By James R. Hansen Monographs in Aerospace
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Astrodynamics
Politecnico di Torino SEEDS SpacE Exploration and Development Systems Astrodynamics II Edition 2006 - 07 - Ver. 2.0.1 Author: Guido Colasurdo Dipartimento di Energetica Teacher: Giulio Avanzini Dipartimento di Ingegneria Aeronautica e Spaziale e-mail: [email protected] Contents 1 Two–Body Orbital Mechanics 1 1.1 BirthofAstrodynamics: Kepler’sLaws. ......... 1 1.2 Newton’sLawsofMotion ............................ ... 2 1.3 Newton’s Law of Universal Gravitation . ......... 3 1.4 The n–BodyProblem ................................. 4 1.5 Equation of Motion in the Two-Body Problem . ....... 5 1.6 PotentialEnergy ................................. ... 6 1.7 ConstantsoftheMotion . .. .. .. .. .. .. .. .. .... 7 1.8 TrajectoryEquation .............................. .... 8 1.9 ConicSections ................................... 8 1.10 Relating Energy and Semi-major Axis . ........ 9 2 Two-Dimensional Analysis of Motion 11 2.1 ReferenceFrames................................. 11 2.2 Velocity and acceleration components . ......... 12 2.3 First-Order Scalar Equations of Motion . ......... 12 2.4 PerifocalReferenceFrame . ...... 13 2.5 FlightPathAngle ................................. 14 2.6 EllipticalOrbits................................ ..... 15 2.6.1 Geometry of an Elliptical Orbit . ..... 15 2.6.2 Period of an Elliptical Orbit . ..... 16 2.7 Time–of–Flight on the Elliptical Orbit . .......... 16 2.8 Extensiontohyperbolaandparabola. ........ 18 2.9 Circular and Escape Velocity, Hyperbolic Excess Speed . .............. 18 2.10 CosmicVelocities -
Electric Propulsion System Scaling for Asteroid Capture-And-Return Missions
Electric propulsion system scaling for asteroid capture-and-return missions Justin M. Little⇤ and Edgar Y. Choueiri† Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ, 08544 The requirements for an electric propulsion system needed to maximize the return mass of asteroid capture-and-return (ACR) missions are investigated in detail. An analytical model is presented for the mission time and mass balance of an ACR mission based on the propellant requirements of each mission phase. Edelbaum’s approximation is used for the Earth-escape phase. The asteroid rendezvous and return phases of the mission are modeled as a low-thrust optimal control problem with a lunar assist. The numerical solution to this problem is used to derive scaling laws for the propellant requirements based on the maneuver time, asteroid orbit, and propulsion system parameters. Constraining the rendezvous and return phases by the synodic period of the target asteroid, a semi- empirical equation is obtained for the optimum specific impulse and power supply. It was found analytically that the optimum power supply is one such that the mass of the propulsion system and power supply are approximately equal to the total mass of propellant used during the entire mission. Finally, it is shown that ACR missions, in general, are optimized using propulsion systems capable of processing 100 kW – 1 MW of power with specific impulses in the range 5,000 – 10,000 s, and have the potential to return asteroids on the order of 103 104 tons. − Nomenclature -
Apollo Program 1 Apollo Program
Apollo program 1 Apollo program The Apollo program was the third human spaceflight program carried out by the National Aeronautics and Space Administration (NASA), the United States' civilian space agency. First conceived during the Presidency of Dwight D. Eisenhower as a three-man spacecraft to follow the one-man Project Mercury which put the first Americans in space, Apollo was later dedicated to President John F. Kennedy's national goal of "landing a man on the Moon and returning him safely to the Earth" by the end of the 1960s, which he proposed in a May 25, 1961 address to Congress. Project Mercury was followed by the two-man Project Gemini (1962–66). The first manned flight of Apollo was in 1968 and it succeeded in landing the first humans on Earth's Moon from 