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Low-Energy Lunar Trajectory Design
LOW-ENERGY LUNAR TRAJECTORY DESIGN Jeffrey S. Parker and Rodney L. Anderson Jet Propulsion Laboratory Pasadena, California July 2013 ii DEEP SPACE COMMUNICATIONS AND NAVIGATION SERIES Issued by the Deep Space Communications and Navigation Systems Center of Excellence Jet Propulsion Laboratory California Institute of Technology Joseph H. Yuen, Editor-in-Chief Published Titles in this Series Radiometric Tracking Techniques for Deep-Space Navigation Catherine L. Thornton and James S. Border Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation Theodore D. Moyer Bandwidth-Efficient Digital Modulation with Application to Deep-Space Communication Marvin K. Simon Large Antennas of the Deep Space Network William A. Imbriale Antenna Arraying Techniques in the Deep Space Network David H. Rogstad, Alexander Mileant, and Timothy T. Pham Radio Occultations Using Earth Satellites: A Wave Theory Treatment William G. Melbourne Deep Space Optical Communications Hamid Hemmati, Editor Spaceborne Antennas for Planetary Exploration William A. Imbriale, Editor Autonomous Software-Defined Radio Receivers for Deep Space Applications Jon Hamkins and Marvin K. Simon, Editors Low-Noise Systems in the Deep Space Network Macgregor S. Reid, Editor Coupled-Oscillator Based Active-Array Antennas Ronald J. Pogorzelski and Apostolos Georgiadis Low-Energy Lunar Trajectory Design Jeffrey S. Parker and Rodney L. Anderson LOW-ENERGY LUNAR TRAJECTORY DESIGN Jeffrey S. Parker and Rodney L. Anderson Jet Propulsion Laboratory Pasadena, California July 2013 iv Low-Energy Lunar Trajectory Design July 2013 Jeffrey Parker: I dedicate the majority of this book to my wife Jen, my best friend and greatest support throughout the development of this book and always. -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
Lunar Ionosphere Exploration Method Using Auroral Kilometric Radiation
Earth Planets Space, 63, 47–56, 2011 Lunar ionosphere exploration method using auroral kilometric radiation Yoshitaka Goto1, Takamasa Fujimoto1, Yoshiya Kasahara1, Atsushi Kumamoto2, and Takayuki Ono2 1Kanazawa University, Kanazawa, Japan 2Tohoku University, Sendai, Japan (Received June 3, 2009; Revised November 10, 2010; Accepted January 14, 2011; Online published February 21, 2011) The evidence of a lunar ionosphere provided by radio occultation experiments performed by the Soviet spacecraft Luna 19 and 22 has been controversial for the past three decades because the observed large density is difficult to explain theoretically without magnetic shielding from the solar wind. The KAGUYA mission provided an opportunity to investigate the lunar ionosphere with another method. The natural plasma wave receiver (NPW) and waveform capture (WFC) instruments, which are subsystems of the lunar radar sounder (LRS) on board the lunar orbiter KAGUYA, frequently observe auroral kilometric radiation (AKR) propagating from the Earth. The dynamic spectra of the AKR sometimes exhibit a clear interference pattern that is caused by phase differences between direct waves and waves reflected on a lunar surface or a lunar ionosphere if it exists. It was hypothesized that the electron density profiles above the lunar surface could be evaluated by comparing the observed interference pattern with the theoretical interference patterns constructed from the profiles with ray tracing. This method provides a new approach to examining the lunar ionosphere that does not involve the conventional radio occultation technique. Key words: KAGUYA, lunar ionosphere, auroral kilometric radiation. 1. Introduction 2001; Kurata et al., 2005). The dense plasma layers may The lunar atmosphere is extremely tenuous compared to be maintained by these strong fields. -
Honoring Yesterday, Inspiring Tomorrow
