National Center for Atmospheric Research 2018 Annual Report
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The Cubesat Mission to Study Solar Particles (Cusp) Walt Downing IEEE Life Senior Member Aerospace and Electronic Systems Society President (2020-2021)
The CubeSat Mission to Study Solar Particles (CuSP) Walt Downing IEEE Life Senior Member Aerospace and Electronic Systems Society President (2020-2021) Acknowledgements – National Aeronautics and Space Administration (NASA) and CuSP Principal Investigator, Dr. Mihir Desai, Southwest Research Institute (SwRI) Feature Articles in SYSTEMS Magazine Three-part special series on Artemis I CubeSats - April 2019 (CuSP, IceCube, ArgoMoon, EQUULEUS/OMOTENASHI, & DSN) ▸ - September 2019 (CisLunar Explorers, OMOTENASHI & Iris Transponder) - March 2020 (BioSentinnel, Near-Earth Asteroid Scout, EQUULEUS, Lunar Flashlight, Lunar Polar Hydrogen Mapper, & Δ-Differential One-Way Range) Available in the AESS Resource Center https://resourcecenter.aess.ieee.org/ ▸Free for AESS members ▸ What are CubeSats? A class of small research spacecraft Built to standard dimensions (Units or “U”) ▸ - 1U = 10 cm x 10 cm x 11 cm (Roughly “cube-shaped”) ▸ - Modular: 1U, 2U, 3U, 6U or 12U in size - Weigh less than 1.33 kg per U NASA's CubeSats are dispensed from a deployer such as a Poly-Picosatellite Orbital Deployer (P-POD) ▸NASA’s CubeSat Launch initiative (CSLI) provides opportunities for small satellite payloads to fly on rockets ▸planned for upcoming launches. These CubeSats are flown as secondary payloads on previously planned missions. https://www.nasa.gov/directorates/heo/home/CubeSats_initiative What is CuSP? NASA Science Mission Directorate sponsored Heliospheric Science Mission selected in June 2015 to be launched on Artemis I. ▸ https://www.nasa.gov/feature/goddard/2016/heliophys ics-cubesat-to-launch-on-nasa-s-sls Support space weather research by determining proton radiation levels during solar energetic particle events and identifying suprathermal properties that could help ▸ predict geomagnetic storms. -
Cornell University
Advanced CubeSat Technologies for Affordable Deep Space Science and Exploration Missions Ground Tournaments, the Moon, and Beyond Jim Cockrell Cube Quest Challenge Administrator iCubeSat - 30 May 2017 • What is Cube Quest? – Why a Cube Quest? – Rules and Prize Structure • Today’s Status Get your CubeSat to the moon, work the best – GT4 Competitors survive the longest win big prizes! – Emerging Technologies • Next Steps – GT4 winners – In-space Competition 30 May 2017 CubeQuest Challenge - iCubeSat 2 • SmallSats/CubeSats > conventional spacecraft – easier to launch – lower in cost • Unique missions with ensembles – planetary seismographs – array of Mars weather stations – distributed, correlated measurements – redundancy at the system level; robust system of systems – nodes for antenna arrays or telescope arrays – Augments traditional probes 30 May 2017 CubeQuest Challenge - iCubeSat 3 To-date, CubeSats don’t venture beyond LEO: Limitation SoA Deep Space Missions Need Limited comm range Low-gain dipoles or patches high gain directional antennas mainly used needed Limited comm data Low power, amateur band High-power, high frequency, wide rate transmitters mainly used bandwidth transmitters needed Lacking radiation COTS, low-cost parts used; more Radiation shielding, fault detection, tolerance benign environment of LEO fault tolerance Lacking in-space Not demonstrated (except solar High thrust, high ISP needed; propulsion sails); chemical fuel/pressurized chemical, electrical, solar containers prohibited Depend on Earth- Passive magnetorquers -