1969 through 1972. Kennedy's goal was accomplished on the Apollo 11 mission when astronauts Neil Armstrong and Buzz Aldrin landed their Lunar Module (LM) on the Moon on July 20, 1969 and walked on its surface while Michael Collins remained in lunar orbit in the command spacecraft, and all three landed safely on Earth on July 24. Five subsequent Apollo missions also landed astronauts on the Moon, the last in December 1972. In these six spaceflights, 12 men walked on the Moon. Apollo ran from 1961 to 1972, and was supported by the two-man Gemini program which ran concurrently with it from 1962 to 1966. Gemini missions developed some of the space travel techniques that were necessary for the success of the Apollo missions. -
Aas 11-509 Artemis Lunar Orbit Insertion and Science Orbit Design Through 2013
AAS 11-509 ARTEMIS LUNAR ORBIT INSERTION AND SCIENCE ORBIT DESIGN THROUGH 2013 Stephen B. Broschart,∗ Theodore H. Sweetser,y Vassilis Angelopoulos,z David C. Folta,x and Mark A. Woodard{ As of late-July 2011, the ARTEMIS mission is transferring two spacecraft from Lissajous orbits around Earth-Moon Lagrange Point #1 into highly-eccentric lunar science orbits. This paper presents the trajectory design for the transfer from Lissajous orbit to lunar orbit in- sertion, the period reduction maneuvers, and the science orbits through 2013. The design accommodates large perturbations from Earth’s gravity and restrictive spacecraft capabili- ties to enable opportunities for a range of heliophysics and planetary science measurements. The process used to design the highly-eccentric ARTEMIS science orbits is outlined. The approach may inform the design of future eccentric orbiter missions at planetary moons. INTRODUCTION The Acceleration, Reconnection, Turbulence and Electrodynamics of the Moons Interaction with the Sun (ARTEMIS) mission is currently operating two spacecraft in lunar orbit under funding from the Heliophysics and Planetary Science Divisions with NASA’s Science Missions Directorate. ARTEMIS is an extension to the successful Time History of Events and Macroscale Interactions during Substorms (THEMIS) mission [1] that has relocated two of the THEMIS spacecraft from Earth orbit to the Moon [2, 3, 4]. ARTEMIS plans to conduct a variety of scientific studies at the Moon using the on-board particle and fields instrument package [5, 6]. The final portion of the ARTEMIS transfers involves moving the two ARTEMIS spacecraft, known as P1 and P2, from Lissajous orbits around the Earth-Moon Lagrange Point #1 (EML1) to long-lived, eccentric lunar science orbits with periods of roughly 28 hr. -
Evolution of the Rendezvous-Maneuver Plan for Lunar-Landing Missions
NASA TECHNICAL NOTE NASA TN D-7388 00 00 APOLLO EXPERIENCE REPORT - EVOLUTION OF THE RENDEZVOUS-MANEUVER PLAN FOR LUNAR-LANDING MISSIONS by Jumes D. Alexunder und Robert We Becker Lyndon B, Johnson Spuce Center ffoaston, Texus 77058 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. AUGUST 1973 1. Report No. 2. Government Accession No, 3. Recipient's Catalog No. NASA TN D-7388 4. Title and Subtitle 5. Report Date APOLLOEXPERIENCEREPORT August 1973 EVOLUTIONOFTHERENDEZVOUS-MANEUVERPLAN 6. Performing Organizatlon Code FOR THE LUNAR-LANDING MISSIONS 7. Author(s) 8. Performing Organization Report No. James D. Alexander and Robert W. Becker, JSC JSC S-334 10. Work Unit No. 9. Performing Organization Name and Address I - 924-22-20- 00- 72 Lyndon B. Johnson Space Center 11. Contract or Grant No. Houston, Texas 77058 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Technical Note I National Aeronautics and Space Administration 14. Sponsoring Agency Code Washington, D. C. 20546 I 15. Supplementary Notes The JSC Director waived the use of the International System of Units (SI) for this Apollo Experience I Report because, in his judgment, the use of SI units would impair the usefulness of the report or I I result in excessive cost. 16. Abstract The evolution of the nominal rendezvous-maneuver plan for the lunar landing missions is presented along with a summary of the significant developments for the lunar module abort and rescue plan. A general discussion of the rendezvous dispersion analysis that was conducted in support of both the nominal and contingency rendezvous planning is included. -
