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Enabling Sustainable Exploration Through the Commercial Development of Space
54th International Astronautical Congress 2003 (IAC 2003) Bremen, Germany 29 September - 3 October 2003 Volume 1 of 8 ISBN: 978-1-61839-418-7 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© (2003) by the International Astronautical Federation All rights reserved. Printed by Curran Associates, Inc. (2012) For permission requests, please contact the International Astronautical Federation at the address below. International Astronautical Federation 94 bis, Avenue de Suffren 75015 PARIS - France Phone: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 [email protected] Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 USA Phone: 845-758-0400 Fax: 845-758-2634 Email: [email protected] Web: www.proceedings.com TABLE OF CONTENTS VOLUME 1 Enabling Sustainable Exploration through the Commercial Development of Space .................................................................................1 Mark Nall, Joseph Casas Space Telescope Mission Design For L2 Point Stationing .............................................................................................................................6 Jill M. Cattrysse Interplanetary Missions Utilising Capture and Escape Through Lagrange Points..................................................................................14 Stephen Kemble A Numerical Study of the Gravitational -
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects NASA Grant No. NNX17AE81G First Year Report Prepared by: Marc G. Millis, Jeff Greason, Rhonda Stevenson Tau Zero Foundation Business Office: 1053 East Third Avenue Broomfield, CO 80020 Prepared for: NASA Headquarters, Space Technology Mission Directorate (STMD) and NASA Innovative Advanced Concepts (NIAC) Washington, DC 20546 June 2018 Millis 2018 Grant NNX17AE81G_for_CR.docx pg 1 of 69 ABSTRACT Progress toward developing an evaluation process for interstellar propulsion and power options is described. The goal is to contrast the challenges, mission choices, and emerging prospects for propulsion and power, to identify which prospects might be more advantageous and under what circumstances, and to identify which technology details might have greater impacts. Unlike prior studies, the infrastructure expenses and prospects for breakthrough advances are included. This first year's focus is on determining the key questions to enable the analysis. Accordingly, a work breakdown structure to organize the information and associated list of variables is offered. A flow diagram of the basic analysis is presented, as well as more detailed methods to convert the performance measures of disparate propulsion methods into common measures of energy, mass, time, and power. Other methods for equitable comparisons include evaluating the prospects under the same assumptions of payload, mission trajectory, and available energy. Missions are divided into three eras of readiness (precursors, era of infrastructure, and era of breakthroughs) as a first step before proceeding to include comparisons of technology advancement rates. Final evaluation "figures of merit" are offered. Preliminary lists of mission architectures and propulsion prospects are provided. -
Review of Laser Lightcraft Propulsion System (Preprint) 5B
This document is made available through the declassification efforts and research of John Greenewald, Jr., creator of: The Black Vault The Black Vault is the largest online Freedom of Information Act (FOIA) document clearinghouse in the world. The research efforts here are responsible for the declassification of hundreds of thousands of pages released by the U.S. Government & Military. Discover the Truth at: http://www.theblackvault.com Form Approved REPORT DOCUMENTATION PAGE OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing this collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. PLEASE DO NOT RETURN YOUR FORM TO THE ABOVE ADDRESS. 1. REPORT DATE (DD-MM-YYYY) 2. REPORT TYPE 3. DATES COVERED (From - To) 16-10-2007 Technical Paper 4. TITLE AND SUBTITLE 5a. CONTRACT NUMBER Review of Laser Lightcraft Propulsion System (Preprint) 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER 6. AUTHOR(S) 5d. PROJECT NUMBER Eric Davis (Institute for Advanced Studies at Austin); Franklin Mead (AFRL/RZSP) 48470159 5e. -
Review: Laser-Ablation Propulsion
