Space Exploration and Development Systems (SEEDS) 2014
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Nasa Langley Research Center 2012
National Aeronautics and Space Administration NASA LANGLEY RESEARCH CENTER 2012 www.nasa.gov An Orion crew capsule test article moments before it is dropped into a An Atlantis flag flew outside Langley’s water basin at Langley to simulate an ocean splashdown. headquarters building during NASA’s final space shuttle mission in July. Launching a New Era of Exploration Welcome to Langley NASA Langley had a banner year in 2012 as we helped propel the nation toward a new age of air and space. From delivering on missions to creating new technologies and knowledge for space, aviation and science, Langley continued the rich tradition of innovation begun 95 years ago. Langley is providing leading-edge research and game-changing technology innovations for human space exploration. We are testing prototype articles of the Orion crew vehicle to optimize designs and improve landing systems for increased crew survivability. Langley has had a role in private-industry space exploration through agreements with SpaceX, Sierra Nevada Corp. and Boeing to provide engineering expertise, conduct testing and support research. Aerospace and Science With the rest of the world, we held our breath as the Curiosity rover landed on Mars – with Langley’s help. The Langley team performed millions of simulations of the entry, descent and landing phase of the Mars Science Laboratory mission to enable a perfect landing, Langley Center Director Lesa Roe and Mark Sirangelo, corporate and for the first time made temperature and pressure vice president and head of Sierra Nevada Space Systems, with measurements as the spacecraft descended, providing the Dream Chaser Space System model. -
Marathon 2,500 Years Edited by Christopher Carey & Michael Edwards
MARATHON 2,500 YEARS EDITED BY CHRISTOPHER CAREY & MICHAEL EDWARDS INSTITUTE OF CLASSICAL STUDIES SCHOOL OF ADVANCED STUDY UNIVERSITY OF LONDON MARATHON – 2,500 YEARS BULLETIN OF THE INSTITUTE OF CLASSICAL STUDIES SUPPLEMENT 124 DIRECTOR & GENERAL EDITOR: JOHN NORTH DIRECTOR OF PUBLICATIONS: RICHARD SIMPSON MARATHON – 2,500 YEARS PROCEEDINGS OF THE MARATHON CONFERENCE 2010 EDITED BY CHRISTOPHER CAREY & MICHAEL EDWARDS INSTITUTE OF CLASSICAL STUDIES SCHOOL OF ADVANCED STUDY UNIVERSITY OF LONDON 2013 The cover image shows Persian warriors at Ishtar Gate, from before the fourth century BC. Pergamon Museum/Vorderasiatisches Museum, Berlin. Photo Mohammed Shamma (2003). Used under CC‐BY terms. All rights reserved. This PDF edition published in 2019 First published in print in 2013 This book is published under a Creative Commons Attribution-NonCommercial- NoDerivatives (CC-BY-NC-ND 4.0) license. More information regarding CC licenses is available at http://creativecommons.org/licenses/ Available to download free at http://www.humanities-digital-library.org ISBN: 978-1-905670-81-9 (2019 PDF edition) DOI: 10.14296/1019.9781905670819 ISBN: 978-1-905670-52-9 (2013 paperback edition) ©2013 Institute of Classical Studies, University of London The right of contributors to be identified as the authors of the work published here has been asserted by them in accordance with the Copyright, Designs and Patents Act 1988. Designed and typeset at the Institute of Classical Studies TABLE OF CONTENTS Introductory note 1 P. J. Rhodes The battle of Marathon and modern scholarship 3 Christopher Pelling Herodotus’ Marathon 23 Peter Krentz Marathon and the development of the exclusive hoplite phalanx 35 Andrej Petrovic The battle of Marathon in pre-Herodotean sources: on Marathon verse-inscriptions (IG I3 503/504; Seg Lvi 430) 45 V. -
MULTIPHYSICS DESIGN and SIMULATION of a TUNGSTEN-CERMET NUCLEAR THERMAL ROCKET a Thesis by BRAD APPEL Submitted to the Office O
