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Galaktika Group: Orbital City «EFIR» «Ethereal Dwelling» Space Colony Concept by Tsiolkovsky
Galaktika group: Orbital city «EFIR» «ethereal dwelling» space colony concept by tsiolkovsky BASIC PRINCIPLES OF CONSTRUCTING A SPACE COLONY UPON THE CONCEPT BY K.E. TSIOLKOVSKY: IN-SPACE ASSEMBLING MANKIND WILL NOT FOREVER REMAIN ON EARTH, BUT IN THE PURSUIT OF LIGHT AND SPACE WILL FIRST USING MATERIALS FROM PLANETS AND ASTEROIDS TIMIDLY EMERGE FROM THE BOUNDS OF THE ATMOSPHERE, AND THEN ADVANCE UNTIL HE HAS CONQUERED THE WHOLE ARTIFICIAL GRAVITY OF CIRCUMSOLAR SPACE. PLANTS CULTIVATION HE PRESENTED HIS RESEARCHES IN THE BOOKS: BEYOND THE PLANET EARTH, BIOLOGICAL LIFE IN COSMOS, ETHEREAL ISLAND, ETC. COLONY CONCEPTS [SHORT] REVIEW BERNAL'S SPHERE, STANFORD TORUS, O’NEILL’S CYLINDER BERNAL’S SPHERE STANFORD TORUS O’NEILL’S CYLINDER JOHN DESMOND BERNAL 1929 POPULATION: STUDENTS OF THE STANFORD UNIVERSITY 1975 GERARD K. O'NEILL, 1979 POPULATION: 20 MLN. 20—30 THOUSAND INHABITANTS DIAMETER POPULATION: 10 THND. AND MORE INHABITANTS INHABITANTS DIAMETER OF CYLINDERS: 6.4 KM ABOUT 16 KM DIAMETER1.8KM AND MORE LENGTH OF CYLINDERS: 32 KM ORBITAL CITY «EFIR» scheme and characteristics TOP VIEW residential torus ASSEMBLY DOCK radiators electric power station elevator 10,000 INHABITANTS DIAMETER OF TORUS – 2 KILOMETRES variable gravity module MASS OF ORBITAL CITY – 25 MLN. TONS RESIDENTIAL AREA DESCRIPTION OF THE INTERIOR AREA RESIDENTIAL AREA CHARACTERISTICS DIAMETER OF TORUS - 2 KILOMETRES ROTATION PERIOD - ONE FULL-CIRCLE TURN PER 63 SECONDS RESIDENTIAL AREA WIDTH - 300 METERS RESIDENTIAL AREA HEIGHT - 150 METERS AREA OF RESIDENTIAL ZONE - 200 HA MAXIMUM POPULATION - 10-40 THOUSAND DESIGNED POPULATION DENSITY IS 50 PEOPLE/HA TO 200 PEOPLE/HA RESIDENTIAL AREA DESCRIPTION OF THE INTERIOR AREA LOGISTICS transport plans for passengers and cargoes ORBITAL CITY AT THE LAGRANGIAN POINT INTERPLANETARY 25 MLN. -
General Issue
Journal of the British Interplanetary Society VOLUME 72 NO.5 MAY 2019 General issue A REACTION DRIVE Powered by External Dynamic Pressure Jeffrey K. Greason DOCKING WITH ROTATING SPACE SYSTEMS Mark Hempsell MARTIAN DUST: the Formation, Composition, Toxicology, Astronaut Exposure Health Risks and Measures to Mitigate Exposure John Cain THE CONCEPT OF A LOW COST SPACE MISSION to Measure “Big G” Roger Longstaff www.bis-space.com ISSN 0007-084X PUBLICATION DATE: 26 JULY 2019 Submitting papers International Advisory Board to JBIS JBIS welcomes the submission of technical Rachel Armstrong, Newcastle University, UK papers for publication dealing with technical Peter Bainum, Howard University, USA reviews, research, technology and engineering in astronautics and related fields. Stephen Baxter, Science & Science Fiction Writer, UK James Benford, Microwave Sciences, California, USA Text should be: James Biggs, The University of Strathclyde, UK ■ As concise as the content allows – typically 5,000 to 6,000 words. Shorter papers (Technical Notes) Anu Bowman, Foundation for Enterprise Development, California, USA will also be considered; longer papers will only Gerald Cleaver, Baylor University, USA be considered in exceptional circumstances – for Charles Cockell, University of Edinburgh, UK example, in the case of a major subject review. Ian A. Crawford, Birkbeck College London, UK ■ Source references should be inserted in the text in square brackets – [1] – and then listed at the Adam Crowl, Icarus Interstellar, Australia end of the paper. Eric W. Davis, Institute for Advanced Studies at Austin, USA ■ Illustration references should be cited in Kathryn Denning, York University, Toronto, Canada numerical order in the text; those not cited in the Martyn Fogg, Probability Research Group, UK text risk omission. -
