Year in Review 2006 Goddard 02
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Magcon White Paper V3
Magnetospheric Constellation Tracing the flow of mass and energy from the solar wind through the magnetosphere Larry Kepko and Guan Le NASA Goddard Space Flight Center 1. Executive Summary The Magnetospheric Constellation (MagCon) mission is designed to understand the transport of mass and energy across the boundaries of and within Earth’s magnetosphere using a constellation of up to 36 small satellites. Energy is input into the geospace system at the dayside and flank magnetopause, yet we still do not understand the azimuthal extent of dayside reconnection sites, nor do we have a quantifiable understanding of how much energy enters the magnetosphere during different solar wind conditions. On the nightside, impulsive flows at various spatial and temporal scales occur frequently during storms and substorms and couple to the ionosphere through still unresolved physical mechanisms. A distributed array of small satellites is the required tool for unraveling the physics of magnetospheric mass and energy transport while providing definitive determinations of how major solar events lead to specific types of space weather. MagCon will map the global circulation of magnetic fields and plasma flows within a domain extending from just above the Earth’s surface to ~22 Earth radii (RE) radius, at all local times, on spatial scales from 1-5 RE and minimum time scales of 3-10 seconds. It will reveal simultaneously for the first time both the global spatial structures and temporal evolution of the magnetotail, the dayside and flank magnetopause, and the nightside transition region, leading to the physical understanding of system dynamics and energy transport across all scales. -
James A. Slavin
James A. Slavin Professor of Space Physics Department of Climate and Space Science & Engineering University of Michigan, College of Engineering Climate & Space Research Building Ann Arbor, MI, 48109 Phone: 240-476-8009 [email protected] EDUCATION: 1982 - Ph.D., Space Physics, University of California at Los Angeles Dissertation: Bow Shock Studies at Mercury, Venus, Earth and Mars with Applications ot the Solar – Planetary Interaction Problem; Advisor: Prof. Robert E. Holzer 1978 - M.S., Geophysics and Space Physics, University of California at Los Angeles 1976 - B.S., Physics, Case Western Reserve University APPOINTMENTS: 2011 - 2018 Chair, Department of Climate and Space Sciences & Engineering, University of Michigan 2005 - 2011 Director, Heliophysics Science Division 1990 - 2004 Head, Electrodynamics Branch 1987 - 1989 Staff Scientist, NASA/GSFC Laboratory for Extraterrestrial Physics 1986 - 1987 Discipline Scientist for Magnetospheric Physics, Space Physics Division, NASA Headquarters 1983 - 1986 Research Scientist, Astrophysics and Space Physics Section, Caltech/Jet Propulsion Laboratory HONORS: 2018 - Heliophysics Summer School Faculty, UCAR High Altitude Observatory 2017 - NASA Group Achievement Award, MESSENGER Project Team 2017 - Asia Oceania Geosciences Society 14th Annual Meeting Distinguished Lecturer in Planetary Sciences 2016 - NASA Group Achievement Award, MMS Instument Suite 2012 - International Academy of Astronautics Laurels for Team Achievement for MESSENGER 2012 - Fellow, American Geophysical Union 2009 - NASA Group -
Soviet Steps Toward Permanent Human Presence in Space
SALYUT: Soviet Steps Toward Permanent Human Presence in Space December 1983 NTIS order #PB84-181437 Recommended Citation: SALYUT: Soviet Steps Toward Permanent Human Presence in Space–A Technical Mere- orandum (Washington, D. C.: U.S. Congress, Office of Technology Assessment, OTA- TM-STI-14, December 1983). Library of Congress Catalog Card Number 83-600624 For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 Foreword As the other major spacefaring nation, the Soviet Union is a subject of interest to the American people and Congress in their deliberations concerning the future of U.S. space activities. In the course of an assessment of Civilian Space Stations, the Office of Technology Assessment (OTA) has undertaken a study of the presence of Soviets in space and their Salyut space stations, in order to provide Congress with an informed view of Soviet capabilities and intentions. The major element in this technical memorandum was a workshop held at OTA in December 1982: it was the first occasion when a significant number of experts in this area of Soviet space activities had met for extended unclassified discussion. As a result of the workshop, OTA prepared this technical memorandum, “Salyut: Soviet Steps Toward Permanent Human Presence in Space. ” It has been reviewed extensively by workshop participants and others familiar with Soviet space activities. Also in December 1982, OTA wrote to the U. S. S. R.’s Ambassador to the United States Anatoliy Dobrynin, requesting any information concerning present and future Soviet space activities that the Soviet Union judged could be of value to the OTA assess- ment of civilian space stations. -