MULTIPHYSICS DESIGN AND SIMULATION OF A TUNGSTEN-CERMET NUCLEAR THERMAL ROCKET A Thesis by BRAD APPEL Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE August 2012 Major Subject: Nuclear Engineering Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket Copyright 2012 Brad Appel ii MULTIPHYSICS DESIGN AND SIMULATION OF A TUNGSTEN-CERMET NUCLEAR THERMAL ROCKET A Thesis by BRAD APPEL Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Approved by: Chair of Committee, Karen Vierow Committee Members, Shannon Bragg-Sitton Paul Cizmas Head of Department, Yassin Hassan August 2012 Major Subject: Nuclear Engineering iii iii ABSTRACT Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. (August 2012) Brad Appel, B.S., Purdue University Chair of Advisory Committee: Dr. Karen Vierow The goal of this research is to apply modern methods of analysis to the design of a tungsten-cermet Nuclear Thermal Rocket (NTR) core. An NTR is one of the most viable propulsion options for enabling piloted deep-space exploration. Concerns over fuel safety have sparked interest in an NTR core based on tungsten-cermet fuel. This work investigates the capability of modern CFD and neutronics codes to design a cermet NTR, and makes specific recommendations for the configuration of channels in the core. First, the best CFD practices available from the commercial package Star-CCM+ are determined by comparing different modeling options with a hot-hydrogen flow experiment. -
EDL – Lessons Learned and Recommendations
."#!(*"# 0 1(%"##" !)"#!(*"#* 0 1"!#"("#"#(-$" ."!##("""*#!#$*#( "" !#!#0 1%"#"! /!##"*!###"#" #"#!$#!##!("""-"!"##&!%%!%&# $!!# %"##"*!%#'##(#!"##"#!$$# /25-!&""$!)# %"##!""*&""#!$#$! !$# $##"##%#(# ! "#"-! *#"!,021 ""# !"$!+031 !" )!%+041 #!( !"!# #$!"+051 # #$! !%#-" $##"!#""#$#$! %"##"#!#(- IPPW Enabled International Collaborations in EDL – Lessons Learned and Recommendations: Ethiraj Venkatapathy1, Chief Technologist, Entry Systems and Technology Division, NASA ARC, 2 Ali Gülhan , Department Head, Supersonic and Hypersonic Technologies Department, DLR, Cologne, and Michelle Munk3, Principal Technologist, EDL, Space Technology Mission Directorate, NASA. 1 NASA Ames Research Center, Moffett Field, CA [email protected]. 2 Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), German Aerospace Center, [email protected] 3 NASA Langley Research Center, Hampron, VA. [email protected] Abstract of the Proposed Talk: One of the goals of IPPW has been to bring about international collaboration. Establishing collaboration, especially in the area of EDL, can present numerous frustrating challenges. IPPW presents opportunities to present advances in various technology areas. It allows for opportunity for general discussion. Evaluating collaboration potential requires open dialogue as to the needs of the parties and what critical capabilities each party possesses. Understanding opportunities for collaboration as well as the rules and regulations that govern collaboration are essential. The authors of this proposed talk have explored and established collaboration in multiple areas of interest to IPPW community. The authors will present examples that illustrate the motivations for the partnership, our common goals, and the unique capabilities of each party. The first example involves earth entry of a large asteroid and break-up. NASA Ames is leading an effort for the agency to assess and estimate the threat posed by large asteroids under the Asteroid Threat Assessment Project (ATAP). -
The J–2X Engine Powering NASA’S Ares I Upper Stage and Ares V Earth Departure Stage
The J–2X Engine Powering NASA’s Ares I Upper Stage and Ares V Earth Departure Stage The U.S. launch vehicles that will carry nozzle. It will weigh approximately 5,300 explorers back to the moon will be powered pounds. With 294,000 pounds of thrust, the in part by a J–2X engine that draws its engine will enable the Ares I upper stage to heritage from the Apollo-Saturn Program. place the Orion crew exploration vehicle in low-Earth orbit. The new engine, being designed and devel oped in support of NASA’s Constellation The J–2X is being designed by Pratt & Program, will power the upper stages of Whitney Rocketdyne of Canoga Park, Calif., both the Ares I crew launch vehicle and Ares for the Exploration Launch Projects Office at V cargo launch vehicle. NASA’s Marshall Space Flight Center in Huntsville, Ala. The J–2X builds on the The Constellation Program is responsible for legacy of the Apollo-Saturn Program and developing a new family of U.S. crew and relies on nearly a half-century of NASA launch vehicles and related systems and spaceflight experience, heritage hardware technologies for exploration of the moon, and technological advances. Mars and destinations beyond. Fueled with liquid oxygen and liquid hydro The J–2X will measure 185 inches long and gen, the J–2X is an evolved variation of two 120 inches in diameter at the end of its historic predecessors: the powerful J–2 upper stage engine that propelled the Apollo-era Shortly after J–2X engine cutoff, the Orion capsule will Saturn IB and Saturn V rockets to the moon in the separate from the upper stage. -