Deuterium – Tritium Pulse Propulsion with Hydrogen As Propellant and the Entire Space-Craft As a Gigavolt Capacitor for Ignition
Deuterium – Tritium pulse propulsion with hydrogen as propellant and the entire space-craft as a gigavolt capacitor for ignition. By F. Winterberg University of Nevada, Reno Abstract A deuterium-tritium (DT) nuclear pulse propulsion concept for fast interplanetary transport is proposed utilizing almost all the energy for thrust and without the need for a large radiator: 1. By letting the thermonuclear micro-explosion take place in the center of a liquid hydrogen sphere with the radius of the sphere large enough to slow down and absorb the neutrons of the DT fusion reaction, heating the hydrogen to a fully ionized plasma at a temperature of ~ 105 K. 2. By using the entire spacecraft as a magnetically insulated gigavolt capacitor, igniting the DT micro-explosion with an intense GeV ion beam discharging the gigavolt capacitor, possible if the space craft has the topology of a torus. 1. Introduction The idea to use the 80% of the neutron energy released in the DT fusion reaction for nuclear micro-bomb rocket propulsion, by surrounding the micro-explosion with a thick layer of liquid hydrogen heated up to 105 K thereby becoming part of the exhaust, was first proposed by the author in 1971 [1]. Unlike the Orion pusher plate concept, the fire ball of the fully ionized hydrogen plasma can here be reflected by a magnetic mirror. The 80% of the energy released into 14MeV neutrons cannot be reflected by a magnetic mirror for thermonuclear micro-bomb propulsion. This was the reason why for the Project Daedalus interstellar probe study of the British Interplanetary Society [2], the neutron poor deuterium-helium 3 (DHe3) reaction was chosen. -
Location #1: Peary/Whipple Crater
Location, Location, Location A Lunar Investment Strategy Hoyt Davidson Near Earth LLC June 2017 ISU's International Institute of Space Commerce Lunar Economic Action Plan (LEAP) Space and Questions from 1960 Still Relevant Today Economic Development • How can we utilize our dynamic system of competitive private enterprise in space, as on earth, to make newly discovered resources useful to man? • How can private enterprise and private capital make their maximum contribution? Philosophy and Policy The ultimate goal is not to impress others, or merely to explore our planetary system, but to use accessible space for the benefit of humankind. It is a goal that is not confined to a decade or a century. Nor is it confined to a single nearby destination, or to a fleeting dash to plant a flag. The idea is to begin preparing now for a future in which the material trapped in the Sun's vicinity is available for incorporation into our way of life. Dr. John Marburger, Head of the Office of Science and Technology Policy 2006 3 The Investment Premise • Just as on Earth, lunar real estate “value” is driven by location, location, location Rank Location Why Valuable 1 Peary Crater Best 1st industrial base and settlement 2 Sinus Medii Good cargo port & space elevator site 3 Largest skylights / lava tubes Best large scale settlements 4 Tsiolkovskiy crater, dark side Prime radio astronomy site 5 High helium-3 concentrations Potential high value mining 6 Lipsky Crater Space elevator site for Earth-Moon L2 7 Aristillus High Thorium concentrations • Lunar real -
