SHUTTLE COLUMBIA: DISASTER in the SKIES YV Introduction
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Final Report of the International Space Station Independent Safety
I Contents Executive Summary........................................................................................ 1 Principal Observations ..................................................................................... 3 Principal Recommendations ............................................................................. 3 1. Introduction..................................................................................................... 5 Charter/Scope ................................................................................................... 5 Approach........................................................................................................... 5 Report Organization ......................................................................................... 5 2. The International Space Station Program.................................................... 7 International Space Station Characteristics..................................................... 8 3. International Space Station Crosscutting Management Functions............ 12 Robust On-Orbit Systems.................................................................................. 12 The Design ........................................................................................................ 12 Verification Requirements ................................................................................ 12 Physical (Fit) Verification ................................................................................ 13 Multi-element Integrated Test.......................................................................... -
Robotic Arm.Indd
Ages: 8-12 Topic: Engineering design and teamwork Standards: This activity is aligned to national standards in science, technology, health and mathematics. Mission X: Train Like an Astronaut Next Generation: 3-5-ETS1-2. Generate and compare multiple possible solutions to a problem based on how well each is likely A Robotic Arm to meet the criteria and constraints of the problem. 3-5-ETS1-3. Plan and carry out fair tests in which variables are controlled and failure points are considered to identify aspects of a model or prototype that can be EDUCATOR SECTION (PAGES 1-7) improved. STUDENT SECTION (PAGES 8-15) Background Why do we need robotic arms when working in space? As an example, try holding a book in your hands straight out in front of you and not moving them for one or two minutes. After a while, do your hands start to shake or move around? Imagine how hard it would be to hold your hands steady for many days in a row, or to lift something really heavy. Wouldn’t it be nice to have a really long arm that never gets tired? Well, to help out in space, scientists have designed and used robotic arms for years. On Earth, scientists have designed robotic arms for everything from moving heavy equipment to performing delicate surgery. Robotic arms are important machines that help people work on Earth as well as in space. Astronaut attached to a robotic arm on the ISS. Look at your arms once again. Your arms are covered in skin for protection. -
International Space Station Program Mobile Servicing System (MSS) To
SSP 42004 Revision E Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part I International Space Station Program Revision E, May 22, 1997 Type 1 Approved by NASA National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NAS15–10000 SSP 42004, Part 1, Revision E May 22, 1997 REVISION AND HISTORY PAGE REV. DESCRIPTION PUB. DATE C Totally revised Space Station Freedom Document into an International Space Station Alpha Document 03–14–94 D Revision D reference PIRNs 42004–CS–0004A, 42004–NA–0002, 42004–NA–0003, TBD 42004–NA–0004, 42004–NA–0007D, 42004–NA–0008A, 42004–NA–0009C, 42004–NA–0010B, 42004–NA–0013A SSP 42004, Part 1, Revision E May 22, 1997 INTERNATIONAL SPACE STATION PROGRAM MOBILE SERVICING SYSTEM TO USER (GENERIC) INTERFACE CONTROL DOCUMENT MAY 22, 1997 CONCURRENCE PREPARED BY: PRINT NAME ORGN SIGNATURE DATE CHECKED BY: PRINT NAME ORGN SIGNATURE DATE SUPERVISED BY (BOEING): PRINT NAME ORGN SIGNATURE DATE SUPERVISED BY (NASA): PRINT NAME ORGN SIGNATURE DATE DQA: PRINT NAME ORGN SIGNATURE DATE i SSP 42004, Part 1, Revision E May 22, 1997 NASA/CSA INTERNATIONAL SPACE STATION PROGRAM MOBILE SERVICING SYSTEM (MSS) TO USER INTERFACE CONTROL DOCUMENT MAY 22, 1997 Print Name For NASA DATE Print Name For CSA DATE ii SSP 42004, Part 1, Revision E May 22, 1997 PREFACE SSP 42004, Mobile Servicing System (MSS) to User Interface Control Document (ICD) Part I shall be implemented on all new Program contractual and internal activities and shall be included in any existing contracts through contract changes. -
Nanoracks External Cubesat Deployer (NRCSD-E) Interface Definition Document (IDD) 08/31/2018