Jjmonl 1603.Pmd
alactic Observer GJohn J. McCarthy Observatory Volume 9, No. 3 March 2016 GRAIL - On the Trail of the Moon's Missing Mass GRAIL (Gravity Recovery and Interior Laboratory) was a NASA scientific mission in 2011/12 to map the surface of the moon and collect data on gravitational anomalies. The image here is an artist's impres- sion of the twin satellites (Ebb and Flow) orbiting in tandem above a gravitational image of the moon. See inside, page 4 for information on gravitational anomalies (mascons) or visit http://solarsystem. nasa.gov/grail. The John J. McCarthy Observatory Galactic Observer New Milford High School Editorial Committee 388 Danbury Road Managing Editor New Milford, CT 06776 Bill Cloutier Phone/Voice: (860) 210-4117 Production & Design Phone/Fax: (860) 354-1595 www.mccarthyobservatory.org Allan Ostergren Website Development JJMO Staff Marc Polansky It is through their efforts that the McCarthy Observatory Technical Support has established itself as a significant educational and Bob Lambert recreational resource within the western Connecticut Dr. Parker Moreland community. Steve Barone Jim Johnstone Colin Campbell Carly KleinStern Dennis Cartolano Bob Lambert Mike Chiarella Roger Moore Route Jeff Chodak Parker Moreland, PhD Bill Cloutier Allan Ostergren Cecilia Dietrich Marc Polansky Dirk Feather Joe Privitera Randy Fender Monty Robson Randy Finden Don Ross John Gebauer Gene Schilling Elaine Green Katie Shusdock Tina Hartzell Paul Woodell Tom Heydenburg Amy Ziffer In This Issue "OUT THE WINDOW ON YOUR LEFT" ............................... 4 SUNRISE AND SUNSET ...................................................... 13 MARE HUMBOLDTIANIUM AND THE NORTHEAST LIMB ......... 5 JUPITER AND ITS MOONS ................................................. 13 ONE YEAR IN SPACE ....................................................... 6 TRANSIT OF JUPITER'S RED SPOT .................................... -
Nagy Commentary on Euripides, Herakles
Informal Commentary on Euripides, Herakles by Gregory Nagy 97 The idea of returning from Hades implies a return from death 109f The mourning swan... Cf. the theme of the swansong. Cf. 692ff. 113 “The phantom of a dream”: cf. skias onar in Pindar Pythian 8. 131f “their father’s spirit flashing from their eyes”: beautiful rendition! 145f Herakles’ hoped-for return from Hades is equated with a return from death, with resurrection; see 297, where this theme becomes even more overt; also 427ff. 150 Herakles as the aristos man: not that he is regularly described in this drama as the best of all humans, not only of the “Greeks” (also at 183, 209). See also the note on 1306. 160 The description of the bow as “a coward’s weapon” is relevant to the Odysseus theme in the Odyssey 203 sôzein to sôma ‘save the body’... This expression seems traditional: if so, it may support the argument of some linguists that sôma ‘body’ is derived from sôzô ‘save’. By metonymy, the process of saving may extend to the organism that is destined to be saved. 270 The use of kleos in the wording of the chorus seems to refer to the name of Herakles; similarly in the wording of Megara at 288 and 290. Compare the notes on 1334 and 1369. 297 See at 145f above. Cf. the theme of Herakles’ wrestling with Thanatos in Euripides Alcestis. 342ff Note the god-hero antagonism as expressed by Amphitryon. His claim that he was superior to Zeus in aretê brings out the meaning of ‘striving’ in aretê (as a nomen actionis derived from arnumai; cf. -
Rideshare and the Orbital Maneuvering Vehicle: the Key to Low-Cost Lagrange-Point Missions