California State University, Northridge Low Earth Orbit
CALIFORNIA STATE UNIVERSITY, NORTHRIDGE LOW EARTH ORBIT BUSINESS CENTER A Project submitted in partial satisfaction of the requirements for the degree of Master of Science in Engineering by Dallas Gene Bienhoff May 1985 The Proj'ectof Dallas Gene Bienhoff is approved: Dr. B. J. Bluth Professor T1mothy Wm. Fox - Chair California State University, Northridge ii iii ACKNOWLEDGEHENTS I wish to express my gratitude to those who have helped me over the years to complete this thesis by providing encouragement, prodding and understanding: my advisor, Tim Fox, Chair of Mechanical and Chemical Engineering; Dr. B. J. Bluth for her excellent comments on human factors; Dr. B. J. Campbell for improving the clarity; Richard Swaim, design engineer at Rocketdyne Division of Rockwell International for providing excellent engineering drawings of LEOBC; Mike Morrow, of the Advanced Engineering Department at Rockwell International who provided the Low Earth Orbit Business Center panel figures; Bob Bovill, a commercial artist, who did all the artistic drawings because of his interest in space commercialization; Linda Martin for her word processing skills; my wife, Yolanda, for egging me on without nagging; and finally Erik and Danielle for putting up with the excuse, "I have to v10rk on my paper," for too many years. iv 0 ' PREFACE The Low Earth Orbit Business Center (LEOBC) was initially conceived as a modular structure to be launched aboard the Space Shuttle, it evolved to its present configuration as a result of research, discussions and the desire to increase the efficiency of space utilization. Although the idea of placing space stations into Earth orbit is not new, as is discussed in the first chapter, and the configuration offers nothing new, LEOBC is unique in its application. -
OMNI Magazine, Captured on Film by Photographer PO
THE STAR ENGINE: UPHILL SKIING: THE LYING IN WAIT ALL-NEW SPORT FOR HALLEY'S COMET OF GRAVITY EVASION SPACEWALKING HOW OBSOLETE IS AT17000 MPH MODERN MEDICINE? THE VISIONARY WORLD GAMES TO PLAY OF THEODORE STURGEON ON YOUR CALCULATOR alb Dnnrui'FEBRUARY 1980 EDITOR & DESIGN DIRECTOR: BOB GUCCIONE EXECUTIVE EDITOR' BEN BOVA ART DIRECTOR: FRANK DEVINO MANAGING EDITOR. J. ANDERSON DORMAN FICTION EDITOR: ROBERT SHECKLEY EUROPEAN EDITOR. DR. BERNARD DIXON DIRECTOR OF ADVERTISING: BEVERLEY WARDALE EXECUTIVE VICE-PRESIDENT: IRWIN E BILLMAN ASSOCIATE PUBLISHER: KATHY KEETON ASSOCIATE PUBLISHER (INT'L): FRANCO ROSSELLIN CONTENTS PAGE FIRST WORD Opinion Ben Bova 6 OMNIBUS Contributors 8 COMMUNICATIONS Correspondence 10 FORUM Dialogue 14 EARTH Environment Kenneth Brower 17 SPACE Astronomy MarkR. Chartrand II 20 LIFE Biomedicine Bernard Dixon 22 FILM The Arts James Delson 24 MUSIC The Arts Sam Bruskin 26 UFO UPDATE Report James Oberg 32 CONTINUUM Data Bank 35 ORTHOHEALING Article Belinda Dumont 44 MESSAGE FROM EARTH Fiction an Stewart 50 COMET CATCHER Article Robert L. Forward 54 WHY DOLPHINS DONT BITE Fiction Theodore Sturgeon 62 INFINITE VOYAGER Pictorial ' F C. Durant III 68 ARNO PENZIAS Interview Monte Davis 78 UPHILL SKIING Pictorial Matthias Wendt 82 THE PRESIDENT'S IMAGE Fiction Stephen Robinett 88 FUTURE CURVES Article Bernard Dixon and John Gribbin 92 PEOPLE Names and Faces Dick Teresi 119 EXPLORATIONS Travel K. C. Cole 123 COMPUTER GRAPHICS Phenomena 126 GAMES Diversions Scot Morns 128 LAST WORD Opinion Daniel S. Greenberg 130 PHOTO CREDITS 124 :;>- P..c ln.emator.3l L;;:l Ah ngnts reserved Cover art for this month's Omni OMNI, 1980 (ISSN 0149-8711). -
