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Telephone Directory October 1962
TELEPHONE DIRECTORY . MANNED SPACECRAFT CENTER HOUSTON 1, TEXAS I OCTOBER 1962 INTERNAL USE ONl Y INDEX HOUSTON MANNED SPACECRAFT CENTER TELEPHONE • DIRECTORY ALPHABETICAL .....................................................•................................. INDEX .......................................................................................................... I GENERAL INFORMATION ...................................................................... 11 SPECIAL INSTRUCTIONS ........................................................................ m NASA STATIONS .................................................................................... m GOVERNMENT INTERDEPARTMENTAL CODES .•........................... IV ORGANIZATIONAL LISTINGS ................................................................ VI MSC BUILDING ADDRESSES ................................................................ XIV SITE LOCATIONS MAP ......................................................................... XV CONTRACTOR REPRESENTATIVES .................................................. 33 EMERGENCY NUMBERS FIRE (Houston Site) .............................................................. CA 7-2323 Ellington ...................................................................... HU 7-1400 ext 117 ACCIDENT ...................................................................................... 3781 AMBULANCE .......................................................................... CA 5-5534 ELLINGTON OPERATOR ............................................................. -
Matematikken Viser Vej Til Mars
S •Matematikken The viser vej til Mars Kim Plauborg © The Terma Group 2016 THE BEGINNING Terma has been in Space since man walked on the Moon! © The Terma Group 2016 FROM ESRO TO EXOMARS Terma powered the first comet landing ever! BREAKING NEWS The mission ends today when the Rosetta satellite will set down on the surface In 2014 the Rosetta satellite deployed the small lander Philae, which landed on the cometof 67P morethe than 10 comet years after Rosetta was launched. © The Terma Group 2016 FROM ESRO TO EXOMARS Rosetta Mars Express Technology Venus Express evolution and Galileo enhancement Small GEO BepiColombo ExoMars © The Terma Group 2016 Why go Mars? Getting to and landing on Mars is difficult ! © The Terma Group 2016 THE EXOMARS PROGRAMME Two ESA missions to Mars in cooperation with Roscosmos with the main objective to search for evidence of life 2016 Mission Trace Gas Orbiter Schiaparelli 2020 Mission Rover Surface platform © The Terma Group 2016 EXOMARS 2016 14th March 2016 Launched from Baikonur cosmodrome, Kazakhstan © The Terma Group 2016 EXOMARS 2016 16th October 2016 Separation of Schiaparelli from the orbiter © The Terma Group 2016 SCHIAPARELLI Schiaparelli (EDM) - an entry, descent and landing demonstrator module © The Terma Group 2016 EXOMARS 2016 19th October 2016 Landing of Schiaparelli the surface of Mars © The Terma Group 2016 EXOMARS 2016 19th October 2016 Landing of Schiaparelli the surface of Mars © The Terma Group 2016 EXOMARS 2020 © The Terma Group 2016 TERMA AND EXOMARS Terma deliveries to the ExoMars 2016 mission • Remote Terminal Power Unit for Schiaparelli • Mission Control System • Spacecraft Simulator • Support for the Launch and Early Orbit Phase © The Terma Group 2016 ExoMars RTPU The RTPU is a central unit in the Schiaparelli lander. -
Comet Interceptor: a Proposed ESA Mission to a Dynamically New Comet
EPSC Abstracts Vol. 13, EPSC-DPS2019-1679-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Comet Interceptor: A proposed ESA Mission to a Dynamically New Comet Geraint H. Jones(1,2), Colin Snodgrass(3), and The Comet Interceptor Consortium (see www.cometinterceptor.space ) (1) UCL Mullard Space Science Laboratory, Holmbury St. Mary, Dorking, RH5 6NT, UK ([email protected]) (2) The Centre for Planetary Sciences at UCL/Birkbeck, London, UK (3) University of Edinburgh, United Kingdom ([email protected]) Abstract allow valuable multi-point measurements of the solar wind over different lengtH-scales as tHese craft In response to the recent European Space Agency’s separate. call for proposals for a Fast (F) Mission, a multi- spacecraft project has been submitted to ESA to For the comet encounter, the primary spacecraft, encounter a dynamically new comet or interstellar planned to also act as the primary communication