The Space-Based Global Observing System in 2010 (GOS-2010)
WMO Space Programme SP-7 The Space-based Global Observing For more information, please contact: System in 2010 (GOS-2010) World Meteorological Organization 7 bis, avenue de la Paix – P.O. Box 2300 – CH 1211 Geneva 2 – Switzerland www.wmo.int WMO Space Programme Office Tel.: +41 (0) 22 730 85 19 – Fax: +41 (0) 22 730 84 74 E-mail: [email protected] Website: www.wmo.int/pages/prog/sat/ WMO-TD No. 1513 WMO Space Programme SP-7 The Space-based Global Observing System in 2010 (GOS-2010) WMO/TD-No. 1513 2010 © World Meteorological Organization, 2010 The right of publication in print, electronic and any other form and in any language is reserved by WMO. Short extracts from WMO publications may be reproduced without authorization, provided that the complete source is clearly indicated. Editorial correspondence and requests to publish, reproduce or translate these publication in part or in whole should be addressed to: Chairperson, Publications Board World Meteorological Organization (WMO) 7 bis, avenue de la Paix Tel.: +41 (0)22 730 84 03 P.O. Box No. 2300 Fax: +41 (0)22 730 80 40 CH-1211 Geneva 2, Switzerland E-mail: [email protected] FOREWORD The launching of the world's first artificial satellite on 4 October 1957 ushered a new era of unprecedented scientific and technological achievements. And it was indeed a fortunate coincidence that the ninth session of the WMO Executive Committee – known today as the WMO Executive Council (EC) – was in progress precisely at this moment, for the EC members were very quick to realize that satellite technology held the promise to expand the volume of meteorological data and to fill the notable gaps where land-based observations were not readily available. -
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. -
FY06 PAR.Indb
National Aeronautics and Space Administration r a 6 e Y PPeerrffoormancermance aandnd 0 l Performance and a c 0 s i F Fiscal Year 2 2006 Fiscal Year 2006 AccountabilityAAccountabilityccountability ReportRRepoeporrtt Table of Contents PART 1: MANAGEMENT DISCUSSION & ANALYSIS . .1 Mission, Vision, Values, & Organization . .3 NASA’s Mission Is on Track . .3 Making Progress . .3 NASA’s Values . .4 NASA’s Organization . .4 NASA Headquarters . .4 Building Healthy NASA Centers . .5 Measuring NASA’s Performance . .7 Establishing Government Performance and Results Act (GPRA) Performance Measures . .7 Rating NASA’s Performance . .7 Program Assessment Rating Tool (PART) . .12 President’s Management Agenda (PMA) . .12 Major Program Annual Reports . .13 Performance Overview . .15 Progress Toward Achieving NASA’s Strategic Goals . .15 A Guide to Performance Overviews . .15 Strategic Goal 1: Fly the Shuttle as safely as possible until its retirement, not later than 2010. .16 Strategic Goal 2: Complete the International Space Station in a manner consistent with NASA’s International Partner commitments and the needs of human exploration. .18 Goal 3: Develop a balanced overall program of science, exploration, and aeronautics consistent with the redirection of the human spacefl ight program to focus on exploration. .20 Sub-goal 3A: Study Earth from space to advance scientifi c understanding and meet societal needs. .22 Sub-goal 3B: Understand the Sun and its effects on Earth and the solar system. .25 Sub-goal 3C: Advance scientifi c knowledge of the origin and history of the solar system, the potential for life elsewhere, and the hazards and resources present as humans explore space. .28 Sub-goal 3D: Discover the origin, structure, evolution, and destiny of the universe, and search for Earth-like planets. -
The Flight Plan