NanoRacks External CubeSat Deployer (NRCSD-E) Interface Definition Document (IDD) 08/31/2018 Doc No: NR-NRCSD-S0004 Revision: - THIS DOCUMENT HAS NOT BEEN APPROVED FOR PUBLIC RELEASE BY THE UNITED STATES DEPARTMENT OF DEFENSE. NANORACKS PROPRIETARY RIGHTS ARE INCLUDED HEREIN. RECIPIENT AGREES THAT NEITHER THIS DOCUMENT NOR THE INFORMATION DISCUSSED HEREIN NOR ANY PART THEREOF SHALL BE REPRODUCED OR DISCLOSED TO OTHERS. NanoRacks External CubeSat Deployer IDD NRCSD External Doc No: NR-NRCSD-S0004 Rev: - NanoRacks External CubeSat Deployer Interface Definition Document (IDD) Prepared by Nathan Daniels; Mission Manager; Date Reviewed by Henry Martin; Senior Mission Manager; Date Reviewed by Conor Brown; External Payloads Manager; Date Reviewed by Troy Guy; Avionics Manager; Date Reviewed by Teresa Freund; Safety Engineer; Date Approved by Mike Lewis; Chief Technology Officer; Date NanoRacks External CubeSat Deployer IDD NRCSD External Doc No: NR-NRCSD-S0004 Rev: - List of Revisions Revision Revision Date Revised By Revision Description - 8/31/2018 N. Daniels Initial Release NanoRacks External CubeSat Deployer IDD NRCSD External Doc No: NR-NRCSD-S0004 Rev: - Table of Contents 1 Introduction 1 1.1 Purpose 1 1.1.1 Scope 1 1.2 Usage 1 1.3 Exceptions 1 2 Acronyms, Definitions, and Applicable Documents 2 3 NanoRacks External CubeSat Deployer System Overview 5 3.1 NRCSD-E Overview and Payload Capacity 5 3.2 NRCSD-E Coordinate System 5 3.3 NRCSD-E Design Features 6 3.4 NRCSD-E Operations Overview 7 3.4.1 Schedule 7 3.4.2 Ground Operations 8 3.4.3 -
Spaceflight a British Interplanetary Society Publication
SpaceFlight A British Interplanetary Society publication Volume 60 No.8 August 2018 £5.00 The perils of walking on the Moon 08> Charon Tim Peake 634072 Russia-Sino 770038 9 Space watches CONTENTS Features 14 To Russia with Love Philip Corneille describes how Russia fell in love with an iconic Omega timepiece first worn by NASA astronauts. 18 A glimpse of the Cosmos 14 Nicholas Da Costa shows us around the Letter from the Editor refurbished Cosmos Pavilion – the Moscow museum for Russian space achievements. In addition to the usual mix of reports, analyses and commentary 20 Deadly Dust on all space-related matters, I am The Editor looks back at results from the Apollo particularly pleased to re- Moon landings and asks whether we are turning introduce in this month’s issue our a blind eye to perils on the lunar surface. review of books. And to expand that coverage to all forms of 22 Mapping the outer limits media, study and entertainment be SpaceFlight examines the latest findings it in print, on video or in a concerning Charon, Pluto’s major satellite, using 18 computer game – so long as it’s data sent back by NASA's New Horizons. related to space – and to have this as a regular monthly contribution 27 Peake Viewing to the magazine. Rick Mulheirn comes face to face with Tim Specifically, it is gratifying to see a young generation stepping Peake’s Soyuz spacecraft and explains where up and contributing. In which this travelling display can be seen. regard, a warm welcome to the young Henry Philp for having 28 38th BIS Russia-Sino forum provided for us a serious analysis Brian Harvey and Ken MacTaggart sum up the of a space-related computer game latest Society meeting dedicated to Russian and which is (surprisingly, to this Chinese space activities. -
Benefits of a Single-Person Spacecraft for Weightless Operations (Stop Walking and Start Flying)
42nd International Conference on Environmental Systems AIAA 2012-3630 15 - 19 July 2012, San Diego, California Benefits of a Single-Person Spacecraft for Weightless Operations (Stop Walking and Start Flying) Brand N. Griffin1 Gray Research, Engineering, Science, and Technical Services Contract, 655 Discovery Drive Ste. 300, Huntsville, AL 35806 U.S.A Historically, less than 20 percent of crew time related to extravehicular activity (EVA) is spent on productive external work. For planetary operations space suits are still the logical choice; however, for safe and rapid access to the weightless environment, spacecraft offer compelling advantages. FlexCraft, a concept for a single-person spacecraft, enables any- time access to space for short or long excursions by different astronauts. For the International Space Station (ISS), going outside is time-consuming, requiring pre-breathing, donning a fitted space suit, and pumping down an airlock. For each ISS EVA this is between 12.5 and 16 hours. FlexCraft provides immediate access to space because it operates with the same cabin atmosphere as its host. Furthermore, compared to the space suit pure oxygen environment, a mixed gas atmosphere lowers the fire risk and allows use of conventional materials and systems. For getting to the worksite, integral propulsion replaces hand-over- hand translation or having another crew member operate the robotic arm. This means less physical exertion and more time at the work site. Possibly more important, in case of an emergency, FlexCraft can return from the most distant point on ISS in less than a minute. The one-size-fits-all FlexCraft means no on-orbit inventory of parts or crew time required to fit all astronauts. -
GLOBAL SPACE SECTOR MARKET TRENDS and DRIVERS Table of Contents
