How Does Spaceflight Affect the Human Body?
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The "Bug" Heard 'Round the World
ACM SIGSOFT SOFTWAREENGINEERING NOTES, Vol 6 No 5, October 1981 Page 3 THE "BUG" HEARD 'ROUND THE WORLD Discussion of the software problem which delayed the first Shuttle orbital flight JohnR. Garman Cn April 10, 1981, about 20 minutes prior to the scheduled launching of the first flight of America's Space Transportation System, astronauts and technicians attempted to initialize the software system which "backs-up" the quad-redundant primary software system ...... and could not. In fact, there was no possible way, it turns out, that the BFS (Backup Flight Control System) in the fifth onboard computer could have been initialized , Froperly with the PASS (Primary Avionics Software System) already executing in the other four computers. There was a "bug" - a very small, very improbable, very intricate, and very old mistake in the initialization logic of the PASS. It was the type of mistake that gives programmers and managers alike nightmares - and %heoreticians and analysts endless challenge. I% was the kind of mistake that "cannot happen" if one "follows all the rules" of good software design and implementation. It was the kind of mistake that can never be ruled out in the world of real systems development: a world involving hundreds of programmers and analysts, thousands of hours of testing and simulation, and millions of pages of design specifications, implementation schedules, and test plans and reports. Because in that world, software is in fact "soft" - in a large complex real time control system like the Shuttle's avionics system, software is pervasive and, in virtually every case, the last subsystem to stabilize. -
Space Launch System (Sls) Motors
Propulsion Products Catalog SPACE LAUNCH SYSTEM (SLS) MOTORS For NASA’s Space Launch System (SLS), Northrop Grumman manufactures the five-segment SLS heavy- lift boosters, the booster separation motors (BSM), and the Launch Abort System’s (LAS) launch abort motor and attitude control motor. The SLS five-segment booster is the largest solid rocket motor ever built for flight. The SLS booster shares some design heritage with flight-proven four-segment space shuttle reusable solid rocket motors (RSRM), but generates 20 percent greater average thrust and 24 percent greater total impulse. While space shuttle RSRM production has ended, sustained booster production for SLS helps provide cost savings and access to reliable material sources. Designed to push the spent RSRMs safely away from the space shuttle, Northrop Grumman BSMs were rigorously qualified for human space flight and successfully used on the last fifteen space shuttle missions. These same motors are a critical part of NASA’s SLS. Four BSMs are installed in the forward frustum of each five-segment booster and four are installed in the aft skirt, for a total of 16 BSMs per launch. The launch abort motor is an integral part of NASA’s LAS. The LAS is designed to safely pull the Orion crew module away from the SLS launch vehicle in the event of an emergency on the launch pad or during ascent. Northrop Grumman is on contract to Lockheed Martin to build the abort motor and attitude control motor—Lockheed is the prime contractor for building the Orion Multi-Purpose Crew Vehicle designed for use on NASA’s SLS. -
The SKYLON Spaceplane
The SKYLON Spaceplane Borg K.⇤ and Matula E.⇤ University of Colorado, Boulder, CO, 80309, USA This report outlines the major technical aspects of the SKYLON spaceplane as a final project for the ASEN 5053 class. The SKYLON spaceplane is designed as a single stage to orbit vehicle capable of lifting 15 mT to LEO from a 5.5 km runway and returning to land at the same location. It is powered by a unique engine design that combines an air- breathing and rocket mode into a single engine. This is achieved through the use of a novel lightweight heat exchanger that has been demonstrated on a reduced scale. The program has received funding from the UK government and ESA to build a full scale prototype of the engine as it’s next step. The project is technically feasible but will need to overcome some manufacturing issues and high start-up