Project Management Insights from NASA’S Goddard Space Flight Center
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Robenschain GSFC July 2012
Goddard Space Flight Center NASA Goddard Space Flight Center • NASA’s first Space Flight Center (established 1959) • We TRANSFORM Human Understanding of Earth and Space • Largest Collection of Scientists & Engineers in the U.S. • Nearly 300 successful missions including the World’s First Weather Satellite and the Hubble Space Telescope • 2006 Nobel Prize in Physics [Big Bang/Cosmic Background] • Hubble Supported 2011 Nobel Prize in Physics • WMAP Team Awarded 2012 Gruber Prize for Cosmology 2 Our Facilities • GSFC Greenbelt, Maryland • GSFC Wallops Flight Facility, Virginia • IV&V Facility, West Virginia • Goddard Institute for Space Studies, New York Wallops Flight Facility • Ground Stations at White Sands Complex, New Mexico White Sands Complex Greenbelt Goddard Institute for Independent Verification and Space Studies Validation Facility 3 Our Lines of Business Cross Cutting Earth Science Technology and Capabilities Suborbital Platforms Astrophysics Planetary & Lunar Human Exploration Science & Operations Communications && Navigation GSFC’s Contributions to a Diverse Mission Portfolio QuikSCAT dinW dinW Voyager O-E1 O-E1 teoSer teoSer SBRE SBRE ACRIMSAT RHESSI TSOM TSOM TMMR TMMR Geotail OOHS OOHS aquA aquA ICESat DETMI DETMI SAMPEX Landsat 7 TRACE THEMIS TOPEX CALIPSO Tarer Tarer ECA ECA GRACE SORCE Cluster SOEP SOEP ODS ODS GEAMI GEAMI MIA MIA aruA aruA TSFA TSFA SGOE SGOE oPlar oPlar MGP MGP SMM SMM Solar-B XEBI XEBI PPN PPN Aquarius CloudSat TDRSS LMCD LMCD Osiris-Rex (Sample Return) PSBR PSBR PAMW PAMW TWINS Cassini (Instrument) -
Mission to Jupiter
This book attempts to convey the creativity, Project A History of the Galileo Jupiter: To Mission The Galileo mission to Jupiter explored leadership, and vision that were necessary for the an exciting new frontier, had a major impact mission’s success. It is a book about dedicated people on planetary science, and provided invaluable and their scientific and engineering achievements. lessons for the design of spacecraft. This The Galileo mission faced many significant problems. mission amassed so many scientific firsts and Some of the most brilliant accomplishments and key discoveries that it can truly be called one of “work-arounds” of the Galileo staff occurred the most impressive feats of exploration of the precisely when these challenges arose. Throughout 20th century. In the words of John Casani, the the mission, engineers and scientists found ways to original project manager of the mission, “Galileo keep the spacecraft operational from a distance of was a way of demonstrating . just what U.S. nearly half a billion miles, enabling one of the most technology was capable of doing.” An engineer impressive voyages of scientific discovery. on the Galileo team expressed more personal * * * * * sentiments when she said, “I had never been a Michael Meltzer is an environmental part of something with such great scope . To scientist who has been writing about science know that the whole world was watching and and technology for nearly 30 years. His books hoping with us that this would work. We were and articles have investigated topics that include doing something for all mankind.” designing solar houses, preventing pollution in When Galileo lifted off from Kennedy electroplating shops, catching salmon with sonar and Space Center on 18 October 1989, it began an radar, and developing a sensor for examining Space interplanetary voyage that took it to Venus, to Michael Meltzer Michael Shuttle engines. -
Nasa Advisory Council Human Exploration and Operations
NASA ADVISORY COUNCIL HUMAN EXPLORATION AND OPERATIONS COMMITTEE NASA Headquarters Washington, DC January 13-14, 2021 MEETING REPORT _____________________________________________________________ N. Wayne Hale, Chair ____________________________________________________________ Bette Siegel, Executive Secretary Table of Contents Call to Order 3 Commercial Crew Program 5 Public Comments 8 Artemis Program 9 SMD Artemis CLPS Activities 11 Moon to Mars Update 12 Solar System and Beyond 12 HERMES Instrument Update Artemis III SDT Update Advancing Biological and Physical Sciences Through Lunar Exploration 14 SMD Mars Science Update 14 Artemis Accords 15 Planetary Protection Activities 15 Discussion/Findings and Recommendations 16 Appendix A- Attendees Appendix B- HEOC Membership Appendix C- Presentations Appendix D- Agenda Appendix E- Chat Transcript Prepared by Joan