M A R C H 2 0 2 1 THE FLIGHT PLAN The Newsletter of AIAA Albuquerque Section The American Institute of Aeronautics and Astronautics AIAA ALBUQUERQUE MARCH 2021 SECTION MEETING: MAKING A DIFFERENCE A T M A C H 2 . Presenter. Lt. Col. Tucker Hamilton Organization USAF F-35 Developmental Test Director of Operations INSIDE THIS ISSUE: Abstract I humbly present my flying experiences through SECTION CALENDAR 2 pictures and videos of what it takes and what it is like to be an Experimental Fighter Test Pilot. My personal stories include NATIONAL AIAA EVENTS 2 major life-threatening aircraft accidents, close saves, combat SPACE NUCLEAR PROPULSION REPORT 3 flying revelations, serendipitous opportunities testing first of its kind technology, flying over 30 aircraft from a zeppelin to a ALBUQUERQUE DECEMBER MEETING 5 MiG-15 to an A-10, and managing the Joint Strike Fighter De- velopmental Test program for all three services. Through ALBUQUERQUE JANUARY MEETING 6 these experiences you will learn not just what a Test Pilot does, but also gain encour- ALBUQUERQUE FEBRUARY MEETING 7 agement through my lessons learned on how to make a difference in your local com- munities…did I mention cool flight test videos! CALL FOR SCIENCE FAIR JUDGES 9 Lt Col Tucker "Cinco" Hamilton started his Air Force career as an CALL FOR SCHOLARSHIP APPLICATIONS 10 operational F-15C pilot. He supported multiple Red Flag Exercises and real world Operation Noble Eagle missions where he protect- NEW AIAA HIGH SCHOOL MEMBERSHIPS 10 ed the President of the United States; at times escorting Air Force One. -
Failures in Spacecraft Systems: an Analysis from The
FAILURES IN SPACECRAFT SYSTEMS: AN ANALYSIS FROM THE PERSPECTIVE OF DECISION MAKING A Thesis Submitted to the Faculty of Purdue University by Vikranth R. Kattakuri In Partial Fulfillment of the Requirements for the Degree of Master of Science in Mechanical Engineering August 2019 Purdue University West Lafayette, Indiana ii THE PURDUE UNIVERSITY GRADUATE SCHOOL STATEMENT OF THESIS APPROVAL Dr. Jitesh H. Panchal, Chair School of Mechanical Engineering Dr. Ilias Bilionis School of Mechanical Engineering Dr. William Crossley School of Aeronautics and Astronautics Approved by: Dr. Jay P. Gore Associate Head of Graduate Studies iii ACKNOWLEDGMENTS I am extremely grateful to my advisor Prof. Jitesh Panchal for his patient guidance throughout the two years of my studies. I am indebted to him for considering me to be a part of his research group and for providing this opportunity to work in the fields of systems engineering and mechanical design for a period of 2 years. Being a research and teaching assistant under him had been a rewarding experience. Without his valuable insights, this work would not only have been possible, but also inconceivable. I would like to thank my co-advisor Prof. Ilias Bilionis for his valuable inputs, timely guidance and extremely engaging research meetings. I thank my committee member, Prof. William Crossley for his interest in my work. I had a great opportunity to attend all three courses taught by my committee members and they are the best among all the courses I had at Purdue. I would like to thank my mentors Dr. Jagannath Raju of Systemantics India Pri- vate Limited and Prof. -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 3 July–September 2019 CONTENTS FOCUS ..................................................................................................................... 1 A new European Commission DG for Defence Industry and Space .............................................. 1 SPACE POLICY AND PROGRAMMES .................................................................................... 2 EUROPE ................................................................................................................. 2 EEAS announces 3SOS initiative building on COPUOS sustainability guidelines ............................ 2 Europe is a step closer to Mars’ surface ......................................................................... 2 ESA lunar exploration project PROSPECT finds new contributor ............................................. 2 ESA announces new EO mission and Third Party Missions under evaluation ................................ 2 ESA advances space science and exploration projects ........................................................ 3 ESA performs collision-avoidance manoeuvre for the first time ............................................. 3 Galileo's milestones amidst continued development .......................................................... 3 France strengthens its posture on space defence strategy ................................................... 3 Germany reveals promising results of EDEN ISS project ....................................................... 4 ASI strengthens -
ODQN 10-3.Indd