100 YEARS the Lightning Task Force THANK YOU to OUR SPONSORS!
VOL. 100 • NO. 1 • JAN 2019 Finding the Source of Dead Sea Sinkholes Want Tenure? Maybe It’s Time to Go Back to High School 100 YEARS The Lightning Task Force THANK YOU TO OUR SPONSORS! AGU would like to thank all of our generous partners and sponsors, whose contributions helped support Fall Meeting 2018. FROM THE EDITOR Editor in Chief Heather Goss, AGU, Washington, D. C., USA; [email protected] Editors Christina M. S. Cohen David Halpern 100 Years of Advancing Science California Institute of Technology Jet Propulsion Laboratory Pasadena, Calif., USA Pasadena, Calif., USA cohen@srl .caltech.edu davidhalpern29@gmail .com n 1919, two small science committees National Climate José D. Fuentes Carol A. Stein merged with the goal of supporting and Assessment was Department of Meteorology Department of Earth Pennsylvania State University and Environmental Sciences promoting geoscience research. Soon after, released recently, we University Park, Pa., USA University of Illinois at Chicago I [email protected] Chicago, Ill., USA the newly named American Geophysical published an exclu- [email protected] Union held its first meeting, with 25 mem- sive from the Wendy S. Gordon Ecologia Consulting bers, all elected to the society. About a decade report’s authors that Austin, Texas, USA later, membership restrictions lifted, and the put numbers to the wendy@ecologiaconsulting .com organization grew rapidly, creating a commu- deaths and costs we Editorial Advisory Board nity that embraced both the joy of science and could see if we don’t Mark G. Flanner, Atmospheric John W. Lane, Near-Surface its practical applications in fostering a sus- curb greenhouse gas Sciences Geophysics Nicola J. -
List of Private Spaceflight Companies - Wikipedia
6/18/2020 List of private spaceflight companies - Wikipedia List of private spaceflight companies This page is a list of non-governmental (privately owned) entities that currently offer—or are planning to offer—equipment and services geared towards spaceflight, both robotic and human. List of abbreviations used in this article Contents Commercial astronauts LEO: Low Earth orbit GTO: Geostationary transfer Manufacturers of space vehicles orbit Cargo transport vehicles VTOL: Vertical take-off and Crew transport vehicles landing Orbital SSTO: Single-stage-to-orbit Suborbital TSTO: Two-stage-to-orbit Launch vehicle manufacturers SSTSO: Single-stage-to-sub- Landers, rovers and orbiters orbit Research craft and tech demonstrators Propulsion manufacturers Satellite launchers Space-based economy Space manufacturing Space mining Space stations Space settlement Spacecraft component developers and manufacturers Spaceliner companies See also References External links Commercial astronauts Association of Spaceflight Professionals[1][2] — Astronaut training, applied research and development, payload testing and integration, mission planning and operations support (Christopher Altman, Soyeon Yi)[1][3] Manufacturers of space vehicles Cargo transport vehicles Dry Launch Return Company Launch Length Payload Diameter Generated Automated Spacecraft mass mass Payload (kg) payload S name system (m) volume (m3) (m) power (W) docking (kg) (kg) (kg) 10.0 (pressurized), 3,310 plus 14 2,500 Falcon 9 pressurized or (unpressurized), Dragon 6.1 4,200[4] 10,200 capsule -
Space Launch System Program March 1, 2018
https://ntrs.nasa.gov/search.jsp?R=20180003498 2019-08-31T15:55:45+00:00Z National Aeronautics and Space Administration 5 . 4 . 3 .SPACE . 2 . 1 . LAUNCH SYSTEM CubeSats - To The Moon & Beyond Scott Spearing CubeSat Subject Matter Expert Space Launch System Program March 1, 2018 www.nasa.gov/sls www.nasa.gov/sls SLS BLOCK 1 EXPLORATION MISSION-1 (EM-1) Forward Ring Launch Abort System Secondary Payloads Electrical Panels Cabling Orion Avionics Box (2 places) Interim Cryogenic Propulsion Stage Launch Vehicle Stage Adapter OSA Diaphragm Core Stage Secondary Payload Brackets (13) Boosters Isogrid Barrel Panels Access Cover Aft Ring (2 places) Orion Stage Adapter (OSA) www.nasa.gov/sls 0418 EM-1 OSA SECONDARY PAYLOAD ACCOMMODATIONS Secondary Payload Avionics Box Cabling 6U CubeSat Payload 6U CubeSat Secondary Payload Dispenser Brackets (13) (PSC) Secondary Payload Mounting Bracket LEGEND: SLS Provided PD Provided www.nasa.gov/sls 0418 EM-1 SYSTEM DESCRIPTION AND PURPOSE Expand and fully utilize the SLS capabilities for exploration purposes without causing harm or inconvenience to SLS or its primary payload. • Thirteen (max capability 17) 6U payload locations • 6U volume/mass is the current standard OSA (14 kg payload mass) Diaphragm • Payloads will be “powered off” from turnover through Orion separation and ~Ø156” (13’) payload deployment • Payload Deployment System Avionics Unit; payload deployment will begin with pre-loaded OSA ~21° sequence following Orion separation and ~22° ICPS disposal burn • Payload requirements captured in Interface -
