MASAD-83-6 Issues Concerning the Future Operation of the Space
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Space Reporter's Handbook Mission Supplement
CBS News Space Reporter's Handbook - Mission Supplement Page 1 The CBS News Space Reporter's Handbook Mission Supplement Shuttle Mission STS-125: Hubble Space Telescope Servicing Mission 4 Written and Produced By William G. Harwood CBS News Space Analyst [email protected] CBS News 5/10/09 Page 2 CBS News Space Reporter's Handbook - Mission Supplement Revision History Editor's Note Mission-specific sections of the Space Reporter's Handbook are posted as flight data becomes available. Readers should check the CBS News "Space Place" web site in the weeks before a launch to download the latest edition: http://www.cbsnews.com/network/news/space/current.html DATE RELEASE NOTES 08/03/08 Initial STS-125 release 04/11/09 Updating to reflect may 12 launch; revised flight plan 04/15/09 Adding EVA breakdown; walkthrough 04/23/09 Updating for 5/11 launch target date 04/30/09 Adding STS-400 details from FRR briefing 05/04/09 Adding trajectory data; abort boundaries; STS-400 launch windows Introduction This document is an outgrowth of my original UPI Space Reporter's Handbook, prepared prior to STS-26 for United Press International and updated for several flights thereafter due to popular demand. The current version is prepared for CBS News. As with the original, the goal here is to provide useful information on U.S. and Russian space flights so reporters and producers will not be forced to rely on government or industry public affairs officers at times when it might be difficult to get timely responses. All of these data are available elsewhere, of course, but not necessarily in one place. -
Out There Somewhere Could Be a PLANET LIKE OURS the Breakthroughs We’Ll Need to find Earth 2.0 Page 30
September 2014 Out there somewhere could be A PLANET LIKE OURS The breakthroughs we’ll need to find Earth 2.0 Page 30 Faster comms with lasers/16 Real fallout from Ukraine crisis/36 NASA Glenn chief talks tech/18 A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS Engineering the future Advanced Composites Research The Wizarding World of Harry Potter TM Bloodhound Supersonic Car Whether it’s the world’s fastest car With over 17,500 staff worldwide, and 2,800 in or the next generation of composite North America, we have the breadth and depth of capability to respond to the world’s most materials, Atkins is at the forefront of challenging engineering projects. engineering innovation. www.na.atkinsglobal.com September 2014 Page 30 DEPARTMENTS EDITOR’S NOTEBOOK 2 New strategy, new era LETTER TO THE EDITOR 3 Skeptical about the SABRE engine INTERNATIONAL BEAT 4 Now trending: passive radars IN BRIEF 8 A question mark in doomsday comms Page 12 THE VIEW FROM HERE 12 Surviving a bad day ENGINEERING NOTEBOOK 16 Demonstrating laser comms CONVERSATION 18 Optimist-in-chief TECH HISTORY 22 Reflecting on radars PROPULSION & ENERGY 2014 FORUM 26 Electric planes; additive manufacturing; best quotes Page 38 SPACE 2014 FORUM 28 Comet encounter; MILSATCOM; best quotes OUT OF THE PAST 44 CAREER OPPORTUNITIES 46 Page 16 FEATURES FINDING EARTH 2.0 30 Beaming home a photo of a planet like ours will require money, some luck and a giant telescope rich with technical advances. by Erik Schechter COLLATERAL DAMAGE 36 Page 22 The impact of the Russia-Ukrainian conflict extends beyond the here and now. -
Year in Review 2013
SM_Dec_2013 cover Worldwide Satellite Magazine December 2013 SatMagazine 2013 YEAR IN REVIEW SatMagazine December 2013—Year In Review Publishing Operations Senior Contributors This Issue’s Authors Silvano Payne, Publisher + Writer Mike Antonovich, ATEME Mike Antonovich Robert Kubbernus Hartley G. Lesser, Editorial Director Tony Bardo, Hughes Eran Avni Dr. Ajey Lele Richard Dutchik Dave Bettinger Tom Leech Pattie Waldt, Executive Editor Chris Forrester, Broadgate Publications Don Buchman Hartley Lesser Jill Durfee, Sales Director, Editorial Assistant Karl Fuchs, iDirect Government Services Eyal Copitt Timothy Logue Simon Payne, Development Director Bob Gough, 21 Carrick Communications Rich Currier Jay Monroe Jos Heyman, TIROS Space Information Tommy Konkol Dybvad Tore Morten Olsen Donald McGee, Production Manager David Leichner, Gilat Satellite Networks Chris Forrester Kurt Peterhans Dan Makinster, Technical Advisor Giles Peeters, Track24 Defence Sima Fishman Jorge Potti Bert Sadtler, Boxwood Executive Search Simen K. Frostad Sally-Anne Ray David Gelerman Susan Sadaat Samer Halawi Bert Sadtler Jos Heyman Patrick Shay Jack Jacobs Mike Towner Casper Jensen Serge Van Herck Alexandre Joint Pattie Waldt Pradman Kaul Ali Zarkesh Published 11 times a year by SatNews Publishers 800 Siesta Way Sonoma, CA 95476 USA Phone: (707) 939-9306 Fax: (707) 838-9235 © 2013 SatNews Publishers We reserve the right to edit all submitted materials to meet our content guidelines, as well as for grammar or to move articles to an alternative issue to accommodate publication space requirements, or removed due to space restrictions. Submission of content does not constitute acceptance of said material by SatNews Publishers. Edited materials may, or may not, be returned to author and/or company for review prior to publication. -
