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Shock Connectivity and the Late Cycle 24 Solar Energetic Particle Events in July and September 2017
Shock Connectivity and the Late Cycle 24 Solar Energetic Particle Events in July and September 2017 J.G. Luhmann1, M.L. Mays2, Yan Li1, C.O. Lee1, H. Bain3, D. Odstrcil4, R.A. Mewaldt5, C.M.S. Cohen5, D. Larson1, Gordon Petrie6 1Space Sciences Laboratory, University of California, Berkeley. 2CCMC, NASA Goddard Space Flight Center. 3NOAA Space Weather Prediction Center. 4George Mason University. 5California Institute of Technology. 6NSO. Corresponding author: Janet Luhmann ([email protected]) Key Points: Observer shock connectivity explains the SEP observations during the July and September 2017 events. The July and September 2017 solar and SEP events had similar characteristics due to similar source region and eruptions. The July and September 2017 events seemed to arise in conjunction with the appearance of a pseudostreamer, a possible alternate ICME source. This article has been accepted for publication and undergone full peer review but has not been through the copyediting, typesetting, pagination and proofreading process which may lead to differences between this version and the Version of Record. Please cite this article as doi: 10.1029/2018SW001860 © 2018 American Geophysical Union. All rights reserved. Abstract As solar activity steadily declined toward the cycle 24 minimum in the early months of 2017, the expectation for major Solar Energetic Particle (SEP) events diminished with the sunspot number. It was thus surprising (though not unprecedented) when a new, potentially significant active region rotated around the East limb in early July that by mid-month was producing a series of coronal eruptions, reaching a crescendo around July 23. This series, apparently associated with the birth of a growing pseudostreamer, produced the largest SEP event(s) seen since the solar maximum years. -
Delta II Icesat-2 Mission Booklet
A United Launch Alliance (ULA) Delta II 7420-10 photon-counting laser altimeter that advances MISSION rocket will deliver the Ice, Cloud and land Eleva- technology from the first ICESat mission tion Satellite-2 (ICESat-2) spacecraft to a 250 nmi launched on a Delta II in 2003 and operated until (463 km), near-circular polar orbit. Liftoff will 2009. Our planet’s frozen and icy areas, called occur from Space Launch Complex-2 at Vanden- the cryosphere, are a key focus of NASA’s Earth berg Air Force Base, California. science research. ICESat-2 will help scientists MISSION investigate why, and how much, our cryosphere ICESat-2, with its single instrument, the is changing in a warming climate, while also Advanced Topographic Laser Altimeter System measuring heights across Earth’s temperate OVERVIEW (ATLAS), will provide scientists with height and tropical regions and take stock of the vege- measurements to create a global portrait of tation in forests worldwide. The ICESat-2 mission Earth’s third dimension, gathering data that can is implemented by NASA’s Goddard Space Flight precisely track changes of terrain including Center (GSFC). Northrop Grumman built the glaciers, sea ice, forests and more. ATLAS is a spacecraft. NASA’s Launch Services Program at Kennedy Space Center is responsible for launch management. In addition to ICESat-2, this mission includes four CubeSats which will launch from dispens- ers mounted to the Delta II second stage. The CubeSats were designed and built by UCLA, University of Central Florida, and Cal Poly. The miniaturized satellites will conduct research DELTA II For nearly 30 years, the reliable in space weather, changing electric potential Delta II rocket has been an industry and resulting discharge events on spacecraft workhorse, launching critical and damping behavior of tungsten powder in a capabilities for NASA, the Air Force Image Credit NASA’s Goddard Space Flight Center zero-gravity environment. -
The Van Allen Probes' Contribution to the Space Weather System
L. J. Zanetti et al. The Van Allen Probes’ Contribution to the Space Weather System Lawrence J. Zanetti, Ramona L. Kessel, Barry H. Mauk, Aleksandr Y. Ukhorskiy, Nicola J. Fox, Robin J. Barnes, Michele Weiss, Thomas S. Sotirelis, and NourEddine Raouafi ABSTRACT The Van Allen Probes mission, formerly the Radiation Belt Storm Probes mission, was renamed soon after launch to honor the late James Van Allen, who discovered Earth’s radiation belts at the beginning of the space age. While most of the science data are telemetered to the ground using a store-and-then-dump schedule, some of the space weather data are broadcast continu- ously when the Probes are not sending down the science data (approximately 90% of the time). This space weather data set is captured by contributed ground stations around the world (pres- ently Korea Astronomy and Space Science Institute and the