costs. This report is not intended for publication or commercial use. Nomenclature SSTO Single Stage To Orbit REL Reaction Engines Ltd UK United Kingdom LEO Low Earth Orbit SABRE Synergetic Air-Breathing Rocket Engine SOMA SKYLON Orbital Maneuvering Assembly HOTOL Horizontal Take-O↵and Landing NASP National Aerospace Program GT OW Gross Take-O↵Weight MECO Main Engine Cut-O↵ LACE Liquid Air Cooled Engine RCS Reaction Control System MLI Multi-Layer Insulation mT Tonne I. Introduction The SKYLON spaceplane is a single stage to orbit concept vehicle being developed by Reaction Engines Ltd in the United Kingdom. It is designed to take o↵and land on a runway delivering 15 mT of payload into LEO, in the current D-1 configuration. -
An Assessment of Aerocapture and Applications to Future Missions
Post-Exit Atmospheric Flight Cruise Approach An Assessment of Aerocapture and Applications to Future Missions February 13, 2016 National Aeronautics and Space Administration An Assessment of Aerocapture Jet Propulsion Laboratory California Institute of Technology Pasadena, California and Applications to Future Missions Jet Propulsion Laboratory, California Institute of Technology for Planetary Science Division Science Mission Directorate NASA Work Performed under the Planetary Science Program Support Task ©2016. All rights reserved. D-97058 February 13, 2016 Authors Thomas R. Spilker, Independent Consultant Mark Hofstadter Chester S. Borden, JPL/Caltech Jessie M. Kawata Mark Adler, JPL/Caltech Damon Landau Michelle M. Munk, LaRC Daniel T. Lyons Richard W. Powell, LaRC Kim R. Reh Robert D. Braun, GIT Randii R. Wessen Patricia M. Beauchamp, JPL/Caltech NASA Ames Research Center James A. Cutts, JPL/Caltech Parul Agrawal Paul F. Wercinski, ARC Helen H. Hwang and the A-Team Paul F. Wercinski NASA Langley Research Center F. McNeil Cheatwood A-Team Study Participants Jeffrey A. Herath Jet Propulsion Laboratory, Caltech Michelle M. Munk Mark Adler Richard W. Powell Nitin Arora Johnson Space Center Patricia M. Beauchamp Ronald R. Sostaric Chester S. Borden Independent Consultant James A. Cutts Thomas R. Spilker Gregory L. Davis Georgia Institute of Technology John O. Elliott Prof. Robert D. Braun – External Reviewer Jefferey L. Hall Engineering and Science Directorate JPL D-97058 Foreword Aerocapture has been proposed for several missions over the last couple of decades, and the technologies have matured over time. This study was initiated because the NASA Planetary Science Division (PSD) had not revisited Aerocapture technologies for about a decade and with the upcoming study to send a mission to Uranus/Neptune initiated by the PSD we needed to determine the status of the technologies and assess their readiness for such a mission. -
Magnetoshell Aerocapture: Advances Toward Concept Feasibility
Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly A thesis submitted in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics & Astronautics University of Washington 2018 Committee: Uri Shumlak, Chair Justin Little Program Authorized to Offer Degree: Aeronautics & Astronautics c Copyright 2018 Charles L. Kelly University of Washington Abstract Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly Chair of the Supervisory Committee: Professor Uri Shumlak Aeronautics & Astronautics Magnetoshell Aerocapture (MAC) is a novel technology that proposes to use drag on a dipole plasma in planetary atmospheres as an orbit insertion technique. It aims to augment the benefits of traditional aerocapture by trapping particles over a much larger area than physical structures can reach. This enables aerocapture at higher altitudes, greatly reducing the heat load and dynamic pressure on spacecraft surfaces. The technology is in its early stages of development, and has yet to demonstrate feasibility in an orbit-representative envi- ronment. The lack of a proof-of-concept stems mainly from the unavailability of large-scale, high-velocity test facilities that can accurately simulate the aerocapture environment. In this thesis, several avenues are identified that can bring MAC closer to a successful demonstration of concept feasibility. A custom orbit code that dynamically couples magnetoshell physics with trajectory prop- agation is developed and benchmarked. The code is used to simulate MAC maneuvers for a 60 ton payload at Mars and a 1 ton payload at Neptune, both proposed NASA mis- sions that are not possible with modern flight-ready technology. In both simulations, MAC successfully completes the maneuver and is shown to produce low dynamic pressures and continuously-variable drag characteristics. -