Orbiter Processing Facility
National Aeronautics and Space Administration Space Shuttle: Orbiter Processing From Landing To Launch he work of preparing a space shuttle for the same facilities. Inside is a description of an flight takes place primarily at the Launch orbiter processing flow; in this case, Discovery. Complex 39 Area. TThe process actually begins at the end of each acts Shuttle Landing Facility flight, with a landing at the center or, after landing At the end of its mission, the Space Shuttle f at an alternate site, the return of the orbiter atop a Discovery lands at the Shuttle Landing Facility on shuttle carrier aircraft. Kennedy’s Shuttle Landing one of two runway headings – Runway 15 extends Facility is the primary landing site. from the northwest to the southeast, and Runway There are now three orbiters in the shuttle 33 extends from the southeast to the northwest fleet: Discovery, Atlantis and Endeavour. Chal- – based on wind currents. lenger was destroyed in an accident in January After touchdown and wheelstop, the orbiter 1986. Columbia was lost during approach to land- convoy is deployed to the runway. The convoy ing in February 2003. consists of about 25 specially designed vehicles or Each orbiter is processed independently using units and a team of about 150 trained personnel, NASA some of whom assist the crew in disembarking from the orbiter. the orbiter and a “white room” is mated to the orbiter hatch. The The others quickly begin the processes necessary to “safe” the hatch is opened and a physician performs a brief preliminary orbiter and prepare it for towing to the Orbiter Processing Fa- medical examination of the crew members before they leave the cility. -
Launch Vehicle Control Center Architectures
Launch Vehicle Control Center Architectures Michael D. Watson1, Amy Epps2, and Van Woodruff3 NASA Marshall Space Flight Center, Huntsville, AL 35812 Michael Jacob Vachon4 NASA Johnson Space Center, Houston, TX 77058 Julio Monreal5 European Space Agency, Launchers Directorate, Paris, France Marl Levesque6 United Launch Alliance, Vandenberg AFB and Randall Williams7 and Tom McLaughlin8 Aerospace Corporation, El Segundo, CA 90245 Launch vehicles within the international community vary greatly in their configuration and processing. Each launch site has a unique processing flow based on the specific launch vehicle configuration. Launch and flight operations are managed through a set of control centers associated with each launch site. Each launch site has a control center for launch operations; however flight operations support varies from being co-located with the launch site to being shared with the space vehicle control center. There is also a nuance of some having an engineering support center which may be co-located with either the launch or flight control center, or in a separate geographical location altogether. A survey of control center architectures is presented for various launch vehicles including the NASA Space Launch System (SLS), United Launch Alliance (ULA) Atlas V and Delta IV, and the European Space Agency (ESA) Ariane 5. Each of these control center architectures shares some similarities in basic structure while differences in functional distribution also exist. The driving functions which lead to these factors are considered and a model of control center architectures is proposed which supports these commonalities and variations. I. INTRODUCTION Launch vehicles in both Europe and the United States have been operating successfully for several decades. -
Building KSC's Launch Complex 39
National Aeronautics and Space Administration Building KSC’s Launch Complex 39 n the beginning, there was sand and adjacent to the VAB would house the Apollo I palmettos and water. Yet out of this idyllic spacecraft and the Launch Control Center. setting would grow the most unique structures -- The launcher-transporter would incorporate engineering milestones -- that would set the stage three major facilities: a pedestal for the space for the future in space. vehicle, an umbilical tower to service the upper The Kennedy Space Center of the 21st reaches of the space vehicle, and a rail transport- century began life in the early 1960s when new er. An arming tower would stand about midway Facts facilities were needed to launch the moon-bound between