Institute of Atmospheric Physics, Czech Republic), automatically sent to the ground facility at the Johns Hopkins University Applied Phys- ics Laboratory, converted to scientific units, and published online in the form of digital data and plots—all within less than 15 minutes from the time that the data are accumulated onboard the Probes. The real-time Van Allen Probes space weather information is publicly accessible via the Van Allen Probes Gateway web interface. INTRODUCTION The overarching goal of the study of space weather ing radiation, were the impetus for implementing a space is to understand and address the issues caused by solar weather broadcast capability on NASA’s Van Allen disturbances and the effects of those issues on humans Probes’ twin pair of satellites, which were launched in and technological systems. -
Town Hall PP Ehrenfreund TA
Vision and Voyages For Planetary Science in the Decade 2013-2022 What Is A Decadal Survey? • Once every ten years, at the request of NASA and NSF, the National Research Council carries out a “decadal survey” for planetary science. • The decadal survey involves broad participation from the planetary science community. • It is the primary scientific input that NASA and NSF use to design their programs of planetary science and exploration. • This decadal survey applies to the decade from 2013 to 2022. 2 Guiding Principles • Science Comes First: All recommendations must be first and foremost science-driven. • Community Involvement: Solicit community input throughout the process. • Transparency and Openness: Make the process as open and visible to all interested members of the community as possible. 3 Committee Organization Steering Group Steve Squyres, Chair Larry Soderblom, Vice Chair Vice Chairs of Panels 9 others Inner Planets Outer Planets Primitive Bodies Panel Panel Panel Ellen Stofan, Chair Heidi Hammel, Chair Joe Veverka, Chair Steve Mackwell, Vice Chair Amy Simon-Miller, Vice Chair Hap McSween, Vice Chair 10 others 9 others 10 others Mars Outer Planet Panel Satellites Panel Phil Christensen, Chair John Spencer, Chair Wendy Calvin, Vice Chair Dave Stevenson, Vice Chair 9 others 10 others 4 Inputs From The Community • The goal of the decadal survey is to seek out the community’s views, and build a consensus around those views. • More than a dozen town hall meetings were held: AGU (twice), LPSC (twice), DPS (twice), EPSC, RAS, AbSciCon, NLSI, LEAG, VEXAG, OPAG, MEPAG, CAPTEM, etc. • The community submitted 199 white papers with 1669 individual authors and endorsers. -
Why NASA Consistently Fails at Congress
W&M ScholarWorks Undergraduate Honors Theses Theses, Dissertations, & Master Projects 6-2013 The Wrong Right Stuff: Why NASA Consistently Fails at Congress Andrew Follett College of William and Mary Follow this and additional works at: https://scholarworks.wm.edu/honorstheses Part of the Political Science Commons Recommended Citation Follett, Andrew, "The Wrong Right Stuff: Why NASA Consistently Fails at Congress" (2013). Undergraduate Honors Theses. Paper 584. https://scholarworks.wm.edu/honorstheses/584 This Honors 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 Undergraduate Honors Theses by an authorized administrator of W&M ScholarWorks. For more information, please contact [email protected]. The Wrong Right Stuff: Why NASA Consistently Fails at Congress A thesis submitted in partial fulfillment of the requirement for the degree of Bachelors of Arts in Government from The College of William and Mary by Andrew Follett Accepted for . John Gilmour, Director . Sophia Hart . Rowan Lockwood Williamsburg, VA May 3, 2013 1 Table of Contents: Acknowledgements 3 Part 1: Introduction and Background 4 Pre Soviet Collapse: Early American Failures in Space 13 Pre Soviet Collapse: The Successful Mercury, Gemini, and Apollo Programs 17 Pre Soviet Collapse: The Quasi-Successful Shuttle Program 22 Part 2: The Thin Years, Repeated Failure in NASA in the Post-Soviet Era 27 The Failure of the Space Exploration Initiative 28 The Failed Vision for Space Exploration 30 The Success of Unmanned Space Flight 32 Part 3: Why NASA Fails 37 Part 4: Putting this to the Test 87 Part 5: Changing the Method. -
Numerical Investigation of a Novel RBCC Ejector Configuration
