The International Space Station a Guide for European Users
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee
National Aeronautics and Space Administration Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee Jason Crusan | Advanced Exploration Systems Director | NASA Headquarters 2 Human Exploration of Mars Is Hard Common Capability Needs Identified from Multiple Studies Days Reliable In-Space 800-1,100 44 min Transportation Total me crew is Maximum two- away from Earth – way communicaon for orbit missions all in 2me delay – 300 KW Micro-g and Radia2on Autonomous Opera2ons Total connuous transportaon power 130 t Heavy-LiA Mass 20-30 t Long Surface Stay Multiple Ability to 500 Days Launches per land large mission payloads Surface Operations Dust Toxicity and 100 km 11.2 km/s Long Range Explora2on Earth Entry Speed 20 t Oxygen produced for ascent to orbit - ISRU 3 The Habitation Development Challenge HABITATATION CAPABILITY Days 800-1,100 Habitation Systems – Total me crew is AES/ISS/STMD away from Earth – • Environmental Control & Life Support for orbit missions all in • Autonomous Systems Micro-g and Radia2on Integrated • EVA testing on ISS • Fire Safety • Radiation Protection Habitation Systems - Crew Health – HRP Long Surface Stay • Human Research 500 Days • Human Performance • Exercise PROVING GROUND Validation in cislunar space • Nutrition Habitation Capability– NextSTEP BAA / Int. Partners • Studies and ground prototypes of pressurized volumes 4 Specific Habitation Systems Objectives TODAY FUTURE Habitation The systems, tools, and protec:ons that allow Systems Elements humans to live and work -
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. -
Internationale Raumstation ISS International Space Station ISS
Internationale Raumstation ISS International Space Station ISS www.DLR.de Europäisches Labormodul COLUMBUS European laboratory module COLUMBUS US-Labormodul DESTINY japanisches Labormodul KIBO US laboratory module DESTINY Japanese laboratory module KIBO Russisches Cargo-Modul SaRja (Functional Cargo Block) Russian cargo module ZARYA 20. November 1998: (Functional Cargo Block) 24. Februar 2011: Start des ersten ISS-Moduls: Start des permanenten der Functional Cargo Block Logistikmoduls PMM (FGB) Sarja Leonardo November 20, 1998: February 24, 2011: launch of the first ISS module: launch of the logistic the Functional Cargo Block module PMM Leonardo (FGB) Zarya 12. juli 2000: 8. Februar 2010: Start des Service- und Wohn- Start des Aussichtsmoduls moduls Swesda Cupola July 12, 2000: February 8, 2011: launch of the observatory launch of the service and Russisches Service-Modul habitation module Zvezda module Cupola SwESDa Russian service module 10. November 2009: 7. Februar 2001: Europäisches Logistikmodul aTV-2 Start des amerikanischen ZvEZDA Start des russischen Docking- Labormoduls DESTINY (automated Transfer Vehicle) moduls POISK Mini-Research „johannes Kepler“ Module 2 February 7, 2001: 7. Februar 2008: 31. Mai 2008: launch of the American European logistics module ATv-2 November 10, 2009: Start des europäischen Start des zweiten Teils des laboratory module DESTINY (Automated Transfer vehicle) launch of the Russian docking Labormoduls japanischen Labormoduls “Johannes Kepler” module POISK Mini-Research COLUMBUS KIBO Pressurized Module (PM) Module 2 February 7, 2008: May 31, 2008: launch of the European launch of the second part of the research module Japanese laboratory module KIBO COLUMBUS Pressurized Module (PM) ISS ISS © NASA, ESA, DLR Forschung im All für die Menschen auf der Erde Research in Space for Mankind on Earth. -
Space Station Freedom. a Foothold on the Future. INSTITUTION National Aeronautics and Space Administration, Washington, DC
DOCUMENT RESUME ED 310 939 SE 050 885 AUTHOR David, Leonard TITLE Space Station Freedom. A Foothold on the Future. INSTITUTION National Aeronautics and Space Administration, Washington, DC. Office of Space Sta.:Ion. REPORT NO NP-107/10-88 PUB DATE 89 NOTE 49p.; Colored photographs and drawings may not reproduce well. PUB TYPE Reports - Descriptive (141) EDRS PRICE MF01/PCO2 Plus Postage. DESCRIPTORS *Aerospace Technology; Engineering Technology; Planning; *Satellites (Aerospace); Science Materials; *Science Programs; *Scientific Research; *Space Exploration; *Space Sciences IDENTIFIERS *Space Station ABSTRACT This booklet describes the planning of the space station program. Sections included are: (1) "Introduction"; (2) "A New Era Begins" (discussing scientific experiments on the space station); (3) "Living in Space";(4) "Dreams Fulfilled" (summarizing the history of the space station development, including the skylab and shuttle); (5) "Building a Way Station to Worlds Beyond" (illustrating an approach to building the space station); (6) ''Orbital Mechanics" (discussing the maneuverability of the space station, including robotic application);(7) "Evolving with Versatility" (describing blueprints for expanding a space station); and (8) "Foothold on the Future" (discussing the future plans of the space station program). (YP) **************************************-******************************* * Reproductions supplied by EDRS are the best that can be made * from the original document. *********************************************************************A* -
Unique Scientific Laboratory Instrument for Sky Monitoring (MVN) Bi-Axial Pointing Platform with Hyper-Spectrometer