the assembly building and the pads. Saturn V rockets. The Apollo Saturn would carry a number of Initial plans called for a launch complex hazardous explosives: the launch escape system comprising a Vertical Assembly Building (VAB), (the tower on top of the vehicle that lifted the a launcher-transporter, an arming area and a spacecraft away from the launch vehicle in case launch pad. The VAB would consist of assembly of an emergency), retrorockets to separate the bay areas for each of the stages, with a high-bay stages, ullage rockets to force fuel to the bottom unit approximately 110 meters in height for final of tanks, and the launch vehicle’s destruct system. assembly and checkout of the vehicle. Buildings These plans would be modified during NASA NASA Launch Pad 39A is under construction (foreground) with the imposing Vertical Assembly Building rising from the sand in the background. -
Microgravity and Macromolecular Crystallography Craig E
CRYSTAL GROWTH & DESIGN 2001 VOL. 1, NO. 1 87-99 Review Microgravity and Macromolecular Crystallography Craig E. Kundrot,* Russell A. Judge, Marc L. Pusey, and Edward H. Snell Mail Code SD48 Biotechnology Science Group, NASA Marshall Space Flight Center, Huntsville, Alabama 35812 Received August 24, 2000 ABSTRACT: Macromolecular crystal growth is seen as an ideal experiment to make use of the reduced acceleration environment provided by an orbiting spacecraft. The experiments are small, are simply operated, and have a high potential scientific and economic impact. In this review we examine the theoretical reasons why microgravity is a beneficial environment for crystal growth and survey the history of experiments on the Space Shuttle Orbiter, on unmanned spacecraft, and on the Mir space station. The results of microgravity crystal growth are considerable when one realizes that the comparisons are always between few microgravity-based experiments and a large number of earth-based experiments. Finally, we outline the direction for optimizing the future use of orbiting platforms. 1. Introduction molecules, including viruses, proteins, DNA, RNA, and complexes of those molecules. In this review, the terms Macromolecular crystallography is a multidisciplinary protein or macromolecule are used to refer to this entire science involving the crystallization of a macromolecule range. or complex of macromolecules, followed by X-ray or The reduced acceleration environment of an orbiting neutron diffraction to determine the three-dimensional spacecraft has been posited as an ideal environment for structure. The structure provides a basis for under- biological crystal growth, since buoyancy-driven convec- standing function and enables the development of new tion and sedimentation are greatly reduced. -
Japan's Technical Prowess International Cooperation
Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Japan’s Technical Prowess Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness. -
+ STS-123 Press
CONTENTS Section Page STS-123 MISSION OVERVIEW................................................................................................ 1 TIMELINE OVERVIEW.............................................................................................................. 11 MISSION PROFILE................................................................................................................... 15 MISSION PRIORITIES............................................................................................................. 17 MISSION PERSONNEL............................................................................................................. 19 STS-123 ENDEAVOUR CREW .................................................................................................. 21 PAYLOAD OVERVIEW .............................................................................................................. 31 KIBO OVERVIEW.................................................................................................................................. 31 KIBO MISSION CONTROL CENTER ....................................................................................................... 39 TSUKUBA SPACE CENTER.................................................................................................................... 43 SPACE STATION INTEGRATION AND PROMOTION CENTER .................................................................. 47 JAXA’S EXPERIMENTS DURING THE 1J/A STAGE................................................................................. -
+ STS-115 Press