M. Zimmermann Zantech IT, Inc. 2 January 13, 2021 Call to order and welcome Dr. Bette Siegel, Executive Secretary of the Human Exploration and Operations Committee (HEOC), called the meeting to order, and provided details of the Federal Advisory Committee Act (FACA), which provides governance rules for the meeting. She introduced Mr. N. Wayne Hale, Chair of the HEOC. Mr. Hale noted to the public that this particular HEO meeting counts as the last meeting of 2020, and the next scheduled meeting in March/April will be the first meeting of 2021. Mr. Hale welcomed three new members, Ms. Lynn Cline, Mr. David Thompson, and Mr. Kwatsi Alibaruho. The present meeting is focused on an update on the HEO areas, and a joint meeting with the NASA Advisory Council (NAC) Science Committee. Mr. Hale asked if NAC Chair, General Lester Lyles, who was attending the meeting virtually, had any remarks to proffer. -
NASA's Lunar Atmosphere and Dust Environment Explorer (LADEE)
Geophysical Research Abstracts Vol. 13, EGU2011-5107-2, 2011 EGU General Assembly 2011 © Author(s) 2011 NASA’s Lunar Atmosphere and Dust Environment Explorer (LADEE) Richard Elphic (1), Gregory Delory (1,2), Anthony Colaprete (1), Mihaly Horanyi (3), Paul Mahaffy (4), Butler Hine (1), Steven McClard (5), Joan Salute (6), Edwin Grayzeck (6), and Don Boroson (7) (1) NASA Ames Research Center, Moffett Field, CA USA ([email protected]), (2) Space Sciences Laboratory, University of California, Berkeley, CA USA, (3) Laboratory for Atmospheric and Space Physics, University of Colorado, Boulder, CO USA, (4) NASA Goddard Space Flight Center, Greenbelt, MD USA, (5) LunarQuest Program Office, NASA Marshall Space Flight Center, Huntsville, AL USA, (6) Planetary Science Division, Science Mission Directorate, NASA, Washington, DC USA, (7) Lincoln Laboratory, Massachusetts Institute of Technology, Lexington MA USA Nearly 40 years have passed since the last Apollo missions investigated the mysteries of the lunar atmosphere and the question of levitated lunar dust. The most important questions remain: what is the composition, structure and variability of the tenuous lunar exosphere? What are its origins, transport mechanisms, and loss processes? Is lofted lunar dust the cause of the horizon glow observed by the Surveyor missions and Apollo astronauts? How does such levitated dust arise and move, what is its density, and what is its ultimate fate? The US National Academy of Sciences/National Research Council decadal surveys and the recent “Scientific Context for Exploration of the Moon” (SCEM) reports have identified studies of the pristine state of the lunar atmosphere and dust environment as among the leading priorities for future lunar science missions. -
Estimating Gale to Hurricane Force Winds Using the Satellite Altimeter
VOLUME 28 JOURNAL OF ATMOSPHERIC AND OCEANIC TECHNOLOGY APRIL 2011 Estimating Gale to Hurricane Force Winds Using the Satellite Altimeter YVES QUILFEN Space Oceanography Laboratory, IFREMER, Plouzane´, France DOUG VANDEMARK Ocean Process Analysis Laboratory, University of New Hampshire, Durham, New Hampshire BERTRAND CHAPRON Space Oceanography Laboratory, IFREMER, Plouzane´, France HUI FENG Ocean Process Analysis Laboratory, University of New Hampshire, Durham, New Hampshire JOE SIENKIEWICZ Ocean Prediction Center, NCEP/NOAA, Camp Springs, Maryland (Manuscript received 21 September 2010, in final form 29 November 2010) ABSTRACT A new model is provided for estimating maritime near-surface wind speeds (U10) from satellite altimeter backscatter data during high wind conditions. The model is built using coincident satellite scatterometer and altimeter observations obtained from QuikSCAT and Jason satellite orbit crossovers in 2008 and 2009. The new wind measurements are linear with inverse radar backscatter levels, a result close to the earlier altimeter high wind speed model of Young (1993). By design, the model only applies for wind speeds above 18 m s21. Above this level, standard altimeter wind speed algorithms are not reliable and typically underestimate the true value. Simple rules for applying the new model to the present-day suite of satellite altimeters (Jason-1, Jason-2, and Envisat RA-2) are provided, with a key objective being provision of enhanced data for near-real- time forecast and warning applications surrounding gale to hurricane force wind events. Model limitations and strengths are discussed and highlight the valuable 5-km spatial resolution sea state and wind speed al- timeter information that can complement other data sources included in forecast guidance and air–sea in- teraction studies. -