object. SucH an encounter with a comet approacHing point for the whole constellation, would be targetted the Sun for the first time would provide valuable data to pass outside the hazardous inner coma, on the to complement that from all previous comet missions, sunward side of tHe comet. At least one sub-spacecraft whicH Have by necessity studied sHort-period comets would be targetted for tHe nucleus/inner coma region. that Have evolved from their original condition during The various component spacecraft will carry a range their time orbiting near the Sun. of miniaturised instruments for remote and in situ studies of tHe object’s composition, nucleus, coma, The mission’s primary science goal is to cHaracterise, and plasma environment. -
Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020
Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020 Christopher Baker NASA Space Technology Mission Directorate Flight Opportunities and Small Spacecraft Technology Program Executive National Aeronautics and Space Administration 1 CHANGING THE PACE OF SPACE Through Small Spacecraft Technology and Flight Opportunities, Space Tech is pursuing the rapid identification, development, and testing of capabilities that exploit agile spacecraft platforms and responsive launch capabilities to increase the pace of space exploration, discovery, and the expansion of space commerce. National Aeronautics and Space Administration 2 THROUGH SUBORBITAL FLIGHT The Flight Opportunities program facilitates rapid demonstration of promising technologies for space exploration, discovery, and the expansion of space commerce through suborbital testing with industry flight providers LEARN MORE: WWW.NASA.GOV/TECHNOLOGY Photo Credit: Blue Origin National Aeronautics and Space Administration 3 FLIGHT OPPORTUNITIES BY THE NUMBERS Between 2011 and today… In 2019 alone… Supported 195 successful fights Supported 15 successful fights Enabled 676 tests of payloads Enabled 47 tests of payloads 254 technologies in the portfolio 86 technologies in the portfolio 13 active commercial providers 9 active commercial providers National Aeronautics and Space Administration Numbers current as of March 1, 2020 4 TECHNOLOGY TESTED IN SUBORBITAL Lunar Payloads ISS SPACE IS GOING TO EARTH ORBIT, THE MOON, MARS, AND BEYOND Mars 2020 Commercial Critical Space Lunar Payload Exploration Services Solutions National Aeronautics and Space Administration 5 SUBORBITAL INFUSION HIGHLIGHT Commercial Lunar Payload Services Four companies selected as Commercial Lunar Payload Services (CPLS) providers leveraged Flight Opportunities-supported suborbital flights to test technologies that are incorporated into their landers and/or are testing lunar landing technologies under Flight Opportunities for others. -
How a Cartoon Series Helped the Public Care About Rosetta and Philae 13 How a Cartoon Series Helped the Public Care About Rosetta and Philae
How a Cartoon Series Helped the Public Care about Best Practice Rosetta and Philae Claudia Mignone Anne-Mareike Homfeld Sebastian Marcu Vitrociset Belgium for European Space ATG Europe for European Space Design & Data GmbH Agency (ESA) Agency (ESA) [email protected] [email protected] [email protected] Carlo Palazzari Emily Baldwin Markus Bauer Design & Data GmbH EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) [email protected] [email protected] [email protected] Keywords Karen S. O’Flaherty Mark McCaughrean Outreach, space science, public engagement, EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) visual storytelling, fairy-tale, cartoon, animation, [email protected] [email protected] anthropomorphising Once upon a time... is a series of short cartoons1 that have been developed as part of the European Space Agency’s communication campaign to raise awareness about the Rosetta mission. The series features two anthropomorphic characters depicting the Rosetta orbiter and Philae lander, introducing the mission story, goals and milestones with a fairy- tale flair. This article explores the development of the cartoon series and the level of engagement it generated, as well as presenting various issues that were encountered using this approach. We also examine how different audiences responded to our decision to anthropomorphise the spacecraft. Introduction internet before the spacecraft came out of exciting highlights to come, using the fairy- hibernation (Bauer et al., 2016). The four tale narrative as a base. The hope was that In late 2013, the European Space Agency’s short videos were commissioned from the video would help to build a degree of (ESA) team of science communicators the cross-media company Design & Data human empathy between the public and devised a number of outreach activ- GmbH (D&D). -