Numerical Investigation of a Novel RBCC Ejector Configuration Compared to a Traditional Circular Ejector by Adrian Gerber A Thesis submitted to the Faculty of Graduate Studies and Research in partial fulfilment of the requirements for the degree of Master of Applied Science in Mechanical and Aerospace Engineering Carleton University Ottawa, Ontario, Canada March 2015 Copyright c 2015 - Adrian Gerber Abstract The rocket based combined cycle can be an alternative engine to power a vehicle into space. The engine has 4 stages and one of the more challenging stages to in- crease performance is the first stage, the ejector stage. One proposed method to increase performance is by achieving higher entrainment performance and mixing at low free-stream velocities. The Exchange Inlet is used as an alternative nozzle to achieve this performance. The Exchange Inlet is compared to a conical nozzle within a RBCC engine with computational fluid dynamics at various pressures. The mixing and entrainment properties are compared between the two engine configurations and additional cases are investigated with shorter mixing sections to further investigate these properties. The Exchange Inlet is found to have better entrainment than the circular nozzle in all cases. ii For my mother, who always pushed me to never give up. iii Acknowledgments I would like to thank my professor for patiently pushing, motivating, and always showing me a little bit of light and knowledge at the end of every turn. I would also like to thank my family, friends, and girlfriend especially for the constant support and patience. iv Table of Contents Abstract ii Acknowledgments iv List of Tables vii List of Figures viii List of Acronyms xii List of Symbols xiv 1 Introduction 1 1.1 Background . -
Pete Aldridge Well, Good Afternoon, Ladies and Gentlemen, and Welcome to the Fifth and Final Public Hearing of the President’S Commission on Moon, Mars, and Beyond
The President’s Commission on Implementation of United States Space Exploration Policy PUBLIC HEARING Asia Society 725 Park Avenue New York, NY Monday, May 3, and Tuesday, May 4, 2004 Pete Aldridge Well, good afternoon, ladies and gentlemen, and welcome to the fifth and final public hearing of the President’s Commission on Moon, Mars, and Beyond. I think I can speak for everyone here when I say that the time period since this Commission was appointed and asked to produce a report has elapsed at the speed of light. At least it seems that way. Since February, we’ve heard testimonies from a broad range of space experts, the Mars rovers have won an expanded audience of space enthusiasts, and a renewed interest in space science has surfaced, calling for a new generation of space educators. In less than a month, we will present our findings to the White House. The Commission is here to explore ways to achieve the President’s vision of going back to the Moon and on to Mars and beyond. We have listened and talked to experts at four previous hearings—in Washington, D.C.; Dayton, Ohio; Atlanta, Georgia; and San Francisco, California—and talked among ourselves and we realize that this vision produces a focus not just for NASA but a focus that can revitalize US space capability and have a significant impact on our nation’s industrial base, and academia, and the quality of life for all Americans. As you can see from our agenda, we’re talking with those experts from many, many disciplines, including those outside the traditional aerospace arena. -
Gateway Program Acquisition Strategy Overview
70th International Astronautical Congress (IAC), Washington D.C., United States, 21-25 October 2019. Copyright ©2019 by the International Astronautical Federation (IAF). All rights reserved. IAC-19,E3,6,5,x53831 GATEWAY PROGRAM ACQUISITION STRATEGY OVERVIEW Emma Lehnhardta, Christopher Zavrelb, Nicole Herrmannc a National Aeronautics and Space Administration, Johnson Space Center, United States, [email protected] b Stellar Solutions Inc, United States, [email protected] c National Aeronautics and Space Administration, Headquarters, United States, [email protected] Abstract This paper will provide an overview of the acquisition strategy for the Gateway Program. The Gateway will be an outpost orbiting the Moon that provides vital support for a sustainable, long-term human return to the lunar surface, as well as a staging point for further deep space exploration. The Gateway will foster U.S. industry and international partnerships and enable multi-discipline utilization. The National Aeronautics and Space Administration (NASA) will lead this next step and will serve as the integrator of the spaceflight capabilities and contributions of U.S. commercial partners and international partners to develop the Gateway. The Gateway will be developed in a manner that will also allow future capabilities and collaborations with U.S. Government, private sector companies, and international partners. Gateway is embracing innovation and flexibility; both in system architecture and in procurement approach. The Gateway’s agile acquisition strategy will shape the entire system life cycle, from design and analysis through production, verification, launch, logistics and operations. This strategy will encourage new ways of doing business to accommodate new techniques, technologies and approaches; improving affordability and maximizing Gateway utility. -
Options and Issues for Nasa's Human Space Flight Program