STS-121 Press Kit CONTENTS Section Page STS-115 MISSION OVERVIEW: SPACE STATION ASSEMBLY RESUMES................................ 1 STS-115 TIMELINE OVERVIEW ............................................................................................... 10 MISSION PRIORITIES............................................................................................................. 12 LAUNCH AND LANDING ........................................................................................................... 14 LAUNCH............................................................................................................................................... 14 ABORT-TO-ORBIT (ATO)...................................................................................................................... 14 TRANSATLANTIC ABORT LANDING (TAL)............................................................................................. 14 RETURN-TO-LAUNCH-SITE (RTLS)....................................................................................................... 14 ABORT ONCE AROUND (AOA)............................................................................................................... 14 LANDING ............................................................................................................................................. 14 MISSION PROFILE................................................................................................................... 15 STS-115 ATLANTIS CREW ..................................................................................................... -
Spacewalk Database
Purchaser First Inscribed First ID Name Purchaser Last Name Name Inscribed Last Name Biographic_Infomation 01558 Beth / Forrest Goodwin Ron & Margo Borrup In 1957 CURTISS S. (ARMY) ARMSTRONG became a member of America's Space Team. His career began with the launch of Explorer I and Apollo programs. His tireless dedication has contributed to America's future. He is truly 00022 Cheryl Ann Armstrong Curtiss S. Armstrong an American Space Pioneer. Science teacher and aerospace educator since 00023 Thomas J. Sarko Thomas J. Sarko 1975. McDonnell Douglas 25 Years, AMF Board of 00024 Lowell Grissom Lowell Grissom Directors Joined KSC in 1962 in the Director's Protocol Office. Responsible for the meticulous details for the arrival, lodging, and banquets for Kings, Queens and other VIP worldwide and their comprehensive tours of KSC with top KSC 00025 Major Jay M. Viehman Jay Merle Viehman Personnel briefing at each poi WWII US Army Air Force 1st Lt. 1943-1946. US Civil Service 1946-1972 Engineer. US Army Ballistic Missile Launch Operations. Redstone, Jupiter, Pershing. 1st Satellite (US), Mercury 1st Flight Saturn, Lunar Landing. Retired 1972 from 00026 Robert F. Heiser Robert F. Heiser NASA John F. Kennedy S Involved in Air Force, NASA, National and Commercial Space Programs since 1959. Commander Air Force Space Division 1983 to 1986. Director Kennedy Space Center - 1986 to 1 Jan 1992. Vice President, Lockheed Martin 00027 Gen. Forrest S. McCartney Forrest S. McCartney Launch Operations. Involved in the operations of the first 41 manned missions. Twenty years with NASA. Ten years 00028 Paul C. Donnelly Paul C. -
Space Shuttle Abort Evolution Edward M
AIAA SPACE 2011 Conference & Exposition AIAA 2011-1072113 26 - 29 Sep 2011, Long Beach, California Space Shuttle Abort Evolution Edward M. Henderson 1 and Tri X. Nguyen2 NASA, Johnson Space Center, Houston, Texas 77058 Abstract This paper documents some of the evolutionary steps in developing a rigorous Space Shuttle launch abort capability. The paper addresses the abort strategy during the design and development and how it evolved during Shuttle flight operations. The Space Shuttle Program made numerous adjustments in both the flight hardware and software as the knowledge of the actual flight environment grew. When failures occurred, corrections and improvements were made to avoid a reoccurrence and to provide added capability for crew survival. Finally some lessons learned are summarized for future human launch vehicle designers to consider. Nomenclature AOA = Abort Once Around ATO = Abort to Orbit ET = External Tank FSW = Flight software ISS = International Space Station MECO = Main Engine cutoff OFT = Orbiter Flight Test Program OMS = Orbiter Maneuvering System RCS = Reaction Control System RTLS = Return to the Landing Site SOFT = Suborbital Flight Test Flight SSME = Space Shuttle Main Engine TAL = Transoceanic Abort Landing TPS = Thermal Protection System TVC = Thrust vector control WTR = Western Test Range I. Introduction he Space Shuttle was intended to be a reusable launch vehicle. However the national budget could not support T that large of an initial investment required for the design and development of a fully recoverable and reusable vehicle. Therefore a compromise design (Fig. 1.) was selected with an expendable external propellant tank that lowered development cost and corresponding increase in the operations cost.