Edison Pettit Papers: Finding Aid
http://oac.cdlib.org/findaid/ark:/13030/tf9q2nb3w2 No online items Edison Pettit Papers: Finding Aid Processed by Ronald S. Brashear in March 1998. The Huntington Library, Art Collections, and Botanical Gardens Manuscripts Department 1151 Oxford Road San Marino, California 91108 Phone: (626) 405-2191 Email: [email protected] URL: http://www.huntington.org © 1998 The Huntington Library. All rights reserved. Edison Pettit Papers: Finding Aid mssPettit papers 1 Overview of the Collection Title: Edison Pettit Papers Dates (inclusive): 1920-1969 Collection Number: mssPettit papers Creator: Pettit, Edison, 1889-1962. Extent: 6 boxes (3,100 pieces) Repository: The Huntington Library, Art Collections, and Botanical Gardens. Manuscripts Department 1151 Oxford Road San Marino, California 91108 Phone: (626) 405-2191 Email: [email protected] URL: http://www.huntington.org Abstract: This collection contains the papers of astronomer Edison Pettit (1889-1962), who was on the staff of the Mount Wilson and Palomar Observatories. The correspondence is chiefly with other astronomers in the United States and deals with astronomy in general including Pettit's work at Mount Wilson, telescopes, and ultraviolet light research. The rest of the collection is made up of manuscripts, notes, notebooks and printed items. Language: English. Access Open to qualified researchers by prior application through the Reader Services Department. For more information, contact Reader Services. Publication Rights The Huntington Library does not require that researchers request permission to quote from or publish images of this material, nor does it charge fees for such activities. The responsibility for identifying the copyright holder, if there is one, and obtaining necessary permissions rests with the researcher. -
JOHN ADAM FLEMING January 28,187/'-July 29,1956
NATIONAL ACADEMY OF SCIENCES J O H N A D A M F LEMING 1877—1956 A Biographical Memoir by M E R L E A . T UVE Any opinions expressed in this memoir are those of the author(s) and do not necessarily reflect the views of the National Academy of Sciences. Biographical Memoir COPYRIGHT 1967 NATIONAL ACADEMY OF SCIENCES WASHINGTON D.C. JOHN ADAM FLEMING January 28,187/'-July 29,1956 BY MERLE A. TUVE OHN ADAM FLEMING, who devoted his life to the study of ter- restrial magnetism and atmospheric electricity (perhaps the Jmost elusive of earth sciences), passed away quietly in San Mateo, California, on July 29, 1956. A resident of Chevy Chase, Maryland, for more than forty years, he was the retired Direc- tor of the Department of Terrestrial Magnetism, Carnegie In- stitution of Washington, where he had served forty-two years before his retirement in 1946. Dr. Fleming was born in Cincinnati, Ohio, January 28, 1877, the son of Americus Vespucius Fleming and Katherine Barbara (Ritzmann) Fleming. He was married twice, first to Henrietta Catherine Barbara Ratjen on June 17, 1903, at Lawrenceburg, Indiana, and after her death in 1912 he married her sister, Carolyn Ratjen, in 1913. He attended the University of Cincinnati during 1895-1899, majoring in civil engineering and chemistry, and received his B.S. degree in Civil Engineering "with highest distinction." The honorary degree of D.Sc. was conferred on him by the University of Cincinnati in 1933 and by Dartmouth College in 1934. After graduating from the University of Cincinnati he was employed as Assistant Engineer for the complete redesigning of the Convention Building for the Sanderbund Society at 104 BIOGRAPHICAL MEMOIRS Cincinnati. -
Beginning, Establishment and Early Development (1919- 1 1939)