OPTIONS AND ISSUES FOR NASA’S HUMAN SPACE FLIGHT PROGRAM: REPORT OF THE ‘‘REVIEW OF U.S. HUMAN SPACE FLIGHT PLANS’’ COMMITTEE HEARING BEFORE THE COMMITTEE ON SCIENCE AND TECHNOLOGY HOUSE OF REPRESENTATIVES ONE HUNDRED ELEVENTH CONGRESS FIRST SESSION SEPTEMBER 15, 2009 Serial No. 111–51 Printed for the use of the Committee on Science and Technology ( Available via the World Wide Web: http://www.science.house.gov U.S. GOVERNMENT PRINTING OFFICE 51–928PDF WASHINGTON : 2010 For sale by the Superintendent of Documents, U.S. Government Printing Office Internet: bookstore.gpo.gov Phone: toll free (866) 512–1800; DC area (202) 512–1800 Fax: (202) 512–2104 Mail: Stop IDCC, Washington, DC 20402–0001 COMMITTEE ON SCIENCE AND TECHNOLOGY HON. BART GORDON, Tennessee, Chair JERRY F. COSTELLO, Illinois RALPH M. HALL, Texas EDDIE BERNICE JOHNSON, Texas F. JAMES SENSENBRENNER JR., LYNN C. WOOLSEY, California Wisconsin DAVID WU, Oregon LAMAR S. SMITH, Texas BRIAN BAIRD, Washington DANA ROHRABACHER, California BRAD MILLER, North Carolina ROSCOE G. BARTLETT, Maryland DANIEL LIPINSKI, Illinois VERNON J. EHLERS, Michigan GABRIELLE GIFFORDS, Arizona FRANK D. LUCAS, Oklahoma DONNA F. EDWARDS, Maryland JUDY BIGGERT, Illinois MARCIA L. FUDGE, Ohio W. TODD AKIN, Missouri BEN R. LUJA´ N, New Mexico RANDY NEUGEBAUER, Texas PAUL D. TONKO, New York BOB INGLIS, South Carolina PARKER GRIFFITH, Alabama MICHAEL T. MCCAUL, Texas STEVEN R. ROTHMAN, New Jersey MARIO DIAZ-BALART, Florida JIM MATHESON, Utah BRIAN P. BILBRAY, California LINCOLN DAVIS, Tennessee ADRIAN SMITH, Nebraska BEN CHANDLER, Kentucky PAUL C. BROUN, Georgia RUSS CARNAHAN, Missouri PETE OLSON, Texas BARON P. HILL, Indiana HARRY E. -
Living with a Star Targeted Research and Technology (TR&T) Steering
Living with a Star Targeted Research and Technology (TR&T) Steering Committee Steering Committee Members: Liaison Members: Co-Chair: Eftyhia Zesta (GSFC) Terry Onsager (NOAA) Co-Chair: Mark Linton (NRL) Rodney Vierick (NOAA) Yuri Shprits (MIT) Ilia Roussev (NSF) Scott McIntosh (NCAR / HAO) Vyacheslav Lukin (NSF) Nathan Schwadron (UNH ex-chair) Masha Kuznetsova (GSFC / Community Karel Schrijver (Lockheed Martin) Coordinated Modeling Center) Jim Slavin (U Michigan) Mona Kessel (NASA HQ / Chadi Salem (UC Berkeley) Van Allen Probes) Alexa Halford (GSFC) Dean Pesnell (GSFC / Pontus Brandt (APL) Solar Dynamics Observatory) Tim Bastian (NRAO) David Sibeck (GSFC / Van Allen Probes) Kent Tobiska Adam Szabo (GSFC / Solar Probe Plus) (Space Environment Tech.) Chris St. Cyr (GSFC / Solar Orbiter) LWS Program Ex Officio: Elsayed Talaat & Jeff Morrill (NASA HQ), Shing Fung (GSFC) 2003 Science Definition Team Report: Living with a Star Objectives LWS initiative: goal-oriented research program targeting those aspects of the Sun-Earth system that directly affect life and society. The objectives of LWS will advance research in Sun-Earth system science to new territory, producing knowledge and understanding that society can ultimately utilize. 2003 LWS Science Definition Team Report: TR&T Program The Targeted Research and Technology (TR&T) component of LWS provides the theory, modeling, and data analysis necessary to enable an integrated, system-wide picture of Sun-Earth connection science with societal relevance. Science Definition Team (SDT) … formed -
The Evolving Launch Vehicle Market Supply and the Effect on Future NASA Missions
Presented at the 2007 ISPA/SCEA Joint Annual International Conference and Workshop - www.iceaaonline.com The Evolving Launch Vehicle Market Supply and the Effect on Future NASA Missions Presented at the 2007 ISPA/SCEA Joint International Conference & Workshop June 12-15, New Orleans, LA Bob Bitten, Debra Emmons, Claude Freaner 1 Presented at the 2007 ISPA/SCEA Joint Annual International Conference and Workshop - www.iceaaonline.com Abstract • The upcoming retirement of the Delta II family of launch vehicles leaves a performance gap between small expendable launch vehicles, such as the Pegasus and Taurus, and large vehicles, such as the Delta IV and Atlas V families • This performance gap may lead to a variety of progressions including – large satellites that utilize the full capability of the larger launch vehicles, – medium size satellites that would require dual manifesting on the larger vehicles or – smaller satellites missions that would require a large number of smaller launch vehicles • This paper offers some comparative costs of co-manifesting single- instrument missions on a Delta IV/Atlas V, versus placing several instruments on a larger bus and using a Delta IV/Atlas V, as well as considering smaller, single instrument missions launched on a Minotaur or Taurus • This paper presents the results of a parametric study investigating the cost- effectiveness of different alternatives and their effect on future NASA missions that fall into the Small Explorer (SMEX), Medium Explorer (MIDEX), Earth System Science Pathfinder (ESSP), Discovery, -
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.