foreword MISSION OF THE CANADIAN SPACE AGENCY I am very pleased to release the latest edition of our Global Space Market Trends and Drivers 2002. Developed by the External Relations Directorate of the Canadian Space The Canadian Space Agency is committed to leading Agency and now in its fourth year of publication, it provides an in-depth analysis the development and application of space knowledge of the principal market and regulatory trends in key areas of the Canadian Space for the benefit of Canadians and humanity. Program, namely: satellite communications; remote sensing; robotics, navigation and space science. The External Relations Directorate The External Relations Directorate manages the Over the past year, as President of the Canadian Space Agency, I have benefited from strategic relationships between the Canadian Space numerous exchanges and consultations with all partners in the Canadian Space Sector Agency and its domestic and international partners. and have developed a profound appreciation of both the multitude of challenges con- Key mandates include the development and imple- fronting us and the great opportunities which lie in our future. mentation of policies and strategies relating to cooperation partnerships with domestic stakeholders I note with pride that the Canadian Space Sector remains internationally competitive, (Federal and Provincial governments, industry and export-oriented and is recognized as a major contributor to Canada’s goal of becoming academia) and international agencies and industries, the best knowledge-based economy in the world. For example, the results of a recent as well as support to the commercial initiatives round of consultations with our federal departments and agencies underscored the very of Canadian space companies on world markets. -
Flight 6A: Deployment of the Space Station Remote Manipulator System (SSRMS)
Proceeding of the 6th International Symposium on Artificial Intelligence and Robotics & Automation in Space: i-SAIRAS 2001, Canadian Space Agency, St-Hubert, Quebec, Canada, June 18-22, 2001. Flight 6A: Deployment and Checkout of the Space Station Remote Manipulator System (SSRMS) Rod McGregor1 and Layi Oshinowo2 Canadian Space Agency 6767 Route de l’Aeroport, St-Hubert, Quebec, Canada, J3Y 8Y9 [email protected] [email protected] Keywords Activation, Canadarm2, Checkout, Deployment, Flight 6A, International Space 1.0 Introduction Station, ISS, Mobile Servicing System, MSS, Space Station Remote Manipulator System, The SSRMS was built for the Canadian Space SSRMS, STS-100. Agency (CSA) by MacDonald Dettwiler Space and Advanced Robotics (formerly Spar Abstract Aerospace) located in Brampton, Ontario. The SSRMS, or Canadarm2, is the principal Flight 6A of the International Space Station component of the MSS, Canada’s primary (ISS) assembly sequence, is currently completing hardware contribution to the International Space stage (shuttle departed) operations after its Station program. The Mobile Base System successful docked phase in April of this year. (MBS) and Special Purpose Dexterous This mission marks the delivery and checkout of Manipulator (SPDM) follow later on Flights UF- the first element of the Canadian Mobile 2 and UF-4 respectively. Delivery of the MSS Servicing System (MSS) – the Space Station components has been planned to progressively Remote Manipulator System (SSRMS). The expand the required robotic reach envelope for presence of this seven-jointed, re-locatable, and component installation and servicing, currently functionally-redundant robotic manipulator on- at the limit of the SRMS. orbit, with it’s larger reach and mass-handling The Canadarm2 was delivered to the ISS by the capacity, will allow for the expansion of the Space Shuttle Endeavor during the recently Station towards its assembly-complete form; completed Flight 6A mission. -
The International Space Station (ISS) Is an Experiment in the Design, Development, and Assembly of an Orbital Space Facility. It
The International Space Station (ISS) is an experiment in the design, development, and assembly of an orbital space facility. It serves as a elements habitat for its crew, a command post for orbital operations, and a port for the rendezvous and berthing of smaller orbiting vehicles. It functions as an orbital microgravity and life sciences laboratory, a test bed for new technologies in areas like life support and robotics, and a platform for astronomical and Earth observations. PMA 2 berthed on Node 1 serves as a primary docking port for the Space Shuttle. The U.S. Lab Module Destiny provides research and habitation accommodations. Node 2 is to the left; the truss is mounted atop the U.S. Lab; Node 1, Unity, is to the right; Node 3 and the Cupola are below and to the right. INTERNATIONAL SPACE STATION GUIDE ELEMENTS 23 ARCHITECTURE DESIGN EVOLUTION Architecture Design Evolution Why does the ISS look the way it does ? The design evolved over more than a decade. The modularity and size of the U.S., Japanese, and European elements were dictated by the use of the Space Shuttle as the primary launch vehicle and by the requirement to make system components maintainable and replaceable over a lifetime of many years. When the Russians joined the program in 1993, their architecture was based largely on the Mir and Salyut stations they had built earlier. Russian space vehicle design philosophy has always emphasized automated operation and remote control. The design of the interior of the U.S., European, and Japanese elements was dictated by four specific principles: modularity, maintainability, reconfigurability, and accessibility. -
Getting in Your Space: Learning from Past Rendezvous and Proximity Operations