The Space Race Continues
The Space Race Continues The Evolution of Space Tourism from Novelty to Opportunity Matthew D. Melville, Vice President Shira Amrany, Consulting and Valuation Analyst HVS GLOBAL HOSPITALITY SERVICES 369 Willis Avenue Mineola, NY 11501 USA Tel: +1 516 248-8828 Fax: +1 516 742-3059 June 2009 NORTH AMERICA - Atlanta | Boston | Boulder | Chicago | Dallas | Denver | Mexico City | Miami | New York | Newport, RI | San Francisco | Toronto | Vancouver | Washington, D.C. | EUROPE - Athens | London | Madrid | Moscow | ASIA - 1 Beijing | Hong Kong | Mumbai | New Delhi | Shanghai | Singapore | SOUTH AMERICA - Buenos Aires | São Paulo | MIDDLE EAST - Dubai HVS Global Hospitality Services The Space Race Continues At a space business forum in June 2008, Dr. George C. Nield, Associate Administrator for Commercial Space Transportation at the Federal Aviation Administration (FAA), addressed the future of commercial space travel: “There is tangible work underway by a number of companies aiming for space, partly because of their dreams, but primarily because they are confident it can be done by the private sector and it can be done at a profit.” Indeed, private companies and entrepreneurs are currently aiming to make this dream a reality. While the current economic downturn will likely slow industry progress, space tourism, currently in its infancy, is poised to become a significant part of the hospitality industry. Unlike the space race of the 1950s and 1960s between the United States and the former Soviet Union, the current rivalry is not defined on a national level, but by a collection of first-mover entrepreneurs that are working to define the industry and position it for long- term profitability. -
Minotaur I User's Guide
This page left intentionally blank. Minotaur I User’s Guide Revision Summary TM-14025, Rev. D REVISION SUMMARY VERSION DOCUMENT DATE CHANGE PAGE 1.0 TM-14025 Mar 2002 Initial Release All 2.0 TM-14025A Oct 2004 Changes throughout. Major updates include All · Performance plots · Environments · Payload accommodations · Added 61 inch fairing option 3.0 TM-14025B Mar 2014 Extensively Revised All 3.1 TM-14025C Sep 2015 Updated to current Orbital ATK naming. All 3.2 TM-14025D Sep 2018 Branding update to Northrop Grumman. All 3.3 TM-14025D Sep 2020 Branding update. All Updated contact information. Release 3.3 September 2020 i Minotaur I User’s Guide Revision Summary TM-14025, Rev. D This page left intentionally blank. Release 3.3 September 2020 ii Minotaur I User’s Guide Preface TM-14025, Rev. D PREFACE This Minotaur I User's Guide is intended to familiarize potential space launch vehicle users with the Mino- taur I launch system, its capabilities and its associated services. All data provided herein is for reference purposes only and should not be used for mission specific analyses. Detailed analyses will be performed based on the requirements and characteristics of each specific mission. The launch services described herein are available for US Government sponsored missions via the United States Air Force (USAF) Space and Missile Systems Center (SMC), Advanced Systems and Development Directorate (SMC/AD), Rocket Systems Launch Program (SMC/ADSL). For technical information and additional copies of this User’s Guide, contact: Northrop Grumman -
Investigating Mars' Atmosphere Using the NOMAD Instrument on The