TALK ThistleThistle TALK Art from the heart Middle Schoolers expressed themselves in creating “Postcards to the Congo,” a unique component of the City as Our Campus initiative. (See story on page 13.) Winchester Nonprofi t Org. Honoring yesterday, Thurston U.S. Postage School PAID inspiring tomorrow. Pittsburgh, PA 555 Morewood Avenue Permit No. 145 Pittsburgh, PA 15213 The evolution of WT www.winchesterthurston.org in academics, arts, and athletics in this issue: Commencement 2007 A Fond Farewell City as Our Campus Expanding minds in expanding ways Ann Peterson Refl ections on a beloved art teacher Winchester Thurston School Autumn 2007 TALK A magnifi cent showing Thistle WT's own art gallery played host in November to LUMINOUS, MAGAZINE a glittering display of 14 local and nationally recognized glass Volume 35 • Number 1 Autumn 2007 artists, including faculty members Carl Jones, Mary Martin ’88, and Tina Plaks, along with eighth-grader Red Otto. Thistletalk is published two times per year by Winchester Thurston School for alumnae/i, parents, students, and friends of the school. Letters and suggestions are welcome. Please contact the Director of Communications, Winchester Thurston School, 555 Morewood Malone Scholars Avenue, Pittsburgh, PA 15213. Editor Anne Flanagan Director of Communications fl [email protected] Assistant Editor Alison Wolfson Director of Alumnae/i Relations [email protected] Contributors David Ascheknas Alison D’Addieco John Holmes Carl Jones Mary Martin ’88 Karen Meyers ’72 Emily Sturman Allison Thompson Printing Herrmann Printing School Mission Winchester Thurston School actively engages each student in a challenging and inspiring learning process that develops the mind, motivates the passion to achieve, and cultivates the character to serve. -
Arxiv:1912.04482V1 [Physics.Space-Ph] 10 Dec 2019
manuscript submitted to Radio Science Measuring the Earth's Synchrotron Emission from Radiation Belts with a Lunar Near Side Radio Array Alexander Hegedus1, Quentin Nenon2, Antoine Brunet3, Justin Kasper1, Ang´elicaSicard3, Baptiste Cecconi4, Robert MacDowall5, Daniel Baker6 1University of Michigan, Department of Climate and Space Sciences and Engineering, Ann Arbor, Michigan, USA 2Space Sciences Laboratory, University of California, Berkeley, CA, USA 3ONERA / DPHY, Universit´ede Toulouse, F-31055 Toulouse France 4LESIA, Observatoire de Paris, Universit PSL, CNRS, Sorbonne Universit, Univ. de Paris, Meudon, France 5NASA Goddard Space Flight Center, Greenbelt, MD, USA 6University of Colorado Boulder, Laboratory for Atmospheric and Space Physics, Boulder, Colorado, USA Key Points: • Synchrotron emission between 500-1000 kHz has a total flux density of 1.4-2 Jy at lunar distances • A 10 km radio array with 16000 elements could detect the emission in 12-24 hours with moderate noise • Changing electron density can make detections 10x faster at lunar night, 10x slower at lunar noon arXiv:1912.04482v1 [physics.space-ph] 10 Dec 2019 Corresponding author: Alexander Hegedus, [email protected] {1{ manuscript submitted to Radio Science Abstract The high kinetic energy electrons that populate the Earth's radiation belts emit synchrotron emissions because of their interaction with the planetary magnetic field. A lunar near side array would be uniquely positioned to image this emission and provide a near real time measure of how the Earth's radiation belts are responding to the current solar in- put. The Salammb^ocode is a physical model of the dynamics of the three-dimensional phase-space electron densities in the radiation belts, allowing the prediction of 1 keV to 100 MeV electron distributions trapped in the belts. -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Apollo Over the Moon: a View from Orbit (Nasa Sp-362)
chl APOLLO OVER THE MOON: A VIEW FROM ORBIT (NASA SP-362) Chapter 1 - Introduction Harold Masursky, Farouk El-Baz, Frederick J. Doyle, and Leon J. Kosofsky [For a high resolution picture- click here] Objectives [1] Photography of the lunar surface was considered an important goal of the Apollo program by the National Aeronautics and Space Administration. The important objectives of Apollo photography were (1) to gather data pertaining to the topography and specific landmarks along the approach paths to the early Apollo landing sites; (2) to obtain high-resolution photographs of the landing sites and surrounding areas to plan lunar surface exploration, and to provide a basis for extrapolating the concentrated observations at the landing sites to nearby areas; and (3) to obtain photographs suitable for regional studies of the lunar geologic environment and the processes that act upon it. Through study of the photographs and all other arrays of information gathered by the Apollo and earlier lunar programs, we may develop an understanding of the evolution of the lunar crust. In this introductory chapter we describe how the Apollo photographic systems were selected and used; how the photographic mission plans were formulated and conducted; how part of the great mass of data is being analyzed and published; and, finally, we describe some of the scientific results. Historically most lunar atlases have used photointerpretive techniques to discuss the possible origins of the Moon's crust and its surface features. The ideas presented in this volume also rely on photointerpretation. However, many ideas are substantiated or expanded by information obtained from the huge arrays of supporting data gathered by Earth-based and orbital sensors, from experiments deployed on the lunar surface, and from studies made of the returned samples. -