CENTER FOR SPACE POLICY AND STRATEGY MAY 2018 GETTING IN YOUR SPACE: LEARNING FROM PAST RENDEZVOUS AND PROXIMITY OPERATIONS REBECCA REESMAN, ANDREW ROGers THE AEROSPACE CORPORATION © 2018 The Aerospace Corporation. All trademarks, service marks, and trade names contained herein are the property of their respective owners. Approved for public release; distribution unlimited. OTR201800593 REBECCA REESMAN Dr. Rebecca Reesman is a member of the technical staff in The Aerospace Corporation’s Performance Modeling and Analysis Department, where she supports government customers in the national security community. Before joining Aerospace in 2017, she was an American Institute of Physics Congressional Fellow handling space, cybersecurity, and other technical issues for a member of Congress. Prior to the fellowship, she was a research scientist at the Center for Naval Analysis, providing technical and analytical support to the Department of Defense, with particular focus on developing and executing wargames. Reesman received her Ph.D. in physics from the Ohio State University and a bachelor’s degree from Carnegie Mellon University. ANDREW ROGERS Dr. Andrew Rogers is a member of the technical staff in The Aerospace Corporation’s Mission Analysis and Operations Department. His expertise is in relative motion astrodynamics, control theory, and space mission design. Rogers supports government customers in the areas of concept- of-operations development, orbital analysis, and small satellite technology development. Prior to joining Aerospace in 2016, Rogers received his Ph.D. in aerospace engineering and a bachelor of science in mechanical engineering from Virginia Polytechnic Institute and State University. CONTRIBUTORS The authors would like to acknowledge contributions from Greg Richardson, Josh Davis, Jose Guzman, George Pollock, Karen L. -
Canadian Space
COTS View Case Study: Space Station Robot Embeds Ada Despite rumors of its demise, Adas is at the heart of the International Space Station’s in-orbit Canadarm 2 where it assures software safety and reliability. The ISS-based, next-generation Canadarm 2, the key element Robert Dewar, President, Ada Core Technologies of the MSS, is a bigger, better, smarter version of Canadarm, the robotic arm that operates from the cargo bay of the Space Shuttle. hile safety-critical characteristics have been introduced This arm is capable of handling large payloads and assisting with into the design of many programming languages, Ada docking the space shuttle to the space station. The new arm, built Wis the language specifically targeted at “life-critical” specifically for the space station, is 17.6 meters (57.7 feet) long systems. Developed between 1975 and 1984 by the US Department when fully extended and has seven motorized joints, each of of Defense (DoD), Ada has been classically targeted for use in which operates as a complex real-time embedded control system. mission-critical embedded systems that emphasize safety, low cost, Canadarm 2 is “self-relocatable” and can move around the sta- and a near-perfect degree of reliability. The most important safety tion’s exterior like an inchworm. Each end of the arm is equipped features that make Ada ideal for development of fail-safe software with a specialized mechanism called a Latching End Effector that include its information-hiding capability, its ability to provide can lock its free end on one of many special fixtures, called Power re-useable code and its “strong typing”, which helps detect and Data Grapple Fixtures placed strategically around the station, and solve many types of coding errors at compile time, very early in then detach its other end and pivot it forward. -
International Space Station Robotic Systems and Operations
INTERNATIONAL SPACE STATION ROBOTIC SYSTEMS OPERATIONS – A HUMAN FACTORS PERSPECTIVE Nancy J. Currie, NASA – Johnson Space Center, Houston, Texas Brian Peacock, National Space Biomedical Research Institute, Houston, Texas Assembly and maintenance of the International Space Station (ISS) relies heavily on the use of extra- vehicular robotic systems. When fully assembled the ISS robotics complement will include three main manipulators, two small dexterous arms, and a mobile base and transporter system. The complexity and mobility of the systems and limited opportunities for direct viewing of the Space Station’s exterior makes telerobotic operations an especially challenging task. Although fundamental manipulator design, control systems, and strategies for autonomous versus manual control vary greatly between the systems, commonality in the design of workstation controls and displays is considered essential to enhance operator performance and reduce the possibility of errors. Principal human factors opportunities are associated with workstation layout, human-computer interface considerations, adequacy of alignment cues for maintenance of safe approach corridors during mating tasks, spatial awareness challenges, integration of supplemental computer graphic displays to enhance operator global situational awareness, and training methodologies for preservation of critical skills during long-duration missions. INTRODUCTION When complete, the ISS will be the largest and most complicated spacecraft ever assembled. Five international space agencies