The International Space Station and the Space Shuttle
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Mission Operations Directorate - Success Legacy of the Space Shuttle Program
https://ntrs.nasa.gov/search.jsp?R=20100030556 2019-08-30T11:10:21+00:00Z View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by NASA Technical Reports Server Mission Operations Directorate - Success Legacy of the Space Shuttle Program Jim Azbell Deputy Division Chief, Space Transportation Vehicle Division, Mission Operations Directorate NASA Lyndon B. Johnson Space Center, Houston, Texas 77058 In support of the Space Shuttle Program, as well as NASA’s other human space flight programs, the Mission Operations Directorate (MOD) at the Johnson Space Center has become the world leader in human spaceflight operations. From the earliest programs - Mercury, Gemini, Apollo - through Skylab, Shuttle, ISS, and our Exploration initiatives, MOD and its predecessors have pioneered ops concepts and emphasized a history of mission leadership which has added value, maximized mission success, and built on continual improvement of the capabilities to become more efficient and effective. MOD’s focus on building and contributing value with diverse teams has been key to their successes both with the US space industry and the broader international community. Since their beginning, MOD has consistently demonstrated their ability to evolve and respond to an ever changing environment, effectively prepare for the expected and successfully respond to the unexpected, and develop leaders, expertise, and a culture that has led to mission and Program success. MOD Background To better understand the evolution and successes of MOD during the Shuttle program, one must first understand the MOD’s current roles and responsibilities. MOD’s responsibilities traditionally fall into four categories: flight design and planning, crew and flight controller training, real-time flight execution, and facility operations. -
Contingency Shuttle Crew Support (Cscs)/Rescue Flight Resource Book
CSCS/Rescue Flight Resource Book JSC-62900 CONTINGENCY SHUTTLE CREW SUPPORT (CSCS)/RESCUE FLIGHT RESOURCE BOOK OVERVIEW 1 Mission Operations CSCS 2 Directorate RESCUE 3 FLIGHT DA8/Flight Director Office Final July 12, 2005 National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, Texas FINAL 07/12/05 2-i Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 CONTINGENCY SHUTTLE CREW SUPPORT (CSCS)/RESCUE FLIGHT RESOURCE BOOK FINAL JULY 12, 2005 PREFACE This document, dated May 24, 2005, is the Basic version of the Contingency Shuttle Crew Support (CSCS)/Rescue Flight Resource Book. It is requested that any organization having comments, questions, or suggestions concerning this document should contact DA8/Book Manager, Flight Director Office, Building 4 North, Room 3039. This is a limited distribution and controlled document and is not to be reproduced without the written approval of the Chief, Flight Director Office, mail code DA8, Lyndon B. Johnson Space Center, Houston, TX 77058. FINAL 07/12/05 2-ii Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 1.0 - OVERVIEW Section 1.0 is the overview of the entire Contingency Shuttle Crew Support (CSCS)/Rescue Flight Resource Book. FINAL 07/12/05 2-iii Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 This page intentionally blank. FINAL 07/12/05 2-iv Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 2.0 - CONTINGENCY SHUTTLE CREW SUPPORT (CSCS) 2.1 Procedures Overview.......................................................................................................2-1 2.1.1 ................................................................................ -
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. -
The Boeing Company 2012 Annual Report at Boeing, We Aspire to Be the Strongest, Best and Best-Integrated Aerospace- Based Company in the World— for Today and Tomorrow
The Boeing Company 2012 Annual Report At Boeing, we aspire to be the strongest, best and best-integrated aerospace- based company in the world— for today and tomorrow. The Boeing Company Contents Boeing is the world’s largest aerospace Operational Summary 1 company and leading manufacturer Message From Our Chairman 2 of commercial airplanes and defense, space and security systems. The top The Executive Council 7 U.S. exporter, Boeing supports airlines and U.S. and allied government cus- Financial Results 8 tomers in more than 150 countries. Our Form 10-K 9 products and tailored services include commercial and military aircraft, satel- Selected Programs, lites, weapons, electronic and defense Products and Services 122 systems, launch systems, advanced Shareholder Information 129 information and communication sys- Cover photo: The liquid tems, and performance-based logistics Board of Directors 