89 Part 1214—Space Flight
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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. -
H M 7 P a G E 1 a MEMORIAL HONORING the MEMORY OF
H A MEMORIAL M HONORING THE MEMORY OF THE SEVEN ASTRONAUTS WHO SERVED ON THE 7 P SPACE SHUTTLE COLUMBIA. a g e WHEREAS, the members of this chamber are grief-stricken at the loss of the 1 space shuttle Columbia and her seven astronauts on Saturday, February 1, 2003; and WHEREAS, the women and men who perished aboard Columbia embodied the very best qualities of mankind. Their intelligence, diligence and valor led to their selection for the space program and their presence on Columbia; and WHEREAS, today we pause not only to remember this tragedy, but we also pause to honor the achievements of seven exemplary people; and WHEREAS, let us recite the names of the seven astronauts: Rick D. Husband, age forty-five and the commander of Columbia. Commander Husband was a colonel in the United States air force. He was selected as an astronaut in 1994 and prior to this mission had logged two hundred thirty hours in space. His home was Amarillo, Texas; William C. McCool, age forty-one and the pilot for the mission. He was a commander in the United States navy and a former test pilot. Commander McCool became an astronaut in 1996, and this was his first space flight. His home was Lubbock, Texas; Michael P. Anderson, age forty-three and the payload commander for Columbia. Lieutenant Colonel Anderson was an air force man who grew up as the son of an air force man. Selected as an astronaut in 1994, he had previously logged over two hundred eleven hours in space. -
Payload Specialist Astronaut Bio: Taylor G. Wang
National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, Texas 77058 Biographical Data TAYLOR G. WANG PAYLOAD SPECIALIST PERSONAL DATA: Born June 16, 1940, in Mainland China. He is a Physicist at the Jet Propulsion Laboratory in California, and is a U.S. citizen. He is married, and has two sons. EDUCATION: Received a bachelor of science degree in physics in 1967, a master of science degree in physics in 1968, and a doctorate in physics in 1971, from the University of California at Los Angeles. ORGANIZATIONS: Member, American Physical Society, Materials Research Society, American Institute of Aeronautics and Astronautics, Sigma Xi, and a Fellow in the Acoustical Society of America. EXPERIENCE: After completing his doctorate, Dr. Wang joined the California Institute of Technology Jet propulsion Laboratory (JPL) in 1972, as a senior scientist. He is currently Program Manager for Materials Processing in Space. At JPL he was responsible for the inception and development of containerless processing science and technology research. He is the Principal Investigator (PI) on the Spacelab 3 mission NASA Drop Dynamics (DDM) experiments, PI on the NASA SPAR Flight Experiment #77-18 "Dynamics of Liquid Bubble," PI on the NASA SPAR Flight Experiment #76- 20 "Containerless Processing Technology," and PI on the Department of Energy Experiment "Spherical Shell Technology." Dr. Wang has been conducting precursor drop dynamics experiments for the DDM in ground-based laboratories employing acoustic levitation systems, neutral buoyancy systems and drop towers, and in the near weightless environment provided by JSC's KC-135 airplane flights and SPAR rockets. These flights have helped to define the experimental parameters and procedures in the DDM experiments to be performed on Spacelab 3. -
Cubesat Mission: from Design to Operation
applied sciences Article CubeSat Mission: From Design to Operation Cristóbal Nieto-Peroy 1 and M. Reza Emami 1,2,* 1 Onboard Space Systems Group, Department of Computer Science, Electrical and Space Engineering, Luleå University of Technology, Space Campus, 981 92 Kiruna, Sweden 2 Aerospace Mechatronics Group, University of Toronto Institute for Aerospace Studies, Toronto, ON M3H 5T6, Canada * Correspondence: [email protected]; Tel.: +1-416-946-3357 Received: 30 June 2019; Accepted: 29 July 2019; Published: 1 August 2019 Featured Application: Design, fabrication, testing, launch and operation of a particular CubeSat are detailed, as a reference for prospective developers of CubeSat missions. Abstract: The current success rate of CubeSat missions, particularly for first-time developers, may discourage non-profit organizations to start new projects. CubeSat development teams may not be able to dedicate the resources that are necessary to maintain Quality Assurance as it is performed for the reliable conventional satellite projects. This paper discusses the structured life-cycle of a CubeSat project, using as a reference the authors’ recent experience of developing and operating a 2U CubeSat, called qbee50-LTU-OC, as part of the QB50 mission. This paper also provides a critique of some of the current poor practices and methodologies while carrying out CubeSat projects. Keywords: CubeSat; miniaturized satellite; nanosatellite; small satellite development 1. Introduction There have been nearly 1000 CubeSats launched to the orbit since the inception of the concept in 2000 [1]. An up-to-date statistics of CubeSat missions can be found in Reference [2]. A summary of CubeSat missions up to 2016 can also be found in Reference [3]. -
