid loud noises and bright colors during my status report. Since the last SETP Symposium, the Apollo Program has been quite busy in a number of different areas. (Figure 1) My problem is to sift through this information and to talk only about those things of most interest to you. First, to review briefly our hardware, we are talking about two different spacecraft and two different boosters. (Figure 2) The Command Module is that part of the stack COLLINS which makes the complete round trip to the moon. Attached to it is the Service Module, containing expendables and a 20,000 pound thrust engine for maneuverability. The Lunar Module will be carried on later flights and is the landing vehicle and active rendezvous partner. The uprated Saturn I can put the Command and Service Modules into earth orbit; the Saturn V is required when the Lunar Module is added. Since the last symposium, we have flown the Command and Service Modules twice and the Lunar Module once, all unmanned. Apollo 4, the first Saturn V flight, was launched in November 1967. (Figure 3) The Saturn V did a beautiful, i.e. nominal, job of putting the spacecraft into earth parking orbit. After a coast period, the third stage (S-IVB by McDonnell Douglas) was ignited a second time, achieving a highly elliptical orbit.
    [Show full text]
  • Delta II Icesat-2 Mission Booklet
    A United Launch Alliance (ULA) Delta II 7420-10 photon-counting laser altimeter that advances MISSION rocket will deliver the Ice, Cloud and land Eleva- technology from the first ICESat mission tion Satellite-2 (ICESat-2) spacecraft to a 250 nmi launched on a Delta II in 2003 and operated until (463 km), near-circular polar orbit. Liftoff will 2009. Our planet’s frozen and icy areas, called occur from Space Launch Complex-2 at Vanden- the cryosphere, are a key focus of NASA’s Earth berg Air Force Base, California. science research. ICESat-2 will help scientists MISSION investigate why, and how much, our cryosphere ICESat-2, with its single instrument, the is changing in a warming climate, while also Advanced Topographic Laser Altimeter System measuring heights across Earth’s temperate OVERVIEW (ATLAS), will provide scientists with height and tropical regions and take stock of the vege- measurements to create a global portrait of tation in forests worldwide. The ICESat-2 mission Earth’s third dimension, gathering data that can is implemented by NASA’s Goddard Space Flight precisely track changes of terrain including Center (GSFC). Northrop Grumman built the glaciers, sea ice, forests and more. ATLAS is a spacecraft. NASA’s Launch Services Program at Kennedy Space Center is responsible for launch management. In addition to ICESat-2, this mission includes four CubeSats which will launch from dispens- ers mounted to the Delta II second stage. The CubeSats were designed and built by UCLA, University of Central Florida, and Cal Poly. The miniaturized satellites will conduct research DELTA II For nearly 30 years, the reliable in space weather, changing electric potential Delta II rocket has been an industry and resulting discharge events on spacecraft workhorse, launching critical and damping behavior of tungsten powder in a capabilities for NASA, the Air Force Image Credit NASA’s Goddard Space Flight Center zero-gravity environment.
