Shuttle Launch and Landing Stats STS-132
Total Page：16
File Type：pdf, Size：1020Kb
Load more
Recommended publications
-
Rendezvous and Proximity Operations of the Space Shuttle Source of Acquisition John L
FROM :UNITED SfffCE RLL I FINE 281 212 6326 2005s 08-11 09: 34 #127 P. 05/21 Rendezvous and Proximity Operations of the Space Shuttle Source of Acquisition John L. Gooban' NASA JO~~SO~Space Center Uniied Space Albance, LLC, Hou.Wm. Texas: 77058 Spnce Shuttle rendmous missinns presented unique chalfengcs Clint were not fully recogni;ccd altea the Shutde WH~:deslgned. Rendezvous hrgcte could be passive (Le., no lights or Wnnrponders), and not designad 10 BcllIfate Shuttro rendezvous, praxlntlty operfirttlons and rclricval. Shuttls rendon control system ]ct plume lmplngetnent nn target spacccmfl prewnrcd Induced dynnmlcs, structoral loading and conhmlndon concerns. These Issues, along with fliiilfed forWard raction control system prupcllxnf drove II change from the GcmlniiApollo cuuillptlc profile heritage to a stnbte orbit proflle. and the development of new prorlmlly opcrntlons techniqucs. Multiple xckiitlfic and an-orbit servicing. tlssions; and crew exchanp, nsocmbly and rcplenlshment nigh& to Mir and io the InlernnBonnf Space S(Bfi0n dmve further pmfflc and pilnfing technique change%,lrcluding new rciative naviptlon senran gnd new ciwputcr generated piloting CPCS. Nomenclature the issucs with Shuffle rmdczvous md proximity operatiom had been f1.111~identified and resolved, which in N~Ircsultcd in complcx H Bar = unit vector along &e =get orbital angular illomcntum opmntionnl work-wounds. koposds for \chicle cepabiiitia vector competed for funding based on available budget, Bvaihbk schcduk, and criticality to Safety and mission success. Technical challenges in ix = LVLH +X axis vcctor $ = LTL~*Wrnk~CIOT ---b-uilding-~wsable~~~'~prt~.c~~-s~c~as propubion, &txid -tr- Lv&--i.Z-xiwe~oT---- _-- . protwtion. -
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. -
Protostar II Mission Overview
THE VEHICLE THE SATELLITE PROTON HISTORY PROTON DESCRIPTION Lead designer was Vladimir Chelomei, who designed it TOTAL HEIGHT with the intention of creating both a powerful rocket for 58.2 m (191 ft) military payloads and a high-performance ICBM. The program was changed, and the rocket was developed GRoss LIFT-OFF exclusively for launching spacecraft. WEIGHT 705,000 kg First named UR-500, but adopted the name (1,554,000 lb) “Proton,” which also was the name of the first PROPELLANT three payloads launched. UDMH and NTO Proton launched Russian interplanetary mis- INITIAL LAUNCH sions to the Moon, Venus, Mars, and Hal- 16 July 1965 ley’s Comet. Proton-1 Spacecraft Proton launched the Salyut space sta- PAYLOAD FAIRINGS tions, the Mir core segment and both There are multiple payload fairing designs presently the Zarya (Dawn) and Zvezda (Star) mod- qualified for flight, including ules for today’s International Space Station. standard commercial payload fairings developed specifically to First commercial Proton launch — 9 April 1996. meet the needs of our customers. First commercial Proton M Breeze M launch BREEZE M UPPER STAGE — 30 December 2002 The Breeze M is powered by one pump-fed Mission Overview gimbaled main engine that develops thrust of 20 kN (4,500 lbf). It is composed of a central core and an auxilliary propellant tank which is jettisoned in flight SATELLITE OPERATOR following depletion. The Breeze M control system includes an SES on-board computer, a three-axis gyro stabilized platform, and a www.ses.com navigation system. The quantity of propellant carried is dependent SATELLITE MANUFACTURER on specific mission requirements and is varied to maximize mission Experience ILS: Achieve Your Mission performance. -
The International Space Station and the Space Shuttle
Order Code RL33568 The International Space Station and the Space Shuttle Updated November 9, 2007 Carl E. Behrens Specialist in Energy Policy Resources, Science, and Industry Division The International Space Station and the Space Shuttle Summary The International Space Station (ISS) program began in 1993, with Russia joining the United States, Europe, Japan, and Canada. Crews have occupied ISS on a 4-6 month rotating basis since November 2000. The U.S. Space Shuttle, which first flew in April 1981, has been the major vehicle taking crews and cargo back and forth to ISS, but the shuttle system has encountered difficulties since the Columbia disaster in 2003. Russian Soyuz spacecraft are also used to take crews to and from ISS, and Russian Progress spacecraft deliver cargo, but cannot return anything to Earth, since they are not designed to survive reentry into the Earth’s atmosphere. A Soyuz is always attached to the station as a lifeboat in case of an emergency. President Bush, prompted in part by the Columbia tragedy, made a major space policy address on January 14, 2004, directing NASA to focus its activities on returning humans to the Moon and someday sending them to Mars. Included in this “Vision for Space Exploration” is a plan to retire the space shuttle in 2010. The President said the United States would fulfill its commitments to its space station partners, but the details of how to accomplish that without the shuttle were not announced. The shuttle Discovery was launched on July 4, 2006, and returned safely to Earth on July 17. -
1998 Year in Review