JOURNAL OF PROPULSION AND POWER Vol. 26, No. 4, July–August 2010 Review: Laser-Ablation Propulsion Claude Phipps Photonic Associates, LLC, Santa Fe, New Mexico 87508 Mitat Birkan U.S. Air Force Office of Scientific Research, Arlington, VA 22203-1768 Willy Bohn BohnLaser Consult, 70569 Stuttgart, Germany Hans-Albert Eckel DLR, German Aerospace Center, 70569 Stuttgart, Germany Hideyuki Horisawa Tokai University, Hiratsuka 259-1292, Japan Thomas Lippert Paul Scherrer Institut, 5232 Villigen PSI Switzerland Max Michaelis University of KwaZulu–Natal, Durban 4001, South Africa Yuri Rezunkov Sosnovy Bor, Leningrad Region, Russia Akihiro Sasoh Nagoya University, Nagoya 464-8603, Japan Wolfgang Schall 71111 Waldenbuch, Germany Stefan Scharring DLR, German Aerospace Center, 70569 Stuttgart, Germany and John Sinko Kratos Defense and Security Solutions, Inc., Huntsville, Alabama 35805 DOI: 10.2514/1.43733 Claude Phipps earned B.S. and M.S. degrees from Massachusetts Institute of Technology and a Ph.D. from Stanford University in 1972. He worked in the Inertial Confinement Fusion Program at Lawrence Livermore Laboratory for two years and, since 1974, as a Senior Research Staff Member in the Advanced Optical Systems Group at Los Alamos (LANL). There, he conducted a research program on mechanical and thermal coupling of pulsed lasers to targets using high-energy-laser facilities in the United States and United Kingdom, and he developed a model for vacuum laser impulse prediction. From 1994 to 1995, he was Associate Director of the Alliance for Photonic Technology at LANL. In 1995, he formed Photonic Associates, which is devoted to applications of laser space propulsion. He is the author of 110 papers and 40 invited talks and an editor of a book on laser ablation, and he has been the organizer and chair of seven symposia on high-power laser ablation. -
Nasa and the Search for Technosignatures
NASA AND THE SEARCH FOR TECHNOSIGNATURES A Report from the NASA Technosignatures Workshop NOVEMBER 28, 2018 NASA TECHNOSIGNATURES WORKSHOP REPORT CONTENTS 1 INTRODUCTION .................................................................................................................................................................... 1 What are Technosignatures? .................................................................................................................................... 2 What Are Good Technosignatures to Look For? ....................................................................................................... 2 Maturity of the Field ................................................................................................................................................... 5 Breadth of the Field ................................................................................................................................................... 5 Limitations of This Document .................................................................................................................................... 6 Authors of This Document ......................................................................................................................................... 6 2 EXISTING UPPER LIMITS ON TECHNOSIGNATURES ....................................................................................................... 9 Limits and the Limitations of Limits ........................................................................................................................... -
Here Walking Fossil Robert A
The Anticipation Hugo Committee is pleased to provide a detailed list of nominees for the 2009 Science Fiction and Fantasy Achievement Awards (the Hugos), and the John W. Campbell Award for Best New Writer (Sponsored by Dell Magazines). Each category is delineated to five nominees, per the WSFS Constitution. Also provided are the number of ballots with nominations, the total number of nominations and the number of unique nominations in each category. Novel The Last Centurion John Ringo 8 Once Upon a Time Philip Pullman 10 Ballots 639; Nominations: 1990; Unique: 335 The Mirrored Heavens David Williams 8 in the North Slow Train to Arcturus Dave Freer 7 To Hie from Far Cilenia Karl Schroeder 9 Little Brother Cory Doctorow 129 Hunter’s Run Martin Dozois Abraham 7 Pinocchio Walter Jon Williams 9 Anathem Neal Stephenson 93 Inside Straight George R. R. Martin 7 Utere Nihill Non Extra John Scalzi 9 The Graveyard Book Neil Gaiman 82 The Ashes of Worlds Kevin J Anderson 7 Quiritationem Suis Saturn’s Children Charles Stross 74 Gentleman Takes Sarah A Hoyt 7 Harvest James Van Pelt 9 Zoe’s Tale John Scalzi 54 a Chance The Inferior Peadar O’Guilin 7 Cenotaxis Sean Williams 9 Matter Iain M. Banks 49 Staked J.F. Lewis 7 In the Forests of Jay Lake 8 Nation Terry Pratchett 46 Graceling Kristin Cashore 6 the Night An Autumn War Daniel Abraham 46 Small Favor Jim Butcher 6 Black Petals Michael Moorcock 8 Implied Spaces Walter Jon Williams 45 Emissaries From Adam-Troy Castro 6 Political Science by Walton (Bud) Simons 7 Pirate Sun Karl Schroeder 41 the Dead & Ian Tregillis Half a Crown Jo Walton 38 A World Too Near Kay Kenyon 6 Mystery Hill Alex Irvine 7 Valley of Day-Glo Nick Dichario 35 Slanted Jack Mark L. -
Johnny Says... Star Wars - Episode 1 the Over-Hyped Menace Page 9 WCSFA Memberships Wcsfactivities New