Research Exploration Utilization Unique scientific laboratory Instrument for sky monitoring (MVN) Bi-axial pointing platform with hyper-spectrometer «Photon-Gamma» apparatus Radiometric sounder РК-21-8 Plasma-wave apparatus «Obstanovka» Plasma-wave apparatus «Obstanovka» Plasma-wave diagnostic device «Seysmoprognoz» High-speed data transmitter Multilayer scintillation spectrometer «Alpha-electron» MLM Mini Research Module (MRM1) • Universal workstations inside (16) and outside (13) will be mounted • Payload pressurized volume about 6 м3, power capability of 2,5 kW (enabling of experiments with electric furnaces) • ERA arm and automated airlock • New universal facilities and tools (multizone furnace, spectrophotometers, vibro-protecting and pointing platforms, glove box, thermostats etc.) Mini Research Module (MRM2) MLM PAYLOADS • MLM will support approximately 40% of the “Soyuz” spacecraft total amount of experiment planned for the ISS Mini Research Module (MRM2) RS “Zvezda“ service module (SM) Mini Research Module (MRM1) “Zarya” • Two scientific and power supply modules of “Progress” resupply vehicle about 15 kW each by 2015. This provides fully independent power supply of RS ISS • Data relay system based on «Luch» relay satellites (up to 300 Mbps). Multipurpose Laboratory • Starting from 2016 Russia plans also to use Module (MLM) АСUSOS МКС for experiments automatic spacecraft “OKA-T” maintained at the periodical docking with ISS. “Soyuz” spacecraft • In total, the plans call for 8 modules of the ISS RS by 2015, with total power capability of 30 kW Science Power Platform (SPP-2) and the payload pressurized volume about 40 “Soyuz” spacecraft Science Power Platform (SPP-1) cubic meters. Nodal module (NM) 102 “Soyuz” spacecraft >170 1998 ------ 2000 2001 --- 2003 --- 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 RS ISS assembling 1 stage 2 stage Pirs Zarya Zvezda MRM2 MRM1 MLM NM SPP-1 SPP-2 Russian crew quota – 3 5 6 16 18 8 45 About 130 unites of scientific 38 equipment of about ton total mass are housed on the ISS RS. -
Orb2: Spherical Space Station Designed for Single Launch and On-Orbit Assembly
Orb2: Spherical Space Station Designed for Single Launch and On-Orbit Assembly Vojtech Holub ∗ Unaffiliated With upcoming heavy and super-heavy lift rockets targeted for launch in 2021, a new class of payloads can be launched into low Earth orbit. This paper presents a design for a space station capable of being lifted by a single Blue Origin New Glenn vehicle. Once assembled on-orbit, it contains more than twice the pressurized volume of the International Space Station. The pressurized volume of traditional space station modules is limited by the dimensions of the payload fairing. The proposed Orb2 design consists of a spherical habitation module and a service module. The habitation module avoids the volume limitation by being launched in a flat-packed stack and assembled and welded robotically in orbit. Using CAD and finite element analysis, this paper shows that the habitation module contains approximately 2000 m3 of pressurized volume, with a mass of 24 tons, and can hold four times the standard atmospheric pressure. Moreover, the Whipple shield configuration is identical to the heavily protected sections of the ISS. The service module has a traditional cylindrical design and its role is to provide all the necessary utilities. Furthermore, the paper explains the assembly and welding method required to convert Orb2 into the fully assembled space station. I. Nomenclature LEO = low Earth orbit ISS = International Space Station PAS = payload adapter system MMOD = micrometeoroids and orbital debris FEA = finite element analysis g = gravitational force, 9:81m/s2 EBW = electron beam welding BEAM = Bigelow Expandable Activity Module ∗Staff Research Engineer, Portland, OR, 97201 USA, Member AIAA. -
The International Space Station Partners: Background and Current Status
The Space Congress® Proceedings 1998 (35th) Horizons Unlimited Apr 28th, 2:00 PM Paper Session I-B - The International Space Station Partners: Background and Current Status Daniel V. Jacobs Manager, Russian Integration, International Partners Office, International Space Station ogrPr am, NASA, JSC Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Jacobs, Daniel V., "Paper Session I-B - The International Space Station Partners: Background and Current Status" (1998). The Space Congress® Proceedings. 18. https://commons.erau.edu/space-congress-proceedings/proceedings-1998-35th/april-28-1998/18 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 INTERNATIONAL SPACE STATION: BACKGROUND AND CURRENT STATUS Daniel V. Jacobs Manager, Russian Integration, International Partners Office International Space Station Program, NASA Johnson Space Center Introduction The International Space Station, as the largest international civil program in history, features unprecedented technical, managerial, and international complexity. Seven interna- tional partners and participants encompassing fifteen countries are involved in the ISS. Each partner is designing, developing and will be operating separate pieces of hardware, to be inte- grated on-orbit into a single orbital station. Mission control centers, launch vehicles, astronauts/ cosmonauts, and support services will be provided by multiple partners, but functioning in a coordinated, integrated fashion. A number of major milestones have been accomplished to date, including the construction of major elements of flight hardware, the development of opera- tions and sustaining engineering centers, astronaut training, and seven Space Shuttle/Mir docking missions. -
International Space Station Overview