MARS an Overview of the 1985–2006 Mars Orbiter Camera Science
MARS MARS INFORMATICS The International Journal of Mars Science and Exploration Open Access Journals Science An overview of the 1985–2006 Mars Orbiter Camera science investigation Michael C. Malin1, Kenneth S. Edgett1, Bruce A. Cantor1, Michael A. Caplinger1, G. Edward Danielson2, Elsa H. Jensen1, Michael A. Ravine1, Jennifer L. Sandoval1, and Kimberley D. Supulver1 1Malin Space Science Systems, P.O. Box 910148, San Diego, CA, 92191-0148, USA; 2Deceased, 10 December 2005 Citation: Mars 5, 1-60, 2010; doi:10.1555/mars.2010.0001 History: Submitted: August 5, 2009; Reviewed: October 18, 2009; Accepted: November 15, 2009; Published: January 6, 2010 Editor: Jeffrey B. Plescia, Applied Physics Laboratory, Johns Hopkins University Reviewers: Jeffrey B. Plescia, Applied Physics Laboratory, Johns Hopkins University; R. Aileen Yingst, University of Wisconsin Green Bay Open Access: Copyright 2010 Malin Space Science Systems. This is an open-access paper distributed under the terms of a Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. Abstract Background: NASA selected the Mars Orbiter Camera (MOC) investigation in 1986 for the Mars Observer mission. The MOC consisted of three elements which shared a common package: a narrow angle camera designed to obtain images with a spatial resolution as high as 1.4 m per pixel from orbit, and two wide angle cameras (one with a red filter, the other blue) for daily global imaging to observe meteorological events, geodesy, and provide context for the narrow angle images. Following the loss of Mars Observer in August 1993, a second MOC was built from flight spare hardware and launched aboard Mars Global Surveyor (MGS) in November 1996. -
LADEE PDS Mission Description Center Document Document No: DES-12.LADEE.LPMD Rev.: 1.5 Effective Date: 05-13-2014
Ames Research Title: LADEE PDS Mission Description Center Document Document No: DES-12.LADEE.LPMD Rev.: 1.5 Effective Date: 05-13-2014 Lunar Atmosphere and Dust Environment Explorer (LADEE) LADEE PDS Mission Description th May 13 , 2014 Ames Research Center Moffett Field, California National Aeronautics and Space Administration i Ames Research Title: LADEE PDS Mission Description Center Document Document No: DES-12.LADEE.LPMD Rev.: 1.5 Effective Date: 05-13-2014 This document is approved in accordance with LADEE Configuration Management Plan, C04.LADEE.CM, paragraph 3.6.1.1 Document Release Routing Approval Process. Page three of this document contains the approved routed release of this document. Approval Signatures _______________________________________ ___________ Butler Hine Date LADEE Project Manager _______________________________________ ___________ Gregory T. Delory Date LADEE Deputy Project Scientist _______________________________________ ___________ Date _______________________________________ ___________ Date ii Ames Research Title: LADEE PDS Mission Description Center Document Document No: DES-12.LADEE.LPMD Rev.: 1.5 Effective Date: 05-13-2014 This page is reserved for routing approval document iii Ames Research Title: LADEE PDS Mission Description Center Document Document No: DES-12.LADEE.LPMD Rev.: 1.5 Effective Date: 05-13-2014 REVISION HISTORY Rev. Description of Change Author(s) Effective Date 1.0 Initial draft G. Delory Nov 1, 2012 1.1 Resolved several TBDs G. Delory Nov 29, 2012 Updated TOC and prepared for conversion to PDF March 21, 1.2 G. Delory 2012 Baseline March 21, NC G. Delory 2012 Edited mission objective #2 as per PDS peer review 1.3 G. Delory April 4, 2013 results Updated mission timeline and orbit plots to reflect as- 1.4 G. -
Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M. -
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. -
Glossary of Acronyms and Definitions
CASSINI FINAL MISSION REPORT 2018 CASSINI FINAL MISSION REPORT 2019 1 Glossary of Acronyms and Definitions A A/D Analog-to-Digital AACS Attitude and Articulation Control Subsystem AAN Automatic Alarm Notification AB Approved By ABS timed Absolute Timed AC Acoustics AC Alternating Current ACC Accelerometer ACCE Accelerometer Electronics ACCH Accelerometer Head ACE Aerospace Communications & Information Expertise ACE Aerospace Control Environment ACE Air Coordination Element ACE Attitude Control Electronics ACI Accelerometer Interface ACME Antenna Calibration and Measurement Equipment ACP Aerosol Collector Pyrolyzer ACS Attitude Control Subsystem ACT Actuator ACT Automated Command Tracker ACTS