130 hydrogen–powered high- and training. With corporate offices in Company Officers 130 altitude long-endurance Chicago, Boeing employs more than Phantom Eye unmanned 174,000 people across the United aircraft system States and in 70 countries. In addition, Photo above: The new our enterprise leverages the talents of 737 MAX—designed for hundreds of thousands of skilled people maximum efficiency, reliabil- working for Boeing suppliers worldwide. ity and customer appeal Financial Highlights U.S. dollars in millions except per share data 2012 2011 2010 2009 2008 Revenues 81,698 68,735 64,306 68,281 60,909 Net earnings 3,900 4,018 3,307 1,312 2,672 Earnings per share* 5.11 5.33 4.46 1.87 3.65 Operating margins 7.7% 8.5% 7.7% 3.1% 6.5% Operating cash flow 7,508 4,023 2,952 5,603 (401) Contractual backlog 372,355 339,657 303,955 296,500 323,860 Total backlog† 390,228 355,432 320,826 315,558 351,926 * Represents diluted earnings per share from continuing operations. -
ARC-OVER April
April Upcoming Events Next Board Meeting: May 6 Next General Meeting: May 12 Field Day: June 27 & 28 Pacificon: October 16 - 18 Dayton Hamvention May 15 TARC Meeting April 14, 2015 Turlock, War Memorial 7:00 p.m. Ron Roos, KJ6KNL, Our honorable President, called the meeting to order Pledge of Allegiance, All members and guests introduced themselves. Dylan Low, KK6SYD, was a first time guest. All were welcomed. Dick Decker, Vice President, K6SUU, gave an interesting presentation on Hams In Space. This was the topic members showed the most interest in. Fox 1 will launch on August 27th, 2015. To contact Space Stations in the past the Uplink was on VHF and the Downlink on UHF. This is now reversed, the Uplink will be UHF and the Downlink will be VHF. For a full copy of the Powerpoint Presentation, Dick announced that those interested could send an email to him and he would send it to those requesting it. Included in the Powerpoint will be the links for further information. Dick explained that Space stations were easier to use than Satellites. A variety of antennas were shown and discussed. They included; The Yagi, Two Elk Antennas (mounted on PVC) and one that really measured up; The Tape Measure Antenna. Dick informed all that he has a radio that members could use to hit the Space Station. Please contact him if you are interested. The process is pretty simple and it is rewarding when you get your card back in the mail! Dick’s email is; [email protected] 1 Ron Roos, asked members if they had read the minutes from our March 10th Meeting. -
Space Shuttle Solid Rocket Motor Plume Pressure and Heat Rate Measurements
2012 New Orleans Conferences Space Shuttle Solid Rocket Motor Plume Pressure and Heat Rate Measurements Journal: 2012 New Orleans Conferences Manuscript ID: Draft luMeetingID: 2227 Date Submitted by the Author: n/a Contact Author: Struchen, Leah http://mc.manuscriptcentral.com/aiaa-mfd12 Page 1 of 23 2012 New Orleans Conferences Space Shuttle Solid Rocket Motor Plume Pressure and Heat Rate Measurements Wulf von Eckroth, Ph.D.,1 Leah Struchen,2 Tom Trovillion, Ph.D.,3 Rafael Perez, Ph.D.,4 and Shaun Nerolich5 United Space Alliance, LLC., Kennedy Space Center, FL, 32780 and Chris Parlier6 NASA, Kennedy Space Center, FL, 32899 The Solid Rocket Booster (SRB) Main Flame Deflector (MFD) at Launch Complex 39A was instrumented with sensors to measure heat rates, pressures, and temperatures on the final three Space Shuttle launches. Because the SRB plume is hot and erosive, a robust Tungsten Piston Calorimeter was developed to compliment measurements made by off-the- shelf sensors. Witness materials were installed and their melting and erosion response to the Mach 2 / 4000°F / 4-second duration plume was observed. The data show that the specification used for the design of the MFD thermal protection system over-predicts heat rates by a factor of 3 and under-predicts pressures by a factor of 2. These findings will be used to baseline NASA Computational Fluid Dynamics (CFD) models and develop innovative MFD designs for the Space Launch System (SLS) before this vehicle becomes operational in 2017. Nomenclature KSC = Kennedy Space Center FEM = Finite Element Model MSFC = Marshall Space Flight Center PSD = power spectral density USA = United Space Alliance, LLC. -
STS-134 Press