Space Propulsion.Pdf
Deep Space Propulsion K.F. Long Deep Space Propulsion A Roadmap to Interstellar Flight K.F. Long Bsc, Msc, CPhys Vice President (Europe), Icarus Interstellar Fellow British Interplanetary Society Berkshire, UK ISBN 978-1-4614-0606-8 e-ISBN 978-1-4614-0607-5 DOI 10.1007/978-1-4614-0607-5 Springer New York Dordrecht Heidelberg London Library of Congress Control Number: 2011937235 # Springer Science+Business Media, LLC 2012 All rights reserved. This work may not be translated or copied in whole or in part without the written permission of the publisher (Springer Science+Business Media, LLC, 233 Spring Street, New York, NY 10013, USA), except for brief excerpts in connection with reviews or scholarly analysis. Use in connection with any form of information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed is forbidden. The use in this publication of trade names, trademarks, service marks, and similar terms, even if they are not identified as such, is not to be taken as an expression of opinion as to whether or not they are subject to proprietary rights. Printed on acid-free paper Springer is part of Springer Science+Business Media (www.springer.com) This book is dedicated to three people who have had the biggest influence on my life. My wife Gemma Long for your continued love and companionship; my mentor Jonathan Brooks for your guidance and wisdom; my hero Sir Arthur C. Clarke for your inspirational vision – for Rama, 2001, and the books you leave behind. Foreword We live in a time of troubles. -
Public Taste: a Comparison of Movie Popularity and Critical Opinion
W&M ScholarWorks Dissertations, Theses, and Masters Projects Theses, Dissertations, & Master Projects 1982 Public taste: A comparison of movie popularity and critical opinion R. Claiborne Riley College of William & Mary - Arts & Sciences Follow this and additional works at: https://scholarworks.wm.edu/etd Part of the Film and Media Studies Commons Recommended Citation Riley, R. Claiborne, "Public taste: A comparison of movie popularity and critical opinion" (1982). Dissertations, Theses, and Masters Projects. Paper 1539625207. https://dx.doi.org/doi:10.21220/s2-hqz7-rj05 This Thesis is brought to you for free and open access by the Theses, Dissertations, & Master Projects at W&M ScholarWorks. It has been accepted for inclusion in Dissertations, Theses, and Masters Projects by an authorized administrator of W&M ScholarWorks. For more information, please contact [email protected]. PUBLIC TASTE: A COMPARISON OF MOVIE u POPULARITY AND CRITICAL OPINION A Thesis Presented to The Faculty of the Department of Sociology The College of William, and Mary in Virginia In Partial Fulfillment Of the Requirements for the Degree of Master of Arts by R. Claiborne Riley 1982 APPROVAL SHEET This thesis is submitted in partial fulfillment the requirements for the degree of Master of Arts R. Claiborne Riley Approved, September 1982 r**1. r i m f Satoshi Ito JL R. Wayne Kernodle Marion G. Vanfossen TABLE OF CONTENTS Page ACKNOWLEDGMENTS .......... iv LIST OF TABLES . ..... .... ..................... v ABSTRACT .......... '......... vi INTRODUCTION .......... ...... 2 Chapter I. THE MOVIES: AN HISTORICAL PERSPECTIVE .............. 6 Chapter II. THE AUDIENCE ........................................ 51 Chapter III. THE C R I T I C ............ 61 Chapter IV. THE WANDERER STUDY AND DUMAZEDIER ON MOVIES AND LEISURE ....... -
October 9, 2012 (XXV:6) David Miller, LONELY ARE the BRAVE (1962, 107 Min)