Associate Administrator for Commercial Space Transportation (AST) January 1999 COMMERCIAL SPACE TRANSPORTATION: 1998 YEAR IN REVIEW Cover Photo Credits (from left): International Launch Services (1998). Image is of the Atlas 2AS launch on June 18, 1998, from Cape Canaveral Air Station. It successfully orbited the Intelsat 805 communications satellite for Intelsat. Boeing Corporation (1998). Image is of the Delta 2 7920 launch on September 8, 1998, from Vandenberg Air Force Base. It successfully orbited five Iridium communications satellites for Iridium LLP. Lockheed Martin Corporation (1998). Image is of the Athena 2 awaiting its maiden launch on January 6, 1998, from Spaceport Florida. It successfully deployed the NASA Lunar Prospector. Orbital Sciences Corporation (1998). Image is of the Taurus 1 launch from Vandenberg Air Force Base on February 10, 1998. It successfully orbited the Geosat Follow-On 1 military remote sensing satellite for the Department of Defense, two Orbcomm satellites and the Celestis 2 funerary payload for Celestis Corporation. Orbital Sciences Corporation (1998). Image is of the Pegasus XL launch on December 5, 1998, from Vandenberg Air Force Base. It successfully orbited the Sub-millimeter Wave Astronomy Satellite for the Smithsonian Astrophysical Observatory. 1998 YEAR IN REVIEW INTRODUCTION INTRODUCTION In 1998, U.S. launch service providers conducted In addition, 1998 saw continuing demand for 22 launches licensed by the Federal Aviation launches to deploy the world’s first low Earth Administration (FAA), an increase of 29 percent orbit (LEO) communication systems. In 1998, over the 17 launches conducted in 1997. Of there were 17 commercial launches to LEO, 14 these 22, 17 were for commercial or international of which were for the Iridium, Globalstar, and customers, resulting in a 47 percent share of the Orbcomm LEO communications constellations. -
The Legal Ordering of Satellite Telecommunication: Problems and Alternatives
Indiana Law Journal Volume 44 Issue 3 Article 1 Spring 1969 The Legal Ordering of Satellite Telecommunication: Problems and Alternatives Delbert D. Smith University of Wisconsin Follow this and additional works at: https://www.repository.law.indiana.edu/ilj Part of the Air and Space Law Commons, and the Communications Law Commons Recommended Citation Smith, Delbert D. (1969) "The Legal Ordering of Satellite Telecommunication: Problems and Alternatives," Indiana Law Journal: Vol. 44 : Iss. 3 , Article 1. Available at: https://www.repository.law.indiana.edu/ilj/vol44/iss3/1 This Article is brought to you for free and open access by the Law School Journals at Digital Repository @ Maurer Law. It has been accepted for inclusion in Indiana Law Journal by an authorized editor of Digital Repository @ Maurer Law. For more information, please contact [email protected]. INDIANA LAW JOURNAL Volume 44 Spring 1969 Number 3 THE LEGAL ORDERING OF SATELLITE TELECOMMUNICATION: PROBLEMS AND ALTERNATIVES DELBERT D. SMITHt The use of satellites in outer space to provide a means of transmission for international telecommunication could be viewed as simply a tech- nological advancement neither necessitating basic structural changes in the international control institutions nor requiring alteration of the control theories designed to regulate unauthorized transmissions. How- ever, the magnitude of the changes involved, coupled with increased governmental concern, has resulted in a number of politico-legal problems. It is the purpose of this article to examine on several levels of analysis the implications of utilizing satellites as a means of telecom- munication transmission. Introductory material on the development of communications satellite technology stresses the need for international organization and co-operation to oversee the launching and maintenance of a global communications system and indicates the pressures for the implementation of control measures over transmissions originating in outer space. -
June, 2013 Mayumi Matsuura JAXA Flight Director Space Vehicle Technology Center Japan Aerospace Exploration Agency (JAXA) Congratulations on 50Th Anniversary
June, 2013 Mayumi Matsuura JAXA Flight Director Space Vehicle Technology Center Japan Aerospace Exploration Agency (JAXA) Congratulations on 50th Anniversary 1963.6.16 2008.3.11 The fist part of Japanese Experiment Module was launched International Space Station 1984： US President Ronald Reagan proposed developing a permanently-occupied space station 1988： Governments of Canada, ESA member countries, US and Japan signed the Intergovernmental Agreement on a cooperative framework for the space station 1993： Russia joined the program 1998： Beginning of on-orbit station assembly 2000： Beginning of continuous stay of the astronauts 2008: Beginning of assembly of Japanese Experiment Module 2011： Completion of station assembly Present： In the utilization phase International Partners ISS is truly an International space collaboration effort, with the participation of many countries. (C) NASA The First Piece of ISS ISS assembly sequence started in 1998 with the Russian module, Zarya (sunrise), launched by a Russian Proton rocket vehicle. Nov. 20, 1998 Zarya provides battery power, fuel storage and rendezvous and docking capability for Soyuz and Progress space vehicles. (C) NASA ISS Under Construction...(1998-2011) Dec. 2000 Dec. 1998 Dec. 1998 Dec. 2006 (C) NASA ISS Assembly Completion July 2011, Space shuttle Atlantis, on its final spaceflight of the Space Shuttle Program, carried the Raffaello multipurpose logistics module. 2011.7＠STS-135 (C) NASA Japanese Experimental Module (JEM) - Kibo Experiment Logistic Module - Pressurized Section (2008.Mar) ・ 8 racks can be installed Pressurized Module (2008. Jun) ・ Cargo storage area ・ The largest pressurized module on ISS ・ 10 payload racks can be installed ・ Various resources provided Remote Manipulator System (power, communication, thermal control, gas supply and exhaust) (2008. -