Mars, the Nearest Habitable World – a Comprehensive Program for Future Mars Exploration
Mars, the Nearest Habitable World – A Comprehensive Program for Future Mars Exploration Report by the NASA Mars Architecture Strategy Working Group (MASWG) November 2020 Front Cover: Artist Concepts Top (Artist concepts, left to right): Early Mars1; Molecules in Space2; Astronaut and Rover on Mars1; Exo-Planet System1. Bottom: Pillinger Point, Endeavour Crater, as imaged by the Opportunity rover1. Credits: 1NASA; 2Discovery Magazine Citation: Mars Architecture Strategy Working Group (MASWG), Jakosky, B. M., et al. (2020). Mars, the Nearest Habitable World—A Comprehensive Program for Future Mars Exploration. MASWG Members • Bruce Jakosky, University of Colorado (chair) • Richard Zurek, Mars Program Office, JPL (co-chair) • Shane Byrne, University of Arizona • Wendy Calvin, University of Nevada, Reno • Shannon Curry, University of California, Berkeley • Bethany Ehlmann, California Institute of Technology • Jennifer Eigenbrode, NASA/Goddard Space Flight Center • Tori Hoehler, NASA/Ames Research Center • Briony Horgan, Purdue University • Scott Hubbard, Stanford University • Tom McCollom, University of Colorado • John Mustard, Brown University • Nathaniel Putzig, Planetary Science Institute • Michelle Rucker, NASA/JSC • Michael Wolff, Space Science Institute • Robin Wordsworth, Harvard University Ex Officio • Michael Meyer, NASA Headquarters ii Mars, the Nearest Habitable World October 2020 MASWG Table of Contents Mars, the Nearest Habitable World – A Comprehensive Program for Future Mars Exploration Table of Contents EXECUTIVE SUMMARY .......................................................................................................................... -
Virgin Galactic Launcherone Service Guide
LauncherOne Service Guide Version 0.2 his is this cover page) SERVICE GUIDE Virgin Galactic, LLC Version 0.2 25 March 2016 1 Cleared for Public Release by the DOD Office of Prepublication and Security Review LauncherOne Service Guide Version 0.2 Revolutionizing Space Access for Small Satellites If the key selling points of small satellites are that they are agile, flexible, and affordable, then these satellites need a launch service with the same qualities. Virgin Galactic has invested in the team, technologies, and facilities required to build just such a customer-focused launch service, LauncherOne. Air-launched from a 747-400 carrier aircraft, LauncherOne is the space access service that will accelerate the small satellite revolution. Overview LauncherOne is a simple, expendable, two stage launch vehicle designed to place small satellites (up to 500 kilograms) into a wide range of Low Earth Orbits (LEO) at an affordable price. LauncherOne System Expanded View 2 Cleared for Public Release by the DOD Office of Prepublication and Security Review LauncherOne Service Guide Version 0.2 Capabilities LauncherOne missions are highly customized to suit each customer’s specific requirements. Operating commercially through the FAA, LauncherOne operates independently of many of the external factors that can delay ground based launches: weather, offline radar tracking assets, boats in the launch pad stay out zone, and traffic jams on the increasingly crowded Eastern and Western ranges. Service Value Payload Payload Capability • Up to 300 kg / 661 lbm to 500 km / 270 nmi Sun Synchronous Orbit (SSO) • Up to 500 kg / 1100 lbm to 200 km / 108 nmi circular 28.5 degree inclination Low Earth Orbit (LEO) • Due to LauncherOne’s high degree of customization, payload capabilities are best calculated for each customer based on their specific requirements. -
Grey and Gold Grungy Classroom Newsletter