NASA Facts National Aeronautics and Space Administration Lyndon B. Johnson Space Center IS-1999-06-ISS022 Houston, Texas 77058 International Space Station June 1999 The International Space Station: An Overview The International Space Station is the largest and most complex international scientific project in history. The station represents a move of unprecedented scale off the home planet that began in 1998 with the launch of the first two components, the Unity and Zarya modules. Led by the United States, the International Space Station draws upon the scientific and technological resources of 16 nations: Canada, Japan, Russia, 11 nations of the European Space Agency and Brazil. More than four times as large as the Russian Mir space station, the completed International Space Station will have a mass of about 1 million pounds. It will measure about 360 feet across and 290 feet long, with almost an acre of solar panels to provide electrical power to six state-of-the-art laboratories. The first two station modules, the Russian-launched Zarya control module and U.S.-launched Unity connecting module, were assembled in orbit in late 1998. The station is in an orbit with an altitude of 250 statute miles with an inclination of 51.6 degrees. This orbit allows the station to be reached by the launch vehicles of all the international partners to provide a robust capability for the delivery of crews and supplies. The orbit also provides excellent Earth observations with coverage of 85 percent of the globe and over flight Artist's concept of the completed International Space Station of 95 percent of the population. -
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. -
Space Stations
Order Code IB93017 CRS Issue Brief for Congress Received through the CRS Web Space Stations Updated November 17, 2005 Marcia S. Smith Resources, Science, and Industry Division Congressional Research Service ˜ The Library of Congress CONTENTS SUMMARY MOST RECENT DEVELOPMENTS BACKGROUND AND ANALYSIS Introduction The Space Station Program: 1984-1993 Space Station Freedom 1993 Redesign — the Clinton Administration Restructuring The International Space Station (ISS): 1993-Present ISS Design, Cost, Schedule, and Lifetime September 1993-January 2001: The Clinton Administration 2001-Present: The George W. Bush Administration Reviews of NASA’s Cost Estimates and Adding Funds for ISS Congressional Action FY2005 FY2006 International Partners The Original Partners: Europe, Canada, and Japan Russia Risks and Benefits of Russian Participation ISS and U.S. Nonproliferation Objectives, Including the Iran Nonproliferation Act (INA) Key Issues For Congress Maintaining ISS Operations While the Shuttle Is Grounded Ensuring U.S. Astronaut Participation in Long-Duration Missions Impact of President Bush’s Vision for Space Exploration, Including a Potential Gap in U.S. Human Access to Space LEGISLATION IB93017 11-17-05 Space Stations SUMMARY Congress continues to debate NASA’s “Moon/Mars” Vision instead of the broadly- International Space Station (ISS), a perma- based program that was planned. nently occupied facility in Earth orbit where astronauts live and conduct research. Canada, Japan, and several European Congress appropriated approximately $35 countries became partners with NASA in billion for the program from FY1985-2005. building the space station in 1988; Russia The initial FY2006 ISS request was $2.180 joined in 1993. Except for money paid to billion: $1.857 billion for construction and Russia, there is no exchange of funds among operations and $324 million for research to be the partners. -
Evolvable Mars Campaign and Technology Development
National Aeronautics and Space Administration Evolvable Mars Campaign and Technology Development Jason Crusan Director, Advanced Exploration Systems Human Exploration & Operations Mission Directorate NASA Headquarters 27July 2015 2 3 Pioneering Space - Goals “Fifty years after the creation of NASA, our goal is no longer just a destination to reach. Our goal is the capacity for people to work and learn and operate and live safely beyond the Earth for extended periods of time, ultimately in ways that are more sustainable and even indefinite. And in fulfilling this task, we will not only extend humanity’s reach in space -- we will strengthen America’s leadership here on Earth.” - President Obama - April, 2010 4 NASA Strategic Plan Objective 1.1 Expand human presence into the solar system and to the surface of Mars to advance exploration, science, innovation, benefits to humanity, and international collaboration. 5 Strategic Principles for Sustainable Exploration • Implementable in the near-term with the buying power of current budgets and in the longer term with budgets commensurate with economic growth; • Exploration enables science and science enables exploration, leveraging robotic expertise for human exploration of the solar system • Application of high Technology Readiness Level (TRL) technologies for near term missions, while focusing sustained investments on technologies and capabilities to address challenges of future missions; • Near-term mission opportunities with a defined cadence of compelling and integrated human and robotic missions providing for an incremental buildup of capabilities for more complex missions over time; • Opportunities for U.S. commercial business to further enhance the experience and business base; • Multi-use, evolvable space infrastructure, minimizing unique major developments, with each mission leaving something behind to support subsequent missions; and • Substantial new international and commercial partnerships, leveraging the current International Space Station partnership while building new cooperative ventures.