    [Show full text]
  • An Early Manned Lunar Landing Q
    . ' - ,, ,, ,, . ... , " X64 80440 O~s7!- A FEASIBLE APPROACH FOR AN EARLY MANNED LUNAR LANDING Q PART I SUMMARY REPORT OF AD HOC TASK GROUP STU6Y (u) JUNE 16, 1961 Restriction/Classification Cancelled NA§A HEADQUARTERS, NATIONAL AERONAUTICS AND SPACE ADMINISTRATION ' I ------AD HOC TASK .GROUP . William A. Fleming - Chairman, Hq. Facilities Addison M. Rothrock - Deputy Chairman, Hq.· Albert J. Kelley - Hq. Samuel Snyder - Hq. Berg Paraghamian - Hq. Robert D. Briskman - ·Hq. Walter W. Haase - Hq. Secrest L. Berry - Hq. Spacecraft Llle Sciences . ..John H. Disher - Hq. James P. Nolan, Jr. - ·Hq • Merle. G•. Waugh - Hq. A.H. Schwichtenberg - Lovelace Foundation. Kenneth Kleinknecht - STG Alan B. Kehlet - STG Advanced Technology Launch Vehicles Ernesto. Pearson, Jr. - Hq. Eldon W. Hall - Hq. Space Sciences Melvyn Savage - Hq. Heinz H. Koelle .- MSFC · William Shipley - JPL William L. Lovejoy_~_Hq. Robert Fellows - Hq •.. Norman Raf el - Hq. Alfred M. Nelson - Hq. The effort: or the Ad Hoc Task Group were supplemented very signllicantly by major contributions in each technical area from a large number or other staff members at the various NASA Centers and at NASA Headquarters. Although these· added participants are too numerous to mention individually, their contributions are a vital part of the study results. i Restriction/Classification Cancelled lil TABLE OF CONTENTS INTRODUCTION ~ Purpose and Study Approach 1 Ground Rules and Guidelines 2 Program Elements 3 Use of the Sequenced Milestone System 4 Approach to Program Funding 5 PROGRAM PLAN ·objectives 6 Program Scope 8 Mission Approach 12 Spacecraft Requirements 24 Launch Vehicle Development 32_ Facilities 48 ' Supporting Research 62 Early .Managemen:b·;_ Actiort:s.
    [Show full text]
  • JUICE Red Book
    ESA/SRE(2014)1 September 2014 JUICE JUpiter ICy moons Explorer Exploring the emergence of habitable worlds around gas giants Definition Study Report European Space Agency 1 This page left intentionally blank 2 Mission Description Jupiter Icy Moons Explorer Key science goals The emergence of habitable worlds around gas giants Characterise Ganymede, Europa and Callisto as planetary objects and potential habitats Explore the Jupiter system as an archetype for gas giants Payload Ten instruments Laser Altimeter Radio Science Experiment Ice Penetrating Radar Visible-Infrared Hyperspectral Imaging Spectrometer Ultraviolet Imaging Spectrograph Imaging System Magnetometer Particle Package Submillimetre Wave Instrument Radio and Plasma Wave Instrument Overall mission profile 06/2022 - Launch by Ariane-5 ECA + EVEE Cruise 01/2030 - Jupiter orbit insertion Jupiter tour Transfer to Callisto (11 months) Europa phase: 2 Europa and 3 Callisto flybys (1 month) Jupiter High Latitude Phase: 9 Callisto flybys (9 months) Transfer to Ganymede (11 months) 09/2032 – Ganymede orbit insertion Ganymede tour Elliptical and high altitude circular phases (5 months) Low altitude (500 km) circular orbit (4 months) 06/2033 – End of nominal mission Spacecraft 3-axis stabilised Power: solar panels: ~900 W HGA: ~3 m, body fixed X and Ka bands Downlink ≥ 1.4 Gbit/day High Δv capability (2700 m/s) Radiation tolerance: 50 krad at equipment level Dry mass: ~1800 kg Ground TM stations ESTRAC network Key mission drivers Radiation tolerance and technology Power budget and solar arrays challenges Mass budget Responsibilities ESA: manufacturing, launch, operations of the spacecraft and data archiving PI Teams: science payload provision, operations, and data analysis 3 Foreword The JUICE (JUpiter ICy moon Explorer) mission, selected by ESA in May 2012 to be the first large mission within the Cosmic Vision Program 2015–2025, will provide the most comprehensive exploration to date of the Jovian system in all its complexity, with particular emphasis on Ganymede as a planetary body and potential habitat.