October 9, 2012 (XXV:6) David Miller, LONELY ARE THE BRAVE (1962, 107 min) Directed by David Miller Screenplay by Dalton Trumbo Based on the novel, The Brave Cowboy, by Edward Abbey Produced by Edward Lewis Original Music by Jerry Goldsmith Cinematography by Philip H. Lathrop Film Editing by Leon Barsha Art Direction by Alexander Golitzen and Robert Emmet Smith Set Decoration by George Milo Makeup by Larry Germain, Dave Grayson, and Bud Westmore Kirk Douglas…John W. "Jack" Burns Gena Rowlands…Jerry Bondi Walter Matthau…Sheriff Morey Johnson Michael Kane…Paul Bondi Carroll O'Connor…Hinton William Schallert…Harry George Kennedy…Deputy Sheriff Gutierrez Karl Swenson…Rev. Hoskins William Mims…First Deputy Arraigning Burns Martin Garralaga…Old Man Lalo Rios…Prisoner Bill Bixby…Airman in Helicopter Bill Raisch…One Arm Table Tennis, 1936 Let's Dance, 1935 A Sports Parade Subject: Crew DAVID MILLER (November 28, 1909, Paterson, New Jersey – April Racing, and 1935 Trained Hoofs. 14, 1992, Los Angeles, California) has 52 directing credits, among them 1981 “Goldie and the Boxer Go to Hollywood”, 1979 “Goldie DALTON TRUMBO (James Dalton Trumbo, December 9, 1905, and the Boxer”, 1979 “Love for Rent”, 1979 “The Best Place to Be”, Montrose, Colorado – September 10, 1976, Los Angeles, California) 1976 Bittersweet Love, 1973 Executive Action, 1969 Hail, Hero!, won best writing Oscars for The Brave One (1956) and Roman 1968 Hammerhead, 1963 Captain Newman, M.D., 1962 Lonely Are Holiday (1953). He was blacklisted for many years and, until Kirk the Brave, 1961 Back Street, 1960 Midnight Lace, 1959 Happy Douglas insisted he be given screen credit for Spartacus was often to Anniversary, 1957 The Story of Esther Costello, 1956 Diane, 1951 write under a pseudonym. -
A New Vision for Fusion Energy Research: Fusion Rocket Engines for Planetary Defense Abstract We Argue That It Is Essential Fo
LA-UR-15-23198 A New Vision for Fusion Energy Research: Fusion Rocket Engines for Planetary Defense G. A. Wurden1, T. E. Weber1, P. J. Turchi2, P. B. Parks3, T. E. Evans3, S. A. Cohen4, J. T. Cassibry5, E. M. Campbell6 1Los Alamos National Laboratory 2Santa Fe, NM 3General Atomics 4Princeton Plasma Physics Laboratory 5University of Alabama, Huntsville 6Sandia National Laboratory Abstract We argue that it is essential for the fusion energy program to identify an imagination- capturing critical mission by developing a unique product which could command the marketplace. We lay out the logic that this product is a fusion rocket engine, to enable a rapid response capable of deflecting an incoming comet, to prevent its impact on the planet Earth, in defense of our population, infrastructure, and civilization. As a side benefit, deep space solar system exploration, with greater speed and orders-of-magnitude greater payload mass would also be possible. The US Department of Energy’s magnetic fusion research program, based in its Office of Science, focuses on plasma and fusion science1 to support the long term goal of environmentally friendly, socially acceptable, and economically viable electricity production from fusion reactors.2 For several decades the US magnetic fusion program has had to deal with a lack of urgency towards and inconsistent funding for this ambitious goal. In many American circles, fusion isn’t even at the table3 when it comes to discussing future energy production. Is there another, more urgent, unique, and even more important application for fusion? Fusion’s unique application As an on-board power source and thruster for fast propulsion in space,4 a fusion reactor would provide unparalleled performance (high specific impulse and high specific power) for a spacecraft. -