SSC15-II-5 Rideshare and the Orbital Maneuvering Vehicle: the Key to Low-cost Lagrange-point Missions Chris Pearson, Marissa Stender, Christopher Loghry, Joe Maly, Valentin Ivanitski Moog Integrated Systems 1113 Washington Avenue, Suite 300, Golden, CO, 80401; 303 216 9777, extension 204 [email protected] Mina Cappuccio, Darin Foreman, Ken Galal, David Mauro NASA Ames Research Center PO Box 1000, M/S 213-4, Moffett Field, CA 94035-1000; 650 604 1313 [email protected] Keats Wilkie, Paul Speth, Trevor Jackson, Will Scott NASA Langley Research Center 4 West Taylor Street, Mail Stop 230, Hampton, VA, 23681; 757 864 420 [email protected] ABSTRACT Rideshare is a well proven approach, in both LEO and GEO, enabling low-cost space access through splitting of launch charges between multiple passengers. Demand exists from users to operate payloads at Lagrange points, but a lack of regular rides results in a deficiency in rideshare opportunities. As a result, such mission architectures currently rely on a costly dedicated launch. NASA and Moog have jointly studied the technical feasibility, risk and cost of using an Orbital Maneuvering Vehicle (OMV) to offer Lagrange point rideshare opportunities. This OMV would be launched as a secondary passenger on a commercial rocket into Geostationary Transfer Orbit (GTO) and utilize the Moog ESPA secondary launch adapter. The OMV is effectively a free flying spacecraft comprising a full suite of avionics and a propulsion system capable of performing GTO to Lagrange point transfer via a weak stability boundary orbit. In addition to traditional OMV ’tug’ functionality, scenarios using the OMV to host payloads for operation at the Lagrange points have also been analyzed. -
IAF Space Propulsion Symposium 2019
IAF Space Propulsion Symposium 2019 Held at the 70th International Astronautical Congress (IAC 2019) Washington, DC, USA 21 -25 October 2019 Volume 1 of 2 ISBN: 978-1-7138-1491-7 Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 Some format issues inherent in the e-media version may also appear in this print version. Copyright© (2019) by International Astronautical Federation All rights reserved. Printed with permission by Curran Associates, Inc. (2020) For permission requests, please contact International Astronautical Federation at the address below. International Astronautical Federation 100 Avenue de Suffren 75015 Paris France Phone: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 www.iafastro.org Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 USA Phone: 845-758-0400 Fax: 845-758-2633 Email: [email protected] Web: www.proceedings.com TABLE OF CONTENTS VOLUME 1 PROPULSION SYSTEM (1) BLUE WHALE 1: A NEW DESIGN APPROACH FOR TURBOPUMPS AND FEED SYSTEM ELEMENTS ON SOUTH KOREAN MICRO LAUNCHERS ............................................................................ 1 Dongyoon Shin KEYNOTE: PROMETHEUS: PRECURSOR OF LOW-COST ROCKET ENGINE ......................................... 2 Jérôme Breteau ASSESSMENT OF MON-25/MMH PROPELLANT SYSTEM FOR DEEP-SPACE ENGINES ...................... 3 Huu Trinh 60 YEARS DLR LAMPOLDSHAUSEN – THE EUROPEAN RESEARCH AND TEST SITE FOR CHEMICAL SPACE PROPULSION SYSTEMS ....................................................................................... 9 Anja Frank, Marius Wilhelm, Stefan Schlechtriem FIRING TESTS OF LE-9 DEVELOPMENT ENGINE FOR H3 LAUNCH VEHICLE ................................... 24 Takenori Maeda, Takashi Tamura, Tadaoki Onga, Teiu Kobayashi, Koichi Okita DEVELOPMENT STATUS OF BOOSTER STAGE LIQUID ROCKET ENGINE OF KSLV-II PROGRAM ....................................................................................................................................................... -
Hesiod Theogony.Pdf
Hesiod (8th or 7th c. BC, composed in Greek) The Homeric epics, the Iliad and the Odyssey, are probably slightly earlier than Hesiod’s two surviving poems, the Works and Days and the Theogony. Yet in many ways Hesiod is the more important author for the study of Greek mythology. While Homer treats cer- tain aspects of the saga of the Trojan War, he makes no attempt at treating myth more generally. He often includes short digressions and tantalizes us with hints of a broader tra- dition, but much of this remains obscure. Hesiod, by contrast, sought in his Theogony to give a connected account of the creation of the universe. For the study of myth he is im- portant precisely because his is the oldest surviving attempt to treat systematically the mythical tradition from the first gods down to the great heroes. Also unlike the legendary Homer, Hesiod