National Aeronautics and Space Administration Orbital Debris Quarterly News Volume 10, Issue 3 July 2006 First Satellite Breakups of 2006 The first significant breakup of a satellite in cm) to be tracked by the U.S. Space Surveillance Earth orbit in nearly a year occurred on 4 May 2006 Network (SSN). Of these, 49 had been officially when a 20-year-old Soviet rocket body fragmented cataloged by mid-June. The accompanying figure Inside... without warning. This was the fifth time since 1988 indicates the orbits of 44 debris, including the main ISS Large Area that a launch vehicle orbital stage of this type ex- remnant of the orbital stage, about one week after Debris Collector perienced a spontaneous explosion after spending the event. many years in a dormant state. A little more than Although the lowest perigees were greater than (LAD-C) Update .........2 a month later, a Russian Proton fourth stage ullage 500 km, some of the debris exhibited significant th STS-114 motor broke-up, the 34 on-orbit fragmentation of decay rates, indicating that their area-to-mass ratios this component type since 1984. were noticeably higher than typical debris. Nine de- Micrometeoroid/ A Tsyklon third stage (International Designa- bris had already reentered by mid-June, and a total Orbital Debris tor 1985-108B, U.S. Satellite Number 16263) had of two dozen or more debris are expected to reenter (MMOD) Post-Flight been used to insert Cosmos 1703 into an orbit of by mid-August. Consequently, the overall effect of Assessment ...............2 635 km by 665 km with an inclination of 82.5°. -
Goddard's Terra and Aqua Help Determine Extent of Oil Spill
Page 1 The Critical Path A Flight Projects Directorate Publication Volume 18 number 2 A Newsletter Published for Code 400 Employees 2010 Summer/Fall INSIDE THIS ISSUE: The Distress Goddard’s Page 1 Alerting Satellite DESDynI DASS System (DASS) It’s not the Biggest! It’s not DESDynl Page 1 -Taking the search out of the Baddest! It’s not the most Search and Rescue- Terra & Aqua Help expensive! It’s not even the Page1 Oil Spill most Well Known!Known But, God- Introduction dard’s newest Deformation, Message From The NASA, which pioneered the tech- Page 2 Ecosystem Structure, Dynamics Director Of nology used for the satellite-aided of Ice (DESDynI’s) Light Detec- search and rescue capability that Tintype Page 3 tion and Ranging (LIDAR) mis- has saved more than 28,000 lives sion promises to deliver the worldwide since its inception Honor Awards Page 14 most comprehensive set of data nearly three decades ago, has when it comes to mapping the developed new technology that Earth’s vegetation canopy and Holocaust Memorial Page 19 will more quickly identify the loca- its evolution. This mission will tions of people in distress and re- Peer Awards Page 22 set out to answer the tough duce the risk to rescuers. This is questions of how the Earth's being accomplished in the Search Christmas in April Page 23 carbon cycle and ecosystems and Rescue Mission Office at are changing. We know that Cultural Tidbit Page 25 (DASS Continued on page 4) (DESDynl Continued on page 10) Things You Should Page 25 Know Social News Page 26 Goddard’s Terra and Aqua Help Determine Extent of Oil Spill Comings & Goings Page 27 Quotes Page 27 (Oil Spill Continued on page 20) Future Launches Page 28 2010 Summer/Fall Issue Page 2 The Critical Path Message from the Director Of Greetings: It’s mid-August already. -
Gao-13-597, Geostationary Weather Satellites
United States Government Accountability Office Report to the Committee on Science, Space, and Technology, House of Representatives September 2013 GEOSTATIONARY WEATHER SATELLITES Progress Made, but Weaknesses in Scheduling, Contingency Planning, and Communicating with Users Need to Be Addressed GAO-13-597 September 2013 GEOSTATIONARY WEATHER SATELLITES Progress Made, but Weaknesses in Scheduling, Contingency Planning, and Communicating with Users Need to Be Addressed Highlights of GAO-13-597, a report to the Committee on Science, Space, and Technology, House of Representatives Why GAO Did This Study What GAO Found NOAA, with the aid of the National The National Oceanic and Atmospheric Administration (NOAA) has completed Aeronautics and Space Administration the design of its Geostationary Operational Environmental Satellite-R (GOES-R) (NASA), is procuring the next series and made progress in building flight and ground components. While the generation of geostationary weather program reports that it is on track to stay within its $10.9 billion life cycle cost satellites. The GOES-R series is to estimate, it has not reported key information on reserve funds to senior replace the current series of satellites management. Also, the program has delayed interim milestones, is experiencing (called GOES-13, -14, and -15), which technical issues, and continues to demonstrate weaknesses in the development will likely begin to reach the end of of component schedules. These factors have the potential to affect the expected their useful lives in 2015. This new October 2015 launch date of the first GOES-R satellite, and program officials series is considered critical to the now acknowledge that the launch date may be delayed by 6 months.