Proof of God Scientific Proof That God Exists Week 1
Proof of God Scientific Proof That God Exists Week 1: Proof of Creation Our Mission: To take as many people to Heaven as we can before we die. Period. But the Lord made the earth by his power... Jeremiah 10:12 NLT As the Scriptures say, “I will destroy the wisdom of the wise and discard the intelligence of the intelligent.” So where does this leave the philosophers, the scholars, and the world’s brilliant debaters? God has made the wisdom of this world look foolish. 21 Since God in his wisdom saw to it that the world would never know him through human wisdom, he has used our foolish preaching to save those who believe…God chose things the world considers foolish in order to shame those who think they are wise. 1 Corinthians 1:19-23, 27 NLT Scientific fact: The universe has a beginning. Bible fact: “In the beginning God created the heavens and the earth.” Genesis 1:1 NLT The biggest evidence that there is a God is found in what the father of modern science Francis Bacon called, the Law of Causality. “True knowledge is knowledge by causes.” - Francis Bacon Cosmological Argument: 1. Everything that had a beginning had a cause. 2. The universe had a beginning. 3. Therefore the universe had a cause. 1. The universe is running out of energy. Second Law of Thermodynamics: The total entropy of an isolated system can never decrease over time. In all spontaneous processes, the total entropy increases and the process is irreversible. Law of Entropy: With time, things naturally fall apart. -
The Following Are Edited Excerpts from Two Interviews Conducted with Dr
Interviews with Dr. Wernher von Braun Editor's note: The following are edited excerpts from two interviews conducted with Dr. Wernher von Braun. Interview #1 was conducted on August 25, 1970, by Robert Sherrod while Dr. von Braun was deputy associate administrator for planning at NASA Headquarters. Interview #2 was conducted on November 17, 1971, by Roger Bilstein and John Beltz. These interviews are among those published in Before This Decade is Out: Personal Reflections on the Apollo Program, (SP-4223, 1999) edited by Glen E. Swanson, whick is vailable on-line at http://history.nasa.gov/SP-4223/sp4223.htm on the Web. Interview #1 In the Apollo Spacecraft Chronology, you are quoted as saying "It is true that for a long time we were not in favor of lunar orbit rendezvous. We favored Earth orbit rendezvous." Well, actually even that is not quite correct, because at the outset we just didn't know which route [for Apollo to travel to the Moon] was the most promising. We made an agreement with Houston that we at Marshall would concentrate on the study of Earth orbit rendezvous, but that did not mean we wanted to sell it as our preferred scheme. We weren't ready to vote for it yet; our study was meant to merely identify the problems involved. The agreement also said that Houston would concentrate on studying the lunar rendezvous mode. Only after both groups had done their homework would we compare notes. This agreement was based on common sense. You don't start selling your scheme until you are convinced that it is superior. -
Through Astronaut Eyes: Photographing Early Human Spaceflight
Purdue University Purdue e-Pubs Purdue University Press Book Previews Purdue University Press 6-2020 Through Astronaut Eyes: Photographing Early Human Spaceflight Jennifer K. Levasseur Follow this and additional works at: https://docs.lib.purdue.edu/purduepress_previews This document has been made available through Purdue e-Pubs, a service of the Purdue University Libraries. Please contact [email protected] for additional information. THROUGH ASTRONAUT EYES PURDUE STUDIES IN AERONAUTICS AND ASTRONAUTICS James R. Hansen, Series Editor Purdue Studies in Aeronautics and Astronautics builds on Purdue’s leadership in aeronautic