is for us an historical figure and a real per- sonality. His Works and Days contains a great deal of autobiographical information, in- cluding his birthplace (Ascra in Boiotia), where his father had come from (Cyme in Asia Minor), and the name of his brother (Perses), with whom he had a dispute that was the inspiration for composing the Works and Days. His exact date cannot be determined with precision, but there is general agreement that he lived in the 8th century or perhaps the early 7th century BC. His life, therefore, was approximately contemporaneous with the beginning of alphabetic writing in the Greek world. Although we do not know whether Hesiod himself employed this new invention in composing his poems, we can be certain that it was soon used to record and pass them on. -
The Advanced Cryogenic Evolved Stage (ACES)- a Low-Cost, Low-Risk Approach to Space Exploration Launch
The Advanced Cryogenic Evolved Stage (ACES)- A Low-Cost, Low-Risk Approach to Space Exploration Launch J. F. LeBar1 and E. C. Cady2 Boeing Phantom Works, Huntington Beach CA 92647 Space exploration top-level objectives have been defined with the United States first returning to the moon as a precursor to missions to Mars and beyond. System architecture studies are being conducted to develop the overall approach and define requirements for the various system elements, both Earth-to-orbit and in-space. One way of minimizing cost and risk is through the use of proven systems and/or multiple-use elements. Use of a Delta IV second stage derivative as a long duration in-space transportation stage offers cost, reliability, and performance advantages over earth-storable propellants and/or all new stages. The Delta IV second stage mission currently is measured in hours, and the various vehicle and propellant systems have been designed for these durations. In order for the ACES to have sufficient life to be useful as an Earth Departure Stage (EDS), many systems must be modified for long duration missions. One of the highest risk subsystems is the propellant storage Thermal Control System (TCS). The ACES effort concentrated on a lower risk passive TCS, the RL10 engine, and the other subsystems. An active TCS incorporating a cryocoolers was also studied. In addition, a number of computational models were developed to aid in the subsystem studies. The high performance TCS developed under ACES was simulated within the Delta IV thermal model and long-duration mission stage performance assessed. -
Short-Term Variability and Mass Loss in Be Stars I
A&A 588, A56 (2016) Astronomy DOI: 10.1051/0004-6361/201528026 & c ESO 2016 Astrophysics Short-term variability and mass loss in Be stars I. BRITE satellite photometry of η and μ Centauri D. Baade1, Th. Rivinius2, A. Pigulski3,A.C.Carciofi4, Ch. Martayan2,A.F.J.Moffat5,G.A.Wade6,W.W.Weiss7, J. Grunhut1, G. Handler8,R.Kuschnig9,7,A.Mehner2,H.Pablo5,A.Popowicz10,S.Rucinski11, and G. Whittaker11 1 European Organisation for Astronomical Research in the Southern Hemisphere (ESO), Karl-Schwarzschild-Str. 2, 85748 Garching, Germany e-mail: [email protected] 2 European Organisation for Astronomical Research in the Southern Hemisphere (ESO), Casilla 19001, Santiago 19, Chile 3 Astronomical Institute, Wrocław University, Kopernika 11, 51-622 Wrocław, Poland 4 Instituto de Astronomia, Geofísica e Ciências Atmosféricas, Universidade de São Paulo, Rua do Matão 1226, Cidade Universitária, 05508-900 São Paulo, SP, Brazil 5 Département de physique and Centre de Recherche en Astrophysique du Québec (CRAQ), Université de Montréal, CP 6128, Succ. Centre-Ville, Montréal, Québec, H3C 3J7, Canada 6 Department of Physics, Royal Military College of Canada, PO Box 17000, Stn Forces, Kingston, Ontario K7K 7B4, Canada 7 Institute of Astronomy, University of Vienna, Universitätsring 1, 1010 Vienna, Austria 8 Nicolaus Copernicus Astronomical Center, ul. Bartycka 18, 00-716 Warsaw, Poland 9 Department of Physics and Astronomy, University of British Columbia, Vancouver, BC V6T1Z1, Canada 10 Institute of Automatic Control, Silesian University of Technology, Gliwice, Poland 11 Department of Astronomy & Astrophysics, University of Toronto, 50 St. George St, Toronto, Ontario, M5S 3H4, Canada Received 21 December 2015 / Accepted 1 February 2016 ABSTRACT Context.