*Pres Report 97
42 APPENDIX C U.S. and Russian Human Space Flights 1961–September 30, 1997 Spacecraft Launch Date Crew Flight Time Highlights (days:hrs:min) Vostok 1 Apr. 12, 1961 Yury A. Gagarin 0:1:48 First human flight. Mercury-Redstone 3 May 5, 1961 Alan B. Shepard, Jr. 0:0:15 First U.S. flight; suborbital. Mercury-Redstone 4 July 21, 1961 Virgil I. Grissom 0:0:16 Suborbital; capsule sank after landing; astronaut safe. Vostok 2 Aug. 6, 1961 German S. Titov 1:1:18 First flight exceeding 24 hrs. Mercury-Atlas 6 Feb. 20, 1962 John H. Glenn, Jr. 0:4:55 First American to orbit. Mercury-Atlas 7 May 24, 1962 M. Scott Carpenter 0:4:56 Landed 400 km beyond target. Vostok 3 Aug. 11, 1962 Andriyan G. Nikolayev 3:22:25 First dual mission (with Vostok 4). Vostok 4 Aug. 12, 1962 Pavel R. Popovich 2:22:59 Came within 6 km of Vostok 3. Mercury-Atlas 8 Oct. 3, 1962 Walter M. Schirra, Jr. 0:9:13 Landed 8 km from target. Mercury-Atlas 9 May 15, 1963 L. Gordon Cooper, Jr. 1:10:20 First U.S. flight exceeding 24 hrs. Vostok 5 June 14, 1963 Valery F. Bykovskiy 4:23:6 Second dual mission (withVostok 6). Vostok 6 June 16, 1963 Valentina V. Tereshkova 2:22:50 First woman in space; within 5 km of Vostok 5. Voskhod 1 Oct. 12, 1964 Vladimir M. Komarov 1:0:17 First three-person crew. Konstantin P. Feoktistov Boris G. Yegorov Voskhod 2 Mar. 18, 1965 Pavel I. -
Deep Space Chronicle Deep Space Chronicle: a Chronology of Deep Space and Planetary Probes, 1958–2000 | Asifa
dsc_cover (Converted)-1 8/6/02 10:33 AM Page 1 Deep Space Chronicle Deep Space Chronicle: A Chronology ofDeep Space and Planetary Probes, 1958–2000 |Asif A.Siddiqi National Aeronautics and Space Administration NASA SP-2002-4524 A Chronology of Deep Space and Planetary Probes 1958–2000 Asif A. Siddiqi NASA SP-2002-4524 Monographs in Aerospace History Number 24 dsc_cover (Converted)-1 8/6/02 10:33 AM Page 2 Cover photo: A montage of planetary images taken by Mariner 10, the Mars Global Surveyor Orbiter, Voyager 1, and Voyager 2, all managed by the Jet Propulsion Laboratory in Pasadena, California. Included (from top to bottom) are images of Mercury, Venus, Earth (and Moon), Mars, Jupiter, Saturn, Uranus, and Neptune. The inner planets (Mercury, Venus, Earth and its Moon, and Mars) and the outer planets (Jupiter, Saturn, Uranus, and Neptune) are roughly to scale to each other. NASA SP-2002-4524 Deep Space Chronicle A Chronology of Deep Space and Planetary Probes 1958–2000 ASIF A. SIDDIQI Monographs in Aerospace History Number 24 June 2002 National Aeronautics and Space Administration Office of External Relations NASA History Office Washington, DC 20546-0001 Library of Congress Cataloging-in-Publication Data Siddiqi, Asif A., 1966 Deep space chronicle: a chronology of deep space and planetary probes, 1958-2000 / by Asif A. Siddiqi. p.cm. – (Monographs in aerospace history; no. 24) (NASA SP; 2002-4524) Includes bibliographical references and index. 1. Space flight—History—20th century. I. Title. II. Series. III. NASA SP; 4524 TL 790.S53 2002 629.4’1’0904—dc21 2001044012 Table of Contents Foreword by Roger D. -
EPSC2017-933, 2017 European Planetary Science Congress 2017 Eeuropeapn Planetarsy Science Ccongress C Author(S) 2017