and astronautic engineering, as well as the historic accomplishments of many of its luminary alums. Works in the series will explore cutting-edge topics in aeronautics and astronautics enterprises, tell unique stories from the history of flight and space travel, and contemplate the future of human space exploration and colonization. RECENT BOOKS IN THE SERIES British Imperial Air Power: The Royal Air Forces and the Defense of Australia and New Zealand Between the World Wars by Alex M Spencer A Reluctant Icon: Letters to Neil Armstrong by James R. Hansen John Houbolt: The Unsung Hero of the Apollo Moon Landings by William F. Causey Dear Neil Armstrong: Letters to the First Man from All Mankind by James R. Hansen Piercing the Horizon: The Story of Visionary NASA Chief Tom Paine by Sunny Tsiao Calculated Risk: The Supersonic Life and Times of Gus Grissom by George Leopold Spacewalker: My Journey in Space and Faith as NASA’s Record-Setting Frequent Flyer by Jerry L. Ross THROUGH ASTRONAUT EYES Photographing Early Human Spaceflight Jennifer K. -
UC San Diego UC San Diego Electronic Theses and Dissertations
UC San Diego UC San Diego Electronic Theses and Dissertations Title The new prophet : Harold C. Urey, scientist, atheist, and defender of religion Permalink https://escholarship.org/uc/item/3j80v92j Author Shindell, Matthew Benjamin Publication Date 2011 Peer reviewed|Thesis/dissertation eScholarship.org Powered by the California Digital Library University of California UNIVERSITY OF CALIFORNIA, SAN DIEGO The New Prophet: Harold C. Urey, Scientist, Atheist, and Defender of Religion A dissertation submitted in partial satisfaction of the requirements for the degree Doctor of Philosophy in History (Science Studies) by Matthew Benjamin Shindell Committee in charge: Professor Naomi Oreskes, Chair Professor Robert Edelman Professor Martha Lampland Professor Charles Thorpe Professor Robert Westman 2011 Copyright Matthew Benjamin Shindell, 2011 All rights reserved. The Dissertation of Matthew Benjamin Shindell is approved, and it is acceptable in quality and form for publication on microfilm and electronically: ___________________________________________________________________ ___________________________________________________________________ ___________________________________________________________________ ___________________________________________________________________ ___________________________________________________________________ Chair University of California, San Diego 2011 iii TABLE OF CONTENTS Signature Page……………………………………………………………………...... iii Table of Contents……………………………………………………………………. iv Acknowledgements…………………………………………………………………. -
Ford Foundation Annual Report 2000 Ford Foundation Annual Report 2000 October 1, 1999 to September 30, 2000
Ford Foundation Annual Report 2000 Ford Foundation Annual Report 2000 October 1, 1999 to September 30, 2000 Ford Foundation Offices Inside front cover 1 Mission Statement 3 President’s Message 14 Board of Trustees 14 Officers 15 Committees of the Board 16 Staff 20 Program Approvals 21 Asset Building and Community Development 43 Peace and Social Justice 59 Education, Media, Arts and Culture 77 Grants and Projects, Fiscal Year 2000 Asset Building and Community Development Economic Development 78 Community and Resource Development 85 Human Development and Reproductive Health 97 Program-Related Investments 107 Peace and Social Justice Human Rights and International Cooperation 108 Governance and Civil Society 124 Education, Media, Arts and Culture Education, Knowledge and Religion 138 Media, Arts and Culture 147 Foundationwide Actions 155 Good Neighbor Grants 156 157 Financial Review 173 Index Communications Back cover flap Guidelines for Grant Seekers Inside back cover flap Library of Congress Card Number 52-43167 ISSN: 0071-7274 April 2001 Ford Foundation Offices • MOSCOW { NEW YORK BEIJING • NEW DELHI • • MEXICO CITY • CAIRO • HANOI • MANILA • LAGOS • NAIROBI • JAKARTA RIODEJANEIRO • • WINDHOEK • JOHANNESBURG SANTIAGO • United States Africa and Middle East West Africa The Philippines Andean Region Makati Central Post Office and Southern Cone Headquarters Eastern Africa Nigeria P.O. Box 1936 320 East 43rd Street P.O. Box 2368 Chile Kenya 1259 Makati City New York, New York Lagos, Nigeria Avenida Ricardo Lyon 806 P.O. Box 41081 The Philippines 10017 Providencia Nairobi, Republic of Kenya Asia Vietnam Santiago 6650429, Chile 340 Ba Trieu Street Middle East and North Africa China Hanoi, Socialist Republic International Club Office Building Russia Egypt of Vietnam Suite 501 Tverskaya Ulitsa 16/2 P.O. -