Vol. 27 Issue 5se Number 312se May 1999 Free Johnny Says... Star Wars - Episode 1 The Over-Hyped Menace Page 9 WCSFA Memberships WCSFActivities New ...................................... $26.00 New Family .......................... $32.00 F.R.E.D. - Every Friday tions of where to eat next.Stepho’s 1124 Davie Renewal ................................ $25.00 The weekly gathering of BCSFAns and all St., Vancouver. An inexpensively perfect place Family (2 Votes) ................... $31.00 (Above prices includes subscription to others interested in joining us for an evening for a VCON postmortem. BCSFAzine. Please e-mail of conversation and relaxation, with pool Saturday June 12th (Saturday) WCSFA Video [email protected] if you wish to table option. At the Burrard Motor Inn oposite Night. Featuring a selection by R. Graeme receive the magazine electronically.) St. Paul’s Hospital (Downtown Vancouver) 6 Cameron! (As seen at VCON 24!) Meet at 7:00 Make checks payable to WCSFA blocks south of Burrard Skytrain Station. 3 pm. The address is: 316-4683 Arbutus St., (West Coast Science Fiction blocks west of Granville (where many buses Vancouver, BC V6J 4A3 Association) run). #22 Knight/McDonald bus along June 19th - (Saturday) WCSFA General Meeting Send cheques to: WCSFA Burrard. Begins 8:00pm. On the Friday before at 1 pm. Firehall Branch Library. 1455 West #110-1855 West 2nd Ave. long weekends, FRED will be at the lounge of 10th Avenue, Vancouver. (Tenth and Granville). Vancouver, B.C. V6J 1J1 Bosman’s Hotel. This is two blocks east and a Phone Doug Finnerty (526-5621) for more WCSFA Executive part of a block north of the Burrard Motor Inn information. -
Tailoring Laser Propulsion for Future Applications in Space
Tailoring Laser Propulsion for Future Applications in Space Hans-Albert Eckel and Stefan Scharring German Aerospace Center (DLR) – Institute of Technical Physics, Pfaffenwaldring 38 – 40, 70569 Stuttgart, Germany Abstract. Pulsed laser propulsion may turn out as a low cost alternative for the transportation of small payloads in future. In recent years DLR investigated this technology with the goal of cheaply launching small satellites into low earth orbit (LEO) with payload masses on the order of 5 to 10 kg. Since the required high power pulsed laser sources are yet not at the horizon, DLR focused on new applications based on available laser technology. Space-borne, i.e. in weightlessness, there exist a wide range of missions requiring small thrusters that can be propelled by laser power. This covers space logistic and sample return missions as well as position keeping and attitude control of satellites. First, a report on the proof of concept of a remote controlled laser rocket with a thrust vector steering device integrated in a parabolic nozzle will be given. Second, the road from the previous ground-based flight experiments in earth’s gravity using a 100-J class laser to flight experiments with a parabolic thruster in an artificial 2D-zero gravity on an air cushion table employing a 1-J class laser and, with even less energy, new investigations in the field of laser micro propulsion will be reviewed. Keywords: Laser propulsion, Free flight experiments, Steering, Lightcraft, Parabolic thruster, Impulse coupling coefficient, Remote control, Laser ablation, Microgravity, Air cushion table. PACS: 41.75.Jv, 42.15.Dp, 42.62.-b, 52.38.Mf. -
Orbital Simulations of Laser-Propelled Spacecraft Qicheng Zhang*A, Kevin J
Orbital simulations of laser-propelled spacecraft Qicheng Zhang*a, Kevin J. Walshb, Carl Melisc, Gary B. Hughesd, Philip M. Lubina * [email protected] aDept. of Physics, Univ. of California, Santa Barbara, CA USA 93106-9530; bSouthwest Research Institute, Boulder, CO USA 80302; cCenter for Astrophysics and Space Sciences, Univ. of California, San Diego, CA USA 92093-0424; dStatistics Dept., California Polytechnic State Univ., San Luis Obispo, CA USA 93407-0405 ABSTRACT Spacecraft accelerate by directing propellant in the opposite direction. In the traditional approach, the propellant is carried onboard in the form of material fuel. This approach has the drawback of being limited in Delta v by the amount of fuel launched with the craft, a limit that does not scale well to high Delta v due to the massive nature of the fuel. Directed energy photon propulsion solves this problem by eliminating the storage of fuel onboard. A phased array of lasers may be used to propel the spacecraft, contributing no mass to the spacecraft beyond that of the reflector, enabling a prolonged acceleration and much higher final speeds. This paper compares the effectiveness of such a system for propelling spacecraft into interplanetary and interstellar space across various laser and sail configurations. Simulated parameters include laser power, optics size and orbit as well as payload mass, reflector size and the trajectory of the spacecraft. As one example, a large 70 GW laser with 10 km optics could propel a 1 kg payload past Neptune (~30 au) in 5 days at 4% the speed of light, or a 1 g payload past Mars (~0.5 au) in 20 minutes at 21% the speed of light. -
Beam Powered Propulsion Systems