EPSC Abstracts Vol. 11, EPSC2017-933, 2017 European Planetary Science Congress 2017 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2017 Radio science electron density profiles of lunar ionosphere based on the service module of circumlunar return and re- entry spacecraft M. Wang (1), S. Han (2), J. Ping (1), G. Tang (2) and Q. Zhang (2) (1) National Astronomical Observatories, Chinese Academy of Sciences, Beijng, China, (2) National Key Laboratory of Science and Technology on Aerospace Flight Dynamics, Beijng, China ([email protected]) Abstract The circumlunar return and reentry spacecraft is a Chinese precursor mission for the Chinese lunar The existence of lunar ionosphere has been under sample return mission. After the status analysis of the debate for a long time. Radio occultation experiments spaceborne microwave communication system, we had been performed by both Luna 19/22 and confirmed that the frequency source of the VLBI SELENE missions and electron column density of beacon in X-band and the signal in S-band is lunar ionosphere was provided. The Apollo 14 provided by the same frequency source onboard the mission also acquired the electron density with in situ satellite and its short-term stability is n*10-9. measurements. But the results of these missions don't Compared to the frequency source onboard SELENE well-matched. In order to explore the lunar whose short-term stability is n*10-7 [6], the service ionosphere, radio occultation with the service module module provides a stable and reliable signal source of Chinese circumlunar return and reentry spacecraft for dual frequency radio occultation. -
ILWS Report 137 Moon
Returning to the Moon Heritage issues raised by the Google Lunar X Prize Dirk HR Spennemann Guy Murphy Returning to the Moon Heritage issues raised by the Google Lunar X Prize Dirk HR Spennemann Guy Murphy Albury February 2020 © 2011, revised 2020. All rights reserved by the authors. The contents of this publication are copyright in all countries subscribing to the Berne Convention. No parts of this report may be reproduced in any form or by any means, electronic or mechanical, in existence or to be invented, including photocopying, recording or by any information storage and retrieval system, without the written permission of the authors, except where permitted by law. Preferred citation of this Report Spennemann, Dirk HR & Murphy, Guy (2020). Returning to the Moon. Heritage issues raised by the Google Lunar X Prize. Institute for Land, Water and Society Report nº 137. Albury, NSW: Institute for Land, Water and Society, Charles Sturt University. iv, 35 pp ISBN 978-1-86-467370-8 Disclaimer The views expressed in this report are solely the authors’ and do not necessarily reflect the views of Charles Sturt University. Contact Associate Professor Dirk HR Spennemann, MA, PhD, MICOMOS, APF Institute for Land, Water and Society, Charles Sturt University, PO Box 789, Albury NSW 2640, Australia. email: [email protected] Spennemann & Murphy (2020) Returning to the Moon: Heritage Issues Raised by the Google Lunar X Prize Page ii CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 2 2. HUMAN ARTEFACTS ON THE MOON 3 What Have These Missions Left BehinD? 4 Impactor Missions 10 Lander Missions 11 Rover Missions 11 Sample Return Missions 11 Human Missions 11 The Lunar Environment & ImpLications for Artefact Preservation 13 Decay caused by ascent module 15 Decay by solar radiation 15 Human Interference 16 3. -
Preparation of Papers for AIAA Journals
Mega-Drivers to Inform NASA Space Technology Strategic Planning Melanie L. Grande,1 Matthew J. Carrier,1 William M. Cirillo,2 Kevin D. Earle,2 Christopher A. Jones,2 Emily L. Judd,1 Jordan J. Klovstad,2 Andrew C. Owens,1 David M. Reeves,2 and Matthew A. Stafford3 NASA Langley Research Center, Hampton, VA, 23681, USA The National Aeronautics and Space Administration (NASA) Space Technology Mission Directorate (STMD) has been developing a new Strategic Framework to guide investment prioritization and communication of STMD strategic goals to stakeholders. STMD’s analysis of global trends identified four overarching drivers which are anticipated to shape the needs of civilian space research for years to come. These Mega-Drivers form the foundation of the Strategic Framework. The Increasing Access Mega-Driver reflects the increase in the availability of launch options, more capable propulsion systems, access to planetary surfaces, and the introduction of new platforms to enable exploration, science, and commercial activities. Accelerating Pace of Discovery reflects the exploration of more remote and challenging destinations, drives increased demand for improved abilities to communicate and process large datasets. The Democratization of Space reflects the broadening participation in the space industry, from governments to private investors to citizens. Growing Utilization of Space reflects space market diversification and growth. This paper will further describe the observable trends that inform each of these Mega Drivers, as well as the interrelationships