Advanced Communications Technology Satellite AD Applicable Document ADAS AWVR Data Acquisition Software ADC Analog-to-Digital Converter ADP Automatic Data Processing AE Activation Energy AEB Agência Espacial Brasileira (Brazilian Space Agency) AF Air Force AFC AACS Flight Computer AFETR Air Force Eastern Test Range AFETRM Air Force Eastern Test Range Manual 2 CASSINI FINAL MISSION REPORT 2019 AFS Atomic Frequency Standard AFT Abbreviated Functional Test AFT Allowable Flight Temperature AFS Andrew File System AGC Automatic Gain Control AGU American Geophysical Union AHSE Assembly, Handling, & Support Equipment AIT Assembly, Integration & Test AIV Assembly, Integration & Verification AKR Auroral Kilometric Radiation AL Agreement Letter AL Aluminum AL Anomalously Large ALAP As Low As Practical ALARA As Low As Reasonably Achievable ALB Automated Link -
Jjmonl 1712.Pmd
alactic Observer John J. McCarthy Observatory G Volume 10, No. 12 December 2017 Holiday Theme Park See page 19 for more information The John J. McCarthy Observatory Galactic Observer New Milford High School Editorial Committee 388 Danbury Road Managing Editor New Milford, CT 06776 Bill Cloutier Phone/Voice: (860) 210-4117 Production & Design Phone/Fax: (860) 354-1595 www.mccarthyobservatory.org Allan Ostergren Website Development JJMO Staff Marc Polansky Technical Support It is through their efforts that the McCarthy Observatory Bob Lambert has established itself as a significant educational and recreational resource within the western Connecticut Dr. Parker Moreland community. Steve Barone Jim Johnstone Colin Campbell Carly KleinStern Dennis Cartolano Bob Lambert Route Mike Chiarella Roger Moore Jeff Chodak Parker Moreland, PhD Bill Cloutier Allan Ostergren Doug Delisle Marc Polansky Cecilia Detrich Joe Privitera Dirk Feather Monty Robson Randy Fender Don Ross Louise Gagnon Gene Schilling John Gebauer Katie Shusdock Elaine Green Paul Woodell Tina Hartzell Amy Ziffer In This Issue "OUT THE WINDOW ON YOUR LEFT"............................... 3 REFERENCES ON DISTANCES ................................................ 18 SINUS IRIDUM ................................................................ 4 INTERNATIONAL SPACE STATION/IRIDIUM SATELLITES ............. 18 EXTRAGALACTIC COSMIC RAYS ........................................ 5 SOLAR ACTIVITY ............................................................... 18 EQUATORIAL ICE ON MARS? ........................................... -
Doing Business with Wallops Flight Facility
National Aeronautics and Space Administration Doing Business with NASA’s Wallops Flight Facility NASA’s Wallops Flight Facility (WFF) in Virginia provides agile, low-cost flight and launch range ser- vices to meet government and commercial sector needs for accessing flight regimes worldwide from the Earth’s surface to the moon and beyond. As a multi-user facility with operational launch range, spaceport, and airfield assets, Wallops is well-positioned to meet ongoing and emerging needs in the science, aerospace, defense, and commercial industries. WALLOPS RANGE The Wallops Range supports many of the mission activities around WFF and abroad. Project managers utlize the support of range services to provide a broad array of technical and instrumentation services, such as radar, optical tracking, telemetry, meteorological, command and control, surveillance and recovery, financial analysis and engineering services to support scientific research and technology development. WALLOPS MOBILE ASSETS Wallops has semi-permanent downrange instrumentation as well as mobile instrumentation to include radar, telemetry, command/control, and data systems that can be transported to offsite and remote locations. Campaigns have been conducted from the semi-permanent locations in Bermuda and North Carolina, as well as from the Arctic and Antarctic regions, South America, Africa, Europe, Australia and even at sea, with our mobile systems. WFF personnel have extensive experience in planning and conducting downrange support and mobile campaigns, developing equipment and systems to support these operations. Downrange and mobile systems include the following: C-band radar, meteorology, optical tracking, orbital tracking, flight termination, telemetry, timing, surveillance, and recovery. Keith Thompson, Wallops Advanced Projects Office | 757-824-1680 www.nasa.gov/wallops MID-ATLANTIC REGIONAL SPACEPORT Virginia’s Mid-Atlantic Regional Spaceport at Wallops supports two launch facilities, one medium-lift liquid-fueled pad and a medium-lift solid propellant pad.