Orbital Debris: a Chronology
NASA/TP-1999-208856 January 1999 Orbital Debris: A Chronology David S. F. Portree Houston, Texas Joseph P. Loftus, Jr Lwldon B. Johnson Space Center Houston, Texas David S. F. Portree is a freelance writer working in Houston_ Texas Contents List of Figures ................................................................................................................ iv Preface ........................................................................................................................... v Acknowledgments ......................................................................................................... vii Acronyms and Abbreviations ........................................................................................ ix The Chronology ............................................................................................................. 1 1961 ......................................................................................................................... 4 1962 ......................................................................................................................... 5 963 ......................................................................................................................... 5 964 ......................................................................................................................... 6 965 ......................................................................................................................... 6 966 ........................................................................................................................ -
NASA Begins 5Th RS-25 Test Series
Volume 14 Issue 8 www.nasa.gov/centers/stennis August 2018 NASA begins 5th RS-25 test series NASA conducts a successful hot fire test of RS-25 developmental engine No. 0525 – featuring a new flight controller unit – on the A-1 Test Stand at Sten- nis Space Center on Aug. 14.The test was viewed by new NASA Administrator Jim Bridenstine and other guests. (See page 3 article) Page 2 LAGNIAPPE August 2018 It is estimated somewhere between 500 million to It was only fitting, then, that new NASA Administra- 600 million people around the world watched Neil tor Jim Bridenstine wasted little time in making his first Armstrong step onto the surface of the Moon in July visit to the site as agency leader. More fitting, he was 1969. It was the largest television audience at the time, able to view the Aug. 14 test and see firsthand the Sten- although they were not all in the same room. Ark! nis blended test team of NASA, Aerojet Rocketdyne and Syncom Space Services engineers and operators Probably nowhere near that many folk watched the at work. He also got a firsthand look at site facilities, NASA-TV and social media live broadcast of the RS- including the Aerojet Rocketdyne Engine Assembly 25 rocket engine test here Aug. 14 – but it is safe to say Facility, the E Test Complex and the B-2 Test Stand. an awful lot of attention is focused on Stennis Space Center these days. More importantly, the new NASA leader was able to visit with center and resident agency leaders, local Stennis is at the forefront of NASA’s work to build and media members, community representatives and site launch its new Space Launch System (SLS) rocket that employees. -
The Delta Launch Vehicle- Past, Present, and Future
The Space Congress® Proceedings 1981 (18th) The Year of the Shuttle Apr 1st, 8:00 AM The Delta Launch Vehicle- Past, Present, and Future J. K. Ganoung Manager Spacecraft Integration, McDonnell Douglas Astronautics Co. H. Eaton Delta Launch Program, McDonnell Douglas Astronautics Co. Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ganoung, J. K. and Eaton, H., "The Delta Launch Vehicle- Past, Present, and Future" (1981). The Space Congress® Proceedings. 7. https://commons.erau.edu/space-congress-proceedings/proceedings-1981-18th/session-6/7 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]. THE DELTA LAUNCH VEHICLE - PAST, PRESENT AND FUTURE J. K. Ganoung, Manager H. Eaton, Jr., Director Spacecraft Integration Delta Launch Program McDonnell Douglas Astronautics Co. McDonnell Douglas Astronautics Co. INTRODUCTION an "interim space launch vehicle." The THOR was to be modified for use as the first stage, the The Delta launch vehicle is a medium class Vanguard second stage propulsion system, was used expendable booster managed by the NASA Goddard as the Delta second stage and the Vanguard solid Space Flight Center and used by the U.S. rocket motor became Delta's third stage. Government, private industry and foreign coun Following the eighteen month development program tries to launch scientific, meteorological, and failure to launch its first payload into or applications and communications satellites. -
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. -
+ 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.................................................................................