Surveyor 1 Space- Craft on June 2, 1966 As Seen by the Narrow Angle Camera of the Lunar Re- Connaissance Orbiter Taken on July 17, 2009 (Also See Fig
i “Project Surveyor, in particular, removed any doubt that it was possible for Americans to land on the Moon and explore its surface.” — Harrison H. Schmitt, Apollo 17 Scientist-Astronaut ii Frontispiece: Landing site of the Surveyor 1 space- craft on June 2, 1966 as seen by the narrow angle camera of the Lunar Re- connaissance Orbiter taken on July 17, 2009 (also see Fig. 13). The white square in the upper photo outlines the area of the enlarged view below. The spacecraft is ca. 3.3 m tall and is casting a 15 m shadow to the East. (NASA/LROC/ ASU/GSFC photos) iii iv Surveyor I: America’s First Moon Landing by William F. Mellberg v © 2014, 2015 William F. Mellberg vi About the author: William Mellberg was a marketing and public relations representative with Fokker Aircraft. He is also an aerospace historian, having published many articles on both the development of airplanes and space vehicles in various magazines. He is the author of Famous Airliners and Moon Missions. He also serves as co-Editor of Harrison H. Schmitt’s website: http://americasuncommonsense.com Acknowledgments: The support and recollections of Frank Mellberg, Harrison Schmitt, Justin Rennilson, Alexander Gurshstein, Paul Spudis, Ronald Wells, Colin Mackellar and Dwight Steven- Boniecki is gratefully acknowledged. vii Surveyor I: America’s First Moon Landing by William F. Mellberg A Journey of 250,000 Miles . December 14, 2013. China’s Chang’e 3 spacecraft successfully touched down on the Moon at 1311 GMT (2111 Beijing Time). The landing site was in Mare Imbrium, the Sea of Rains, about 25 miles (40 km) south of the small crater, Laplace F, and roughly 100 miles (160 km) east of its original target in Sinus Iridum, the Bay of Rainbows. -
Fusion Rockets for Planetary Defense
| Los Alamos National Laboratory | Fusion Rockets for Planetary Defense Glen Wurden Los Alamos National Laboratory PPPL Colloquium March 16, 2016 LA-UR-16-21396 LA-UR-15-xxxx UNCLASSIFIED Operated by Los Alamos National Security, LLC for the U.S. Department of Energy's NNSA | Los Alamos National Laboratory | My collaborators on this topic: T. E. Weber1, P. J. Turchi2, P. B. Parks3, T. E. Evans3, S. A. Cohen4, J. T. Cassibry5, E. M. Campbell6 . 1Los Alamos National Laboratory . 2Santa Fe, NM . 3General Atomics . 4Princeton Plasma Physics Laboratory . 5University of Alabama, Huntsville . 6LLE, University of Rochester, Rochester Wurden et al., Journal of Fusion Energy, Vol. 35, 1, 123 (2016) UNCLASSIFIED Operated by Los Alamos National Security, LLC for the U.S. Department of Energy's NNSA | Los Alamos National Laboratory | How many ways is electricity made today? Primary Energy Source Nominally CO2 Free Current capacity (%) Expected Lifetime (yrs) Natural Gas no 100 Coal no 80.6 400 Oil no < 50 Biomass neutral 11.4 > 400 Wind yes 0.5 > 1000 Solar photovoltaic yes 0.06 > 1000 Solar thermal yes 0.17 > 1000 Hydro yes 3.3 > 1000 Wave/Tidal yes 0.001 > 1000 Geothermal yes 0.12 > 1000 Nuclear fission yes 2.7 > 400 [i] REN21–Renewable Energy Policy Network for the 21st Century Renewables 2012–Global Status Report, 2012, http://www.map.ren21.net/GSR/GSR2012.pdf , http://en.wikipedia.org/wiki/Energy_development UNCLASSIFIED Operated by Los Alamos National Security, LLC for the U.S. Department of Energy's NNSA | Los Alamos National Laboratory | What is the most important product that fusion could deliver? .