Beam Powered Propulsion Systems Nishant Agarwal University of Colorado, Boulder, 80309 While chemical rockets have dominated space exploration, other forms of rocket propulsion based on nuclear power, electrostatic and magnetic drives, and other principles have been considered from the earliest days of the field with the goal to improve efficiency through higher exhaust velocities, in order to reduce the amount of fuel the rocket vehicle needs to carry. However, the gap between technology to reach orbit from surface and from orbit to interplanetary travel still remains open considering both economics of time and money. In addition, methods have been tested over the years to reach the orbit with single stage rocket from earth’s surface which will eventually result in drastic cost savings. Reusable SSTO vehicles offer the promise of reduced launch expenses by eliminating recurring costs associated with hardware replacement inherent in expendable launch systems. No Earth- launched SSTO launch vehicles have ever been constructed till date. Beam Powered Propulsion has emerged as a promising concept that is capable to fulfill all regimes of space travel. This paper takes a look at these concepts and studies the feasibility of Microwave Propulsion for possibility of SSTO vehicle. Nomenclature At = nozzle throat area C* = characteristic velocity Cf = Thrust Coefficient Cp = Specific heat constant Dt, Dexit = Diameter of nozzle throat, Nozzle exit diameter g = acceleration due to gravity Gamma = Specific heat ratio LOX/LH = Liquid Oxygen/Liquid Hydrogen MR = mass ratio Mi,Ms,Mp = total mass, structural mass, propellant mass, payload mass Mpayl = payload mass Mdot = flow rate Isp = Specific Impulse Ve = exhaust velocity I. -
If You Like Science Fiction Try These Authors
if you like science fiction try these authors. Classic | Adventure | SF Mysteries | Militaristic | Aliens | Techno | Dystopias | Time Travel| Alt Universes | Humorous | Space Opera Classic Authors Adventure Isaac Asimov Roger MacBride Allen Ray Bradbury Ben Bova Arthur C. Clarke Michael Crichton Philip K. Dick Jack Finney Robert Heinlein Robert Heinlein Frank Herbert Ken MacLeod Larry Niven George R.R. Martin Mary Shelley Andre Norton Jules Verne Kim Stanley Robinson Kurt Vonnegut Spider Robinson H.G. Wells Charles Sheffield Clifford Simak Timothy Zahn SF Mysteries Militaristic Jayne Castle David Brin William C Dietz - (Sam McCade series) Lois McMaster Bujold - (Vorkosigan series) Peter F. Hamilton Orson Scott Card Jack McDevitt William C Dietz - (Legion series) China Mieville Joe Haldeman Richard K. Morgan Elizabeth Moon JD Robb Dan Simmons Wen Spencer David Weber S.L. Viehl Gene Wolf Aliens / Space Colonies Techno SF Jack Campbell Isaac Asimov - Robot series Edgar Rice Burroughs – (Mars Series) Iain Banks C.J. Cherryh Meljean Brook - Iron seas Nancy Kress William Gibson Ursula LeGuin Larry Niven Anne McCaffrey Robert J. Sawyer - WWW series Stephenie Meyer - The Host Brian Stableford St. Charles City-County Library District – Your Answer Place! http://www.youranswerplace.org/if-you-science-fiction Kim Stanley Robinson Neal Stephenson Charles Sheffield Bruce Sterling Robert Silverberg John Varley Jack Williamson James White Dystopias Time Travel Margaret Atwood Robert Asprin--Time Scout series Suzanne Collins Kage Baker – The Company series James Dashner Andre Norton - Time Traders series Aldous Huxley Cherie Priest- Clockwork Century series Patrick Ness S. M. Stirling George Orwell Connie Willis S.M. Stirling Scott Westerfeld Alternate Histories / Universes Humorous Taylor Anderson Douglas Adams Stephen Baxter Jasper Fforde John Birmingham Alan Dean Foster Marion Zimmer Bradley Dave Freer Philip K. -
Affordable Spacecraft: Design and Launch Alternatives (Part 7 of 8)
Chapter 5 Microspacecraft Microspacecraft would be satellites or deep-space the accelerations to which electromagnetic launch probes weighing no more than about 10 kilograms would subject them. (22 pounds).1 Tens or hundreds could be usedto Placed in different orbits or trajectories, they measure magnetism, gravity, or solar wind at widely could trade off field of view for resolution, or vice separated points simultaneously. A swarm of differ- versa. For example, one MOC microspacecraft in a ent microspacecraft could obtain detailed radio polar orbit about Mars could serve as a Martian images of galaxies, while others could be used for weather satellite, providing two-color images with a communications, gamma-ray astronomy, or plane- resolution of 5 to 10 kilometers (km )-sufficient to tary photoreconnaissance. resolve Martian clouds. A similar MOC microspace- They would not require development of new craft in a lower orbit could serve as a mapper, launch systems; they could be launched like buck- providing two-color images of a smaller field of shot on existing small launch vehicles. However, if view with better resolution—100 meters (m). In time there were a demand for launching thousands per it could map the entire planet. A similar MOC year, it might be cheaper to launch them on microspacecraft in an even lower orbit about the laser-powered rockets (see figure 5-1 ), if these prove Moon could provide a two-color global map of the feasible. Moon with 10 m resolution. Existing global maps of the Moon currently show no features smaller than Extremely rugged microspacecraft, constructed several hundred meters.