The Space Challenge and Soviet Science Fiction
Corso di Laurea magistrale ( ordinamento ex D.M. 270/2004 ) in Relazioni Internazionali Comparate – International Relations Tesi di Laurea The space challenge and Soviet science fiction Relatore Ch.mo Prof. Duccio Basosi Correlatore Ch.ma Prof. Donatella Possamai Laureanda Serena Zanin Matricola 835564 Anno Accademico 2011 / 2012 TABLE OF CONTENTS ABSTRACT ……………………………………………………………………...1 INTRODUCTION …………………………………………………...…………..7 CHAPTER I The science fiction in the Soviet bloc: the case of Stanislaw Lem’s “Solaris”…………………….…………………………………....…………...…16 CHAPTER II The space race era from the Soviet bloc side …………..….........37 CHAPTER III The enthusiasm for the cosmos and Soviet propaganda ……………….. …………………………...……...………………………………..73 FINAL CONSIDERATIONS ……………...………………………………...101 APPENDIX ........……………………………………………………..……..…106 REFERENCES …..……………………………………………………………113 ACKNOWLEDGEMENTS …………………………………………………..118 ABSTRACT La studiosa Julia Richers sottolinea come le ricerche sulla storia dell’esplorazione spaziale sovietica abbiano tre principali direzioni. La prima riguarda la storia politica della Guerra Fredda che considera la conquista dello spazio e lo sviluppo di potenti missili come parte di una più grande competizione tra gli USA e l’URSS. La seconda esamina in particolar modo lo sviluppo scientifico e tecnologico a partire dagli anni Ottanta, ossia da quando l’abolizione della censura ha permesso l’apertura al pubblico di molti archivi storici e la rivelazione di importanti informazioni. La terza include la propaganda sovietica e la fantascienza come parte fondamentale della storia culturale e sociale sia dell’URSS che della Russia post-rivoluzione. Il presente lavoro analizza la storia dell’esplorazione spaziale sovietica e, partendo dalle sue origini (fine XIX° secolo), prende in considerazione i principali successi che portarono al lancio del primo satellite artificiale nel 1957 e il primo uomo sulla luna nel 1961. -
Aprl-8-Transcript.Pdf
The Dark Arts in Space: Developments in Counterspace Weapons April 8, 2021 Virtual Event Moderator: Kaitlyn Johnson, Deputy Director and Fellow, Aerospace Security Project, CSIS Speakers: . LtCol Joe Moye, U.S. Marine Corps Military Fellow, International Security Program, CSIS . Victoria Samson, Washington Office Director, Secure World Foundation . Dr. Brian Weeden, Director of Program Planning, Secure World Foundation Kaitlyn Johnson: All right, well, the numbers keep jumping up, but we'll go ahead and get started. Again, thank you for joining. My name is Kaitlyn Johnson. I am the Deputy Director of the Aerospace Security Project at CSIS. I am so excited to be here and be joined by my good friends from the Secure World Foundation Victoria Samson and Brian Weeden, and then also our very own CSIS military fellow Joe Moye is a member of the Marine Corps and did a big assist with this report for us helping out. Unfortunately, you might have noticed we are missing a team member, Makena Young, our research associate was unable to join it. Unfortunately, you've got me filling in first section. I think she's pretty open and active on Twitter. If you have anything specific to ask, you can just shoot her a tweet. We will go ahead and get started with a quick overview from all of my panelists of what they think the top updates were for each country. Then we'll walk through some overall trends and general assessment and then get into some audience questions as well. Brian, can you please kick us off? Dr.