Sts-45 Press Kit March 1992
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION SPACE SHUTTLE MISSION STS-45 PRESS KIT MARCH 1992 ATLAS-1 MISSION Edited by Richard W. Orloff, 01/2000/Page 1 STS-45 INSIGNIA STS045-S-001 -- Designed by the crewmembers, the STS-45 insignia depicts the space shuttle launching from the Kennedy Space Center into a high inclination orbit. From this vantage point, the Atmospheric Laboratory for Applications and Science (ATLAS) payload can view the Earth, the sun, and their dynamic interactions against the background of space. Earth is prominently displayed and is the focus of the mission's space plasma physics and Earth sciences observations. The colors of the setting sun, measured by sensitive instruments, provide detailed information about ozone, carbon dioxide, and other gases which determined Earth's climate and environment. Encircling the scene are the names of the flight crew members. The additional star in the ring is to recognize Charles R. Chappell and Michael Lampton, alternate payload specialists, and the entire ATLAS-1 team for its dedication and support of this "Mission to Planet Earth." The NASA insignia design for space shuttle flights is reserved for use by the astronauts and for other official use as the NASA Administrator may authorize. Public availability has been approved only in the form of illustrations by the various news media. When and if there is any change in this policy, which we do not anticipate, it will be publicly announced. PHOTO CREDIT: NASA or National Aeronautics and Space Administration. Edited by Richard -
First of a New Generation by Philip Corneille
Subject Spaceflight Vol 44 April 2002 Belgian Dirk Frimout considers tenth anniversary of his Shuttle flight First of a new generation By Philip Corneille When Belgiums second astronaut Frank de Winne blasts into space this autumn on a mission to the International Space Station it will be more than a decade since the flight of his fellow country-man Dirk Frimout. Unlike Frimout, who was a member of the STS-45 Space Shuttle crew, de Winne will ride into space on a Russian Soyuz TM craft. He is currently in training at Star City, Moscow. Frimout recalls that one of his best memories of the flight in March 1992 was the feeling just eight minutes after launch when the engines fell silent and microgravity became a reality. Born in Poperinge, Belgium, in 1941, Frimouts generation was the first to be able to study and work in space flight technology. Sputnik 1 flew in space on my sixteenth birthday and I decided to orientate my university studies towards engineering and technology, he said. He received a degree in electro-technical engineering and a doctorate in applied physics at the State University of Ghent, performing a post- doctorate at the University of Colorado, Laboratory of Atmospheric and Space Physics in 1972. At this time he also started to work with BIRA (Belgisch Instituut Ruimte Aeronomie) on atmospheric experiments carried by balloons and sounding rockets. Frimout was senior engineer in the Payload Utilisation Department of the European Space Agency (ESA) and was responsible for European experiments for the Atlas-1 mission since 1985. -
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................................................................................. -
Social, Cultural, and Educational Legacies