T H E M A R T I A N D E C E M B E R 2 0 1 9 THE MARTIAN M O N T H L Y N E W S L E T T E R MESSAGE FROM THE DIRECTOR Greetings! Back in May 2019, we founded the GD Goenka World School's Astronomy Club, with tremendous support from our Respected Director-Principal Ma'am Dr. Neeta Bali, DHM Ms. Shahnaz Banoo Butt, IBDP Coordinator Dr. Manisha Mehta, all the IB teachers, and the students. Today, all the members of the Astronomy Club proudly speak for all that they have learnt and explored, be it from the wonders of physical Astronomy, to the mysteries of black holes. We started with our very own Solar System - the Sun, Planets, Satellites, Comets, Asteroids and went on as far as the enormous El Gordo. Our classes include lectures, debates, quizzes, interactive games and RIP TO THIS videos, and brainstorming sessions. In the coming months, we aim to learn more about the mysteries of DYNAMIC DUO the universe. We bring to you the maiden edition of our Astronomy For seven years, NASA’s Van Allen Club's Monthly Newsletter, titled 'The Martian'. Probes have studied one of the nastiest We thank our club members Sumer Kaistha, Rehaan radiation environments known to Chibber, Aekum Kamboj, Jeevesh Raj Gupta, Naman humans: the Van Allen radiation belts. Akankshi, Omar Mir, and the Deputy Director Jusjeev They're an extremely important factor Singh for their effort into bringing this magazine to to plan for when it comes to satellite you. -
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. -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
Status of the Space Shuttle Solid Rocket Booster
The Space Congress® Proceedings 1980 (17th) A New Era In Technology Apr 1st, 8:00 AM Status of The Space Shuttle Solid Rocket Booster William P. Horton Solid Rocket Booster Engineering Office, George C. Marshall Space Flight Center, Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Horton, William P., "Status of The Space Shuttle Solid Rocket Booster" (1980). The Space Congress® Proceedings. 3. https://commons.erau.edu/space-congress-proceedings/proceedings-1980-17th/session-1/3 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. STATUS OF THE SPACE SHUTTLE SOLID ROCKET BOOSTER William P. Horton, Chief Engineer Solid Rocket Booster Engineering Office George C. Marshall Space Flight Center, AL 35812 ABSTRACT discuss retrieval and refurbishment plans for Booster reuse, and will address Booster status Two Solid Rocket Boosters provide the primary for multimission use. first stage thrust for the Space Shuttle. These Boosters, the largest and most powerful solid rocket vehicles to meet established man- BOOSTER CONFIGURATION rated design criteria, are unique in that they are also designed to be recovered, refurbished, It is appropriate to review the Booster config and reused. uration before describing the mission profile. The Booster is 150 feet long and is 148 inches The first SRB f s have been stacked on the in diameter (Figure 1), The inert weight Mobile Launch Platform at the Kennedy Space is 186,000 pounds and the propellant weight is Center and are ready to be mated with the approximately 1.1 million pounds for each External Tank and Orbiter in preparation for Booster. -
Arxiv:2005.12932V1 [Astro-Ph.EP] 26 May 2020 with Eccentricity, E = 1.2, ‘Oumuamua Encountered the Solar System with V∞ = 26 Km S
Draft version May 28, 2020 Typeset using LATEX default style in AASTeX63 Evidence that 1I/2017 U1 (`Oumuamua) was composed of molecular hydrogen ice. Darryl Seligman1 and Gregory Laughlin2 1 Dept. of the Geophysical Sciences, University of Chicago, Chicago, IL 60637 2Dept. of Astronomy, Yale University, New Haven, CT 06517 (Received April 14, 2020; Revised May 22, 2020; Accepted May 28, 2020) Submitted to ApJL ABSTRACT `Oumuamua (I1 2017) was the first macroscopic (l ∼ 100 m) body observed to traverse the inner solar system on an unbound hyperbolic orbit. Its light curve displayed strong periodic variation, and it showed no hint of a coma or emission from molecular outgassing. Astrometric measurements indicate that 'Oumuamua experienced non-gravitational acceleration on its outbound trajectory, but energy balance arguments indicate this acceleration is inconsistent with a water ice sublimation-driven jet of the type exhibited by solar system comets. We show that all of `Oumaumua's observed properties can be explained if it contained a significant fraction of molecular hydrogen (H2) ice. H2 sublimation at a rate proportional to the incident solar flux generates a surface-covering jet that reproduces the observed acceleration. Mass wasting from sublimation leads to monotonic increase in the body axis ratio, explaining `Oumuamua's shape. Back-tracing `Oumuamua's trajectory through the Solar System permits calculation of its mass and aspect ratio prior to encountering the Sun. We show that H2-rich bodies plausibly form in the coldest dense cores of Giant Molecular Clouds, where number densities are of order n ∼ 105, and temperatures approach the T = 3 K background.