Investigating Mars’ atmosphere using the NOMAD instrument on the ExoMars Trace Gas Orbiter Supervision team: Dr Manish Patel, Dr Stephen Lewis, Dr Jonathon Mason External supervisor: N/A Lead contact: [email protected] Description: This project provides the opportunity to be directly involved in an active space mission and play a key role in the preparation and exploitation of results from a spaceflight instrument on the ESA ExoMars Trace Gas Orbiter mission, which is currently in orbit around Mars. The project will involve supporting work on: - Continued development of a radiative transfer model of the martian atmosphere in preparation for ExoMars - Characterisation of Flight Spare instrumentation and data interpretation from mid-cruise checkouts - Preparation of new techniques for retrieval of atmospheric species - Exploitation of data returned from the NOMAD-UVIS instrument This mission is aimed at furthering our understanding of the composition and dynamics of the martian environment, through the measurement of trace gases such as ozone and methane in the martian atmosphere from orbit. The project relates to the UVIS channel of the NOMAD instrument; UVIS is an optical spectrometer led by the Open University to measure solar radiation travelling through the martian atmosphere at UV and visible wavelengths, in order to detect and map the presence of ozone, dust and ice clouds in the atmosphere of Mars in unprecedented detail. This project will involve scope for a wide range of potential research from instrument testing through to exploitation of real spaceflight instrument data. The focus of the project is on the retrieval of ozone and aerosol abundance and properties from spectra that will be returned from the UVIS instrument. -
The Esa Exploration Programme – Exomars and Beyond
Lunar and Planetary Science XXXVI (2005) 2408.pdf THE ESA EXPLORATION PROGRAMME – EXOMARS AND BEYOND. G. Kminek1 and the Exploration Team, 1European Space Agency, D/HME, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands, [email protected]. Management and Organization: The countries Technology Development for Exploration: Two participating in the European Exploration Programme categories for exploration technology developments Aurora have recently confirmed and increased their have been identified: contribution. The ESA Council has later approved the Generic Exploration Technology: They have a Agency’s budgets for 2005, including the budget for long-term strategic value, both for robotic and human Aurora. These developments enable major industrial exploration missions. Planetary protection, habitable activities to continue in line with original plans. These systems, risk assessment for human missions to planets, include work on the ExoMars mission and the Mars grey and black water recycling as well as psychological Sample Return mission, in-orbit assembly, rendezvous support for the Concordia Antarctic Station, Facility and docking, habitation and life support systems plus a for Integrated Planetary Exploration Simulations are broad range of technology development work. examples of selected generic exploration technologies. The Aurora Exploration Programme has been inte- Mission Specific Technologies: Specifically devel- grated into the Human Spaceflight and Microgravity oped for the programme’s missions, and will eventually Directorate , which now forms the Human Spaceflight, be implemented after reaching a minimum technology Microgravity, and Exploration Directorate of ESA. readiness level. EVD, sealing and sealing monitoring Early Robotic Missions: Robotic mission have technology, containment technology, specific instru- been identified as necessary prerequisite before send- ment developments, sample handling and distribution ing human to Mars. -
Human Spaceflight Plans of Russia, China and India
Presentation to the ASEB Committee on NASA Technology Roadmaps Panel on Human Health and Surface Exploration June 1, 2011 by Marcia S. Smith Space and Technology Policy Group, LLC Russia Extensive experience in human spaceflight First animal in space (1957), first man in space (1961), first woman in space (1963), first spacewalk (1965), first space station (1971) Seven successful space stations (Salyut 1, 3, 4, 5, 6, 7 and Mir) before partnering in International Space Station (ISS) No people beyond low Earth orbit (LEO), however For earth orbit, continues to rely on Soyuz, first launched in 1967, but upgraded many times and is key to ISS operations Designed space shuttle, Buran, but launched only once in automated mode (no crew) in 1988 06-01-2011 2 Russia (2) Existing reliable launch vehicles Proton is largest: 21 tons to LEO; 5.5 tons to geostationary transfer orbit (GTO) Attempts to build Saturn V-equivalent in 1960s and 1970s failed (N1 failed four times in four attempts 1969-1972) Energiya booster in 1980s only flew twice (1987 with Polyus and 1988 with Buran). Abandoned for financial reasons. Was 100 tons to LEO; 18-20 tons to GTO; 32 tons to lunar trajectory. RD-170 engines for Energiya’s strap-ons live on today in other forms for Zenit, Atlas V, and Angara (under development) 06-01-2011 3 Russia (3) Robotic planetary space exploration mixed Excellent success at – Moon (Luna and Lunokhod series, plus Zond circumlunar flights) Venus (Venera series) Halley’s Comet (Vega 1 and 2—also Venus) Jinxed at Mars More than a dozen failures in 1960s - 1970s Partial success with Phobos 2 in 1988 (Phobos 1 failed) Mars 96 failed to leave Earth orbit Phobos-Grunt scheduled for later this year; designed as sample return from Phobos (includes Chinese orbiter) 06-01-2011 4 Russia (4) Grand statements over decades about sending people to the Moon and Mars, but never enough money to proceed. -
Human Spaceflight in Social Media: Promoting Space Exploration Through Twitter
Human Spaceflight in Social Media: Promoting Space Exploration Through Twitter Pierre J. Bertrand,1 Savannah L. Niles,2 and Dava J. Newman1,3 turn back now would be to deny our history, our capabilities,’’ said James Michener.1 The aerospace industry has successfully 1 Man-Vehicle Laboratory, Department of Aeronautics and Astro- commercialized Earth applications for space technologies, but nautics; 2Media Lab, Department of Media Arts and Sciences; and 3 human space exploration seems to lack support from both fi- Department of Engineering Systems, Massachusetts Institute of nancial and human public interest perspectives. Space agencies Technology, Cambridge, Massachusetts. no longer enjoy the political support and public enthusiasm that historically drove the human spaceflight programs. If one uses ABSTRACT constant year dollars, the $16B National Aeronautics and While space-based technologies for Earth applications are flourish- Space Administration (NASA) budget dedicated for human ing, space exploration activities suffer from a lack of public aware- spaceflight in the Apollo era has fallen to $7.9B in 2014, of ness as well as decreasing budgets. However, space exploration which 41% is dedicated to operations covering the Internati- benefits are numerous and include significant science, technological onal Space Station (ISS), the Space Launch System (SLS) and development, socioeconomic benefits, education, and leadership Orion, and commercial crew programs.2 The European Space contributions. Recent robotic exploration missions have -
Cosmos: a Spacetime Odyssey (2014) Episode Scripts Based On
Cosmos: A SpaceTime Odyssey (2014) Episode Scripts Based on Cosmos: A Personal Voyage by Carl Sagan, Ann Druyan & Steven Soter Directed by Brannon Braga, Bill Pope & Ann Druyan Presented by Neil deGrasse Tyson Composer(s) Alan Silvestri Country of origin United States Original language(s) English No. of episodes 13 (List of episodes) 1 - Standing Up in the Milky Way 2 - Some of the Things That Molecules Do 3 - When Knowledge Conquered Fear 4 - A Sky Full of Ghosts 5 - Hiding In The Light 6 - Deeper, Deeper, Deeper Still 7 - The Clean Room 8 - Sisters of the Sun 9 - The Lost Worlds of Planet Earth 10 - The Electric Boy 11 - The Immortals 12 - The World Set Free 13 - Unafraid Of The Dark 1 - Standing Up in the Milky Way The cosmos is all there is, or ever was, or ever will be. Come with me. A generation ago, the astronomer Carl Sagan stood here and launched hundreds of millions of us on a great adventure: the exploration of the universe revealed by science. It's time to get going again. We're about to begin a journey that will take us from the infinitesimal to the infinite, from the dawn of time to the distant future. We'll explore galaxies and suns and worlds, surf the gravity waves of space-time, encounter beings that live in fire and ice, explore the planets of stars that never die, discover atoms as massive as suns and universes smaller than atoms. Cosmos is also a story about us. It's the saga of how wandering bands of hunters and gatherers found their way to the stars, one adventure with many heroes.