    [Show full text]
  • Development of Turbopump for LE-9 Engine
    Development of Turbopump for LE-9 Engine MIZUNO Tsutomu : P. E. Jp, Manager, Research & Engineering Development, Aero Engine, Space & Defense Business Area OGUCHI Hideo : Manager, Space Development Department, Aero Engine, Space & Defense Business Area NIIYAMA Kazuki : Ph. D., Manager, Space Development Department, Aero Engine, Space & Defense Business Area SHIMIYA Noriyuki : Space Development Department, Aero Engine, Space & Defense Business Area LE-9 is a new cryogenic booster engine with high performance, high reliability, and low cost, which is designed for H3 Rocket. It will be the first booster engine in the world with an expander bleed cycle. In the designing process, the performance requirements of the turbopump and other components can be concurrently evaluated by the mathematical model of the total engine system including evaluation with the simulated performance characteristic model of turbopump. This paper reports the design requirements of the LE-9 turbopump and their latest development status. Liquid oxygen 1. Introduction turbopump Liquid hydrogen The H3 rocket, intended to reduce cost and improve turbopump reliability with respect to the H-II A/B rockets currently in operation, is under development toward the launch of the first H3 test rocket in FY 2020. In rocket development, engine is an important factor determining reliability, cost, and performance, and as a new engine for the H3 rocket first stage, an LE-9 engine(1) is under development. A rocket engine uses a turbopump to raise the pressure of low-pressure propellant supplied from a tank, injects the pressurized propellant through an injector into a combustion chamber to combust it under high-temperature and high- pressure conditions.
    [Show full text]
  • The Titanic Origin of Humans: the Melian Nymphs and Zagreus Velvet Yates
    The Titanic Origin of Humans: The Melian Nymphs and Zagreus Velvet Yates HE FIRST PART of this paper examines a minor mystery in Hesiod’s Theogony, centering around the Melian Nymphs, Tin order to assess the suggestions, both ancient and modern, that the Melian Nymphs were the mothers of the human race. The second part examines the afterlife of Hesiod’s Melian Nymphs over a thousand years later, in the allegorizing myths of late Neoplatonism, in order to suggest that the Hesiodic myth in which the Melian Nymphs primarily figure, namely the castration of Ouranos, has close similarities to a central Neoplatonic myth, that of Zagreus. Both myths depict a “Titanic” act of destruction and separation which leads to the birth of the human race. Both myths furthermore seek to account for a divine element which human nature retains from its origins. The Melian Nymphs in Hesiod ˜ssai går =ayãmiggew ép°ssuyen aflmatÒessai, pãsaw d°jato Ga›a: periplom°nou d' §niautoË ge¤nat' ÉErinËw te krateråw megãlouw te G¤gantaw, teÊxesi lampom°nouw, dol¤x' ¶gxea xers‹n ¶xontaw, NÊmfaw y' ìw Mel¤aw kal°ous' §p' épe¤rona ga›an. Gaia took in all the bloody drops that spattered off, and as the seasons of the year turned round she bore the potent Furies and the Giants, immense, dazzling in their armor, holding long spears in their hands, and then she bore the Melian Nymphs on the boundless earth.1 1 Theog. 183–187. Translations of Hesiod adapted from A. Athanassakis, Hesiod: Theogony, Works and Days, Shield (Baltimore 1983).
    [Show full text]
  • Privacy Statement Link at the Bottom of Aerojet Rocketdyne Websites
    Privacy Notice Aerojet Rocketdyne – For external use Contents Introduction ...................................................................................................................... 3 Why we collect personal information? ............................................................................. 3 How we collect personal information? ............................................................................. 3 How we use information we collect? ............................................................................... 4 How we share your information? .................................................................................... 4 How we protect your personal information? ..................................................................... 4 How we collect consent? .............................................................................................. 4 How we provide you access? ........................................................................................ 4 How to contact Aerojet Rocketdyne privacy?.................................................................... 5 Collection of personal information .................................................................................. 5 Disclosure of personal information.................................................................................. 5 Sale of personal information .......................................................................................... 6 Children’s online privacy ..............................................................................................
    [Show full text]