CONTENTS Section Page STS-134 MISSION OVERVIEW ................................................................................................ 1 STS-134 TIMELINE OVERVIEW ............................................................................................... 9 MISSION PROFILE ................................................................................................................... 11 MISSION OBJECTIVES ............................................................................................................ 13 MISSION PERSONNEL ............................................................................................................. 15 STS-134 ENDEAVOUR CREW .................................................................................................. 17 PAYLOAD OVERVIEW .............................................................................................................. 25 ALPHA MAGNETIC SPECTROMETER-2 .................................................................................................. 25 EXPRESS LOGISTICS CARRIER 3 ......................................................................................................... 31 RENDEZVOUS & DOCKING ....................................................................................................... 43 UNDOCKING, SEPARATION AND DEPARTURE ....................................................................................... 44 SPACEWALKS ........................................................................................................................ -
IAF-01-T.1.O1 Progress on the International Space Station
https://ntrs.nasa.gov/search.jsp?R=20150020985 2019-08-31T05:38:38+00:00Z IAF-01-T.1.O1 Progress on the International Space Station - We're Part Way up the Mountain John-David F. Bartoe and Thomas Holloway NASA Johnson Space Center, Houston, Texas, USA The first phase of the International Space Station construction has been completed, and research has begun. Russian, U.S., and Canadian hardware is on orbit, ard Italian logistics modules have visited often. With the delivery of the U.S. Laboratory, Destiny, significant research capability is in place, and dozens of U.S. and Russian experiments have been conducted. Crew members have been on orbit continuously since November 2000. Several "bumps in the road" have occurred along the way, and each has been systematically overcome. Enormous amounts of hardware and software are being developed by the International Space Station partners and participants around the world and are largely on schedule for launch. Significant progress has been made in the testing of completed elements at launch sites in the United States and Kazakhstan. Over 250,000 kg of flight hardware have been delivered to the Kennedy Space Center and integrated testing of several elements wired together has progressed extremely well. Mission control centers are fully functioning in Houston, Moscow, and Canada, and operations centers Darmstadt, Tsukuba, Turino, and Huntsville will be going on line as they are required. Extensive coordination efforts continue among the space agencies of the five partners and two participants, involving 16 nations. All of them continue to face their own challenges and have achieved significant successes. -
Space Shuttle Discovery Launched on the First Post-Columbia Mission on July 26, 2005, 905 Days After the Accident
AFTERWORD Space shuttle Discovery launched on the first post-Columbia mission on July 26, 2005, 905 days after the accident. Coincidentally, the launch took place at 10:39 A.M. EDT, the same time as Columbia’s launch on its final flight. STS-114 was the culmination of a $1.4 billion effort to improve the shuttle, most notably the External Tank. The bipod foam was replaced with an electrical heater to prevent ice from forming. Marshall Space- flight Center External Tank manager Sandy Coleman promised that no foam larger than a marshmallow would fall off of the improved tank. In the 147-page press kit’s description of all of the improvements to the shuttle, KSC’s acceptance of the industry standard definition for FOD (Foreign Object Debris) is presented as a positive. In a spin doctor- ing attempt it’s described how new FOD procedures improve safety, and ignores that FOD rules existed until two years before the Columbia acci- dent when the rules were reduced in a conscious move to make more bonus money for the contractor. Over 100 tracking cameras viewed Discovery’s launch. The E208 camera in Cocoa Beach, the one that had been “soft focused” on STS- 107, was replaced with a state-of-the-art setup. Cameras were also mounted on Discovery’s External Tank and Solid Rocket Boosters, and The bipod fitting on STS-114, on the right, shows the most significant external change— there is no longer any foam on the bipod fitting. 428 AFTERWORD 429 two aircraft with high-definition cameras offered the unique perspective of a shuttle flying toward the viewer. -
Thesisbook.Fm(Appendix