NASA Reflects America’s Changing Opportunities; Social, NASA Impacts US Culture Education: Inspiring Cultural, and Students as Only NASA Can Educational Legacies Social, Cultural, and Educational Legacies 459 NASA Reflects The Space Shuttle, which began flying in 1981 and ushered in an entirely new human spaceflight program, was a watershed for cultural diversity America’s within NASA and had substantial cultural impact outside the realm of Changing spaceflight. In the 1950s and 1960s, opportunities for American women and minorities were limited as they were often segregated into pink Opportunities; collar and menial jobs. NASA’s female and minority employees faced NASA Impacts similar obstacles. The Space Shuttle Program opened up opportunities US Culture for these groups—opportunities that did not exist during Projects Mercury and Gemini or the Apollo and Skylab Programs. NASA’s transformation was a direct consequence of a convergence of events Jennifer Ross-Nazzal Shannon Lucid that happened in the 1960s and 1970s and continued through the Helen Lane following 3 decades. These included: public policy changes instituted on the national level; the development of a spacecraft whose physical capabilities departed radically from the capsule concept; and an increase in the number of women and minorities holding degrees in the fields of science and engineering, making them attractive candidates for the space agency’s workforce. Over the course of the program, the agency’s demographics reflected this transformation: women and minorities were incorporated into the Astronaut Corps and other prominent technical and administrative positions. The impact of NASA’s longest-running program extends beyond these dramatic changes. -
Increasing Launch Rate and Payload Capabilities
Aerial Launch Vehicles: Increasing Launch Rate and Payload Capabilities Yves Tscheuschner1 and Alec B. Devereaux2 University of Colorado, Boulder, Colorado Two of man's greatest achievements have been the first flight at Kitty Hawk and pushing into the final frontier that is space. Air launch systems aim to combine these great achievements into a revolutionary way to deliver satellites, cargo and eventually people into space. Launching from an aircraft has many advantages, including the ability to launch at any inclination and from above bad weather, which could delay ground launches. While many concepts for launching rockets from an airplane have been developed, very few have made it past the drawing board. Only the Pegasus and, to a lesser extent, SpaceShipOne have truly shown the feasibility of such a system. However, a recent push for rapid, small payload to orbit launches by the military and a general need for cheaper, heavy lift options are leading to an increasing interest in air launch methods. In order for the efficiency and flexibility of the system to be realized, however, additional funding and research are necessary. Nomenclature ALASA = airborne launch assist space access ALS = air launch system DARPA = defense advanced research project agency LEO = low Earth orbit LOX = liquid oxygen RP-1 = rocket propellant 1 MAKS = Russian air launch system MECO = main engine cutoff SS1 = space ship one SS2 = space ship two I. Introduction W hat typically comes to mind when considering launching people or satellites to space are the towering rocket poised on the launch pad. These images are engraved in the minds of both the public and scientists alike. -
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. -
Paper Session II-B-National Launch System Payload Accommodations
The Space Congress® Proceedings 1992 (29th) Space - Quest For New Fontiers Apr 22nd, 2:00 PM Paper Session II-B - National Launch System Payload Accommodations Capt James M. Knauf National Launch System Requirements Officer HQ Airor F ce Space Command Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Knauf, Capt James M., "Paper Session II-B - National Launch System Payload Accommodations" (1992). The Space Congress® Proceedings. 15. https://commons.erau.edu/space-congress-proceedings/proceedings-1992-29th/april-22-1992/15 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]. NATIONAL LAUNCH SYSTEM PAYLOAD ACCOMMODATIONS Capt James M. Knauf National Launch System Requirements Officer HQ Air Force Space Command - Peterson AFB, CO ABSTRACT Early definition, documentation, acceptance, and continuing implementation of a standard system of payload accommodations for space launch systems is essential. Attempts to provide truly standard payload accommodations have not met with significant success in increasing responsiveness or reducing operations costs. The operational philosophy of the National Launch System (NLS) is based on standardization and includes standardized payload accommodations. These must be incorporated into NLS design concepts early in the development phase to ensure the NLS goal of increased responsiveness and reduced operating cost. At the same time, sufficient flexibility will be maintained to accommodate the rare unique payload requirement which cannot meet the standard due to specific mission requirements, safety concerns, or other reasons.