1 IUGG: Beginning, Establishment and Early Development (1919- 2 1939) 3 Alik Ismail-Zadeh1,2 and Jo Ann Joselyn3 * 4 1 Karlsruhe Institute of Technology, Institute of Applied Geophysics, Karlsruhe, Germany 5 2 International Union of Geodesy and Geophysics, Secretariat, Potsdam, Germany 6 3 Space Environment Center, National Oceanic and Atmospheric Administration, Boulder, Colorado, USA 7 * Retired 8 Correspondence to: Alik Ismail-Zadeh ([email protected]); Jo Ann Joselyn ([email protected]) 9 Abstract. The International Union of Geodesy and Geophysics (IUGG) was established in 1919 to promote activities of 10 already-existing international scientific societies dealing with geodesy, terrestrial magnetism and electricity, meteorology, 11 physical oceanography, seismology, and volcanology. At the first General Assembly a section of scientific hydrology was 12 added, making a total of seven sections of the Union. This paper introduces IUGG by presenting its current mission, structure, 13 partners, and programs; discussing various international geophysical efforts before its origin; and, describing the Union’s 14 development from the end of World War I to the beginning of World War II. During this period (1919-1939), the number of 15 member countries increased from the nine founding member countries to 35; seven general assemblies were held, each in a 16 different international venue; and the number of delegates attending the assemblies increased from a few dozen to more than 17 800 scientists. At the Fifth General Assembly in 1933, the term “section” was replaced by “international association”. Each 18 general assembly of the Union, since the First General Assembly in Rome, Italy in 1922 to the VII General Assembly in 19 Washington, D.C., USA in 1939, is summarized, and the distinguished scientists who contributed to the Union’s formation 20 and it early development are introduced. -
From Ground Tournaments to Lunar and Deep Space Derby
NASA’s CubeQuest Challenge – From Ground Tournaments to Lunar and Deep Space Derby Liz Hyde1 Millennium Engineering and Integration, Moffett Field, CA, 94035 and Jim Cockrell2 NASA Ames Research Center, Moffett Field, CA, 94035 The First Flight of NASA’s Space Launch System will feature 13 CubeSats that will launch into cis-lunar space. Three of these CubeSats are winners of the CubeQuest Challenge, part of NASA’s Space Technology Mission Directorate (STMD) Centennial Challenge Program. In order to qualify for launch on EM-1, the winning teams needed to win a series of Ground Tournaments, periodically held since 2015. The final Ground Tournament, GT-4, was held in May 2017, and resulted in the Top 3 selection for the EM-1 launch opportunity. The Challenge now proceeds to the in-space Derbies, where teams must build and test their spacecraft before launch on EM-1. Once in space, they will compete for a variety of Communications and Propulsion-based challenges. This is the first Centennial Challenge to compete in space and is a springboard for future in-space Challenges. In addition, the technologies gained from this challenge will also propel development of deep space CubeSats. Nomenclature ARC = Ames Research Center BCT = Blue Canyon Technologies CDR = Critical Design Review ConOps = Concept of Operations COTS = Commercial Off-The-Shelf CU-E3 = University of Colorado Earth Escape Explorer DSN = Deep Space Network EDU = Engineering Development Unit EM-1 = Exploration Mission 1 GRC = Glenn Research Center GT = Ground Tournament Isp = Specific Impulse LEO = Low-Earth Orbit MCR = Mission Concept Review mN = milinewtons MSFC = Marshall Space Flight Center PDR = Preliminary Design Review RACP = Resilient Affordable CubeSat Processor SAR = System Acceptance Review SDR = Software Defined Radio SLS = Space Launch System SRR = System Requirements Review 1 Mechanical Engineer, MEI, MS 213-6, Moffett Field, CA, AIAA Member. -
Cobham Overview