Appendix D THE INTERNATIONAL SPACE STATION This appendix presents an review of the International Space Station Program and the facil- ities that are or will be available for research. First, the appendix reviews the objectives of the ISS and the identified research directions for the station. Next, it presents an overview of all the ISS components. That is followed by a more in depth review of the components which directly support research aboard the ISS. The appendix ends with a presentation of the identified challenges of the ISS and expected upgrades to the program to overcome these challenges. Chapter 2 utilizes this review to identify the most important resources provided by the ISS. D.1 Objectives and Research Directions The objectives of the ISS as stated in the ISS Familiarization Manual developed by NASA are: "The purpose of the ISS is to provide an “Earth orbiting facility that houses experiment payloads, distributes resource utilities, and supports permanent human habitation for conducting research and science experiments in a microgravity environment.” (ISSA IDR no. 1, Reference Guide, March 29, 1995) "This overall purpose leads directly into the following specific objectives of the ISS program: • Develop a world-class orbiting laboratory for conducting high-value sci- entific research 391 392 APPENDIX D • Provide access to microgravity resources as early as possible in the assembly sequence • Develop ability to live and work in space for extended periods • Develop effective international cooperation • Provide a testbed for developing 21st Century technology." [NASA, 1998] After creating these objectives, NASA worked to further detail the research objectives of the ISS. -
Columbia and Challenger: Organizational Failure at NASA
ARTICLE IN PRESS Space Policy 19 (2003) 239–247 Columbia and Challenger: organizational failure at NASA Joseph Lorenzo Hall* Astronomy Department/School of Information Management and Systems, Astronomy Department, University of California at Berkeley, 601 Campbell Hall, Berkeley, CA 94720-3411, USA Abstract The National Aeronautics and Space Administration (NASA)—as the global leader in all areas of spaceflight and space science— is a unique organization in terms of size, mission, constraints, complexity and motivations. NASA’s flagship endeavor—human spaceflight—is extremely risky and one of the most complicated tasks undertaken by man. It is well accepted that the tragic destruction of the Space Shuttle Challenger on 28 January 1986 was the result of organizational failure. The surprising disintegration of the Space Shuttle Columbia in February 2003—nearly 17 years to the day after Challenger—was a shocking reminder of how seemingly innocuous details play important roles in risky systems and organizations. NASA as an organization has changed considerably over the 42 years of its existence. If it is serious about minimizing failure and promoting its mission, perhaps the most intense period of organizational change lies in its immediate future. This paper outlines some of the critical features of NASA’s organization and organizational change, namely path dependence and ‘‘normalization of deviance’’. Subsequently, it reviews the rationale behind calling the Challenger tragedy an organizational failure. Finally, it argues that the recent Columbia accident displays characteristics of organizational failure and proposes recommendations for the future. r 2003 Elsevier Ltd. All rights reserved. 1. Introduction in 1967 are examples of failure at NASA that cost a total of 17 astronaut lives. -
The New Vision for Space Exploration
Constellation The New Vision for Space Exploration Dale Thomas NASA Constellation Program October 2008 The Constellation Program was born from the Constellation’sNASA Authorization Beginnings Act of 2005 which stated…. The Administrator shall establish a program to develop a sustained human presence on the moon, including a robust precursor program to promote exploration, science, commerce and U.S. preeminence in space, and as a stepping stone to future exploration of Mars and other destinations. CONSTELLATION PROJECTS Initial Capability Lunar Capability Orion Altair Ares I Ares V Mission Operations EVA Ground Operations Lunar Surface EVA EXPLORATION ROADMAP 0506 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 LunarLunar OutpostOutpost BuildupBuildup ExplorationExploration andand ScienceScience LunarLunar RoboticsRobotics MissionsMissions CommercialCommercial OrbitalOrbital Transportation ServicesServices forfor ISSISS AresAres II andand OrionOrion DevelopmentDevelopment AltairAltair Lunar LanderLander Development AresAres VV and EarthEarth DepartureDeparture Stage SurfaceSurface SystemsSystems DevelopmentDevelopment ORION: NEXT GENERATION PILOTED SPACECRAFT Human access to Low Earth Orbit … … to the Moon and Mars ORION PROJECT: CREW EXPLORATION VEHICLE Orion will support both space station and moon missions Launch Abort System Orion will support both space stationDesigned and moonto operate missions for up to 210 days in Earth or lunar Designedorbit to operate for up to 210 days in Earth or lunar orbit Designed for lunar