Advances in European Processor Technology Cobham Gaisler AB ESCCON 12 March 2019 ESTEC/ESA, Noordwijk, The Netherlands In October 2018, the MASCOT lander touched down on the Ryugu asteroid after hitching a ride with the Japanese Hayabusa 2 probe. MASCOT successfully completed its mission 325 million kilometers away from Earth! Cobham developed the MASCOT onboard computer based on their GR712RC processor. In year 2020, NASA’s Exploration Mission 1 to the Moon will carry 13 CubeSats of which 8 use LEON3FT SPARC processor technology either as IP cores, EEE components, or both, all supplied by Cobham: • CubeSat for Solar Particles (CuSP): GR712RC & LEON3FT IP • Near-Earth Asteroid Scout: GR712RC & LEON3FT IP • Lunar Flashlight: GR712RC & LEON3FT IP • BioSentinel: UT669 & LEON3FT IP • ArgoMoon: GR712RC • Lunar IceCube: LEON3FT IP • Earth Escape Explorer (CU-E3): LEON3FT IP • Lunar Polar Hydrogen Mapper (LunaH-Map): LEON3FT IP GR712RC - Dual-Core LEON3FT Processor An ongoing success story • Why choose GR712RC? • Flight proven technology • Highly integrated system on-chip solution • Low power solution • Simple package for assembly • Several single board computer designs • Selected by several ESA and NASA missions • Forward and backward compatible architecture • GR712RC value add • Radiation-hardened by design • A multi-core solution developed for space • Multiple SpaceWire interfaces with RMAP • Mil-Std-1553, SPI, CAN, I2C, Ethernet • CCSDS Telemetry and Telecommand on-chip • Outstanding floating-point performance - times two • Engage second -
Attitude Control for the Lumio Cubesat in Deep Space
70th International Astronautical Congress, Washington D.C., United States, 21-25 October 2019. Copyright 2019 by the authors. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-19,C1,6,4,x50894 ATTITUDE CONTROL FOR THE LUMIO CUBESAT IN DEEP SPACE A.´ Romero-Calvo,1 J. D. Biggs, 1 F. Topputo1 The Lunar Meteoroid Impact Observer(LUMIO) is a 12U CubeSat designed to observe, quantify, and characterize the impact of meteoroids on the lunar surface. The combination of a highly demanding Concept of Operations(ConOps) and the characteristics of the deep-space environment determine the configuration of the spacecraft. This paper presents the preliminary Attitude Determination and Control System(ADCS) design of LUMIO, the reaction wheels desaturation strategy and Moon tracking control laws. The proposed solution is shown to (a) prevent the saturation of the reaction wheels, (b) minimize propellant consumption, (c) minimize the parasitic ∆V , (d) keep the pointing angle below a certain limit, and e) maximize power generation. Although no attempt is made to optimize the control parameters, the most efficient alternative in terms of propellant consumption is identified. The proposed LUMIO design could lay the foundations for a standardized minimum mass and volume ADCS system for CubeSats operating in deep-space. Nomenclature ~ns Unit vector normal to surface A Actual DCM matrix Ω Aperture angle of a regular tetrahedron Hadamard’s product Ad Desired DCM matrix P Solar constant Ae Error DCM matrix R Reaction wheels -
Progress Toward Implementation of the 2013 Decadal Survey for Solar and Space Physics
Prepublication Copy – Subject to Further Editorial Correction Progress Toward Implementation of the 2013 Decadal Survey for Solar and Space Physics A Midterm Assessment ADVANCE COPY NOT FOR PUBLIC RELEASE BEFORE February 3, 2020 at 2:00 p.m. EST ___________________________________________________________________________________ PLEASE CITE AS A REPORT OF THE NATIONAL ACADEMIES OF SCIENCES, ENGINEERING, AND MEDICINE Committee on the Review of Progress Toward Implementing the Decadal Survey – Solar and Space Physics: A Science for a Technological Society Space Studies Board Division on Engineering and Physical Sciences A Consensus Study Report of PREPUBLICATION COPY – SUBJECT TO FURTHER EDITORIAL CORRECTION THE NATIONAL ACADEMIES PRESS 500 Fifth Street, NW Washington, DC 20001 This study is based on work supported by Contract XXXXXX with the XXXXXXXX. Any opinions, findings, conclusions, or recommendations expressed in this publication do not necessarily reflect the views of any agency or organization that provided support for the project. International Standard Book Number-13: XXX-X-XXX-XXXXX-X International Standard Book Number-10: X-XXX-XXXXX-X Digital Object Identifier: https://doi.org/10.17226/XXXXX Cover: Copies of this publication are available free of charge from Space Studies Board National Academies of Sciences, Engineering, and Medicine Keck Center of the National Academies 500 Fifth Street, NW Washington, DC 20001 Additional copies of this publication are available from the National Academies Press, 500 Fifth Street, NW, Keck 360, Washington, DC 20001; (800) 624-6242 or (202) 334-3313; http://www.nap.edu. Copyright 2019 by the National Academy of Sciences. All rights reserved. Printed in the United States of America Suggested citation: National Academies of Sciences, Engineering, and Medicine.