Solar Warning Architecture for Manned Missions to Mars James S
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Near-Earth Asteroids Accessible to Human Exploration with High-Power Electric Propulsion
AAS 11-446 NEAR-EARTH ASTEROIDS ACCESSIBLE TO HUMAN EXPLORATION WITH HIGH-POWER ELECTRIC PROPULSION Damon Landau* and Nathan Strange† The diverse physical and orbital characteristics of near-Earth asteroids provide progressive stepping stones on a flexible path to Mars. Beginning with cislunar exploration capability, the variety of accessible asteroid targets steadily increas- es as technology is developed for eventual missions to Mars. Noting the poten- tial for solar electric propulsion to dramatically reduce launch mass for Mars ex- ploration, we apply this technology to expand the range of candidate asteroid missions. The variety of mission options offers flexibility to adapt to shifting exploration objectives and development schedules. A robust and efficient explo- ration program emerges where a potential mission is available once per year (on average) with technology levels that span cislunar to Mars-orbital capabilities. Examples range from a six-month mission that encounters a 10-m object with 65 kW to a two-year mission that reaches a 2-km asteroid with a 350-kW system. INTRODUCTION In the wake of the schedule and budgetary woes that led to the cancellation of the Constella- tion Moon program, the exploration of near-Earth asteroids (NEAs) has been promoted as a more realizable and affordable target to initiate deep space exploration with astronauts.1,2 Central to the utility of NEAs in a progressive exploration program is their efficacy to span a path as literal stepping stones between cislunar excursions and the eventual human -
AAS SFMC Manuscript Format Template
Proof-reading draft. Final version will be made available at http://dx.doi.org/10.2514/1.62412 PASSIVE SORTING OF ASTEROID MATERIAL USING SOLAR RADIATION PRESSURE D. García Yárnoz,* J. P. Sánchez Cuartielles,† and C. R. McInnes ‡ Understanding dust dynamics in the vicinity of asteroids is key for future science missions and, in the long-term, for asteroid exploitation. This paper ana- lyzes the feasibility of manipulating asteroid material by means of solar radia- tion pressure. A novel method is proposed for passively sorting material as a function of its grain size or density, where solar radiation pressure is used as a passive in-situ ‘mass spectrometer’. A simplified analysis shows that in prin- ciple this method allows an effective sorting of regolith material. This could have immediate applications for a sample return mission, and for industrial scale in-situ resource utilization to separate and concentrate regolith according to par- ticle size or composition. INTRODUCTION Asteroids are regarded as prime targets for space exploration missions. This interest is justi- fied as asteroids are among the least evolved bodies in the Solar System and can provide a better understanding of its formation from the solar nebula [1]. Under NASA’s flexible path plan [2], * PhD Researcher, Advanced Space Concepts Laboratory, Dept. of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow G1 1XQ, UK. † Research Fellow, Advanced Space Concepts Laboratory. ‡‡ Director, Advanced Space Concepts Laboratory. 1 asteroids have also become attractive targets to be visited by crewed missions, with the benefit of not requiring the capability to land in and take-off from a deep gravity well. -
The Next Steps for Environmental Control and Life Support Systems Development for Deep Space Exploration
48th International Conference on Environmental Systems ICES-2018-276 8-12 July 2018, Albuquerque, New Mexico The Next Steps for Environmental Control and Life Support Systems Development for Deep Space Exploration Mark Jernigan1 NASA Johnson Space Center, Houston, TX 77058 Robyn Gatens2 and Jitendra Joshi3 NASA Headquarters, Washington, D.C. 20546 and Jay Perry4 NASA Marshall Space Flight Center, Huntsville, AL 35812 Throughout the life of the International Space Station (ISS), NASA has developed, deliv- ered and operated a suite of progressively more capable environmental control and life support system (ECLSS) components and assemblies. These efforts have resulted in substan- tially reducing the supply chain necessary to sustain crews in flight and garnering invaluable lessons for sustained long term operations of the equipment. Currently, the ISS provides a unique platform for understanding the effects of the environment on the hardware. NASA’s strategy, already underway, is to evolve the ISS ECLSS into the Exploration ECLSS and perform a long-duration demonstration on ISS in preparation for deep space missions. This includes demonstrations of upgrades and/or new capabilities for waste management, atmos- phere revitalization, water recovery, and environmental monitoring. Within the Advanced Exploration Systems Program under the Next Space Technologies for Exploration Partner- ships (NextSTEP) model, NASA intends to revise the architecture developed for ISS to make the systems completely independent of the Earth supply chain for the duration of a deep space crewed mission by increasing robustness, including prospective system monitoring to anticipate failures, designing for maintenance, repair and refurbishment, reducing spare part count through use of common components, and grouping subsystems into modular pal- lets to minimize interfaces and reduce complexity. -
Report on Space Weather Observing Systems: Current Capabilities And
REPORT ON SPACE WEATHER OBSERVING SYSTEMS: CURRENT CAPABILITIES AND REQUIREMENTS FOR THE NEXT DECADE April 2013 Prepared by the Office of the Federal Coordinator for Meteorological Services and Supporting Research National Space Weather Program Council - Joint Action Group for Space Environmental Gap Analysis In response to a request by the Office of Science and Technology Policy Executive Office of the President NATIONAL SPACE WEATHER PROGRAM COUNCIL (NSWPC) MR. SAMUEL P. WILLIAMSON, Chairman MS. VICTORIA COX* Federal Coordinator for Meteorology Department of Transportation DR. JOHN HAYES* DR. RICHARD FISHER* Department of Commerce National Aeronautics and Space Administration DR. FRED LEWIS* DR. TIMOTHY KILLEEN* Department of Defense National Science Foundation MR. W. RANDALL BELL MS. MARY KICZA Department of Energy Department of Commerce Alternate MS. ROBIN FINEGAN* DR. HARROLD BELL Department of Homeland Security National Aeronautics and Space Administration Alternate MR. JAMES F. DEVINE* MR. DAMON WELLS* Department of the Interior Office of Science and Technology Policy Observer MR. KENNETH HODGKINS MS. GRACE HU Department of State Office of Management and Budget Observer MR. MICHAEL F. BONADONNA, Executive Secretary Office of the Federal Coordinator for Meteorological Services and Supporting Research *Denotes individuals who have rotated off the National Space Weather Program Council. This document was prepared by the Office of the Federal Coordinator for Meteorological Services and Supporting Research (OFCM) at the request of the Office of Science and Technology Policy (OSTP) in the Executive Office of the President. OSTP retains distribution control of the report. Do not copy or distribute this document outside of U.S. Government agencies without express permission from OSTP. -
Seeking a Human Spaceflight Program Worthy of a Great Nation
SEEKING A HUMAN SPACEFLIGHT PROGRAM WORTHY OF A GREAT NATION Review of U.S. HUMAN SPACEFLIGHT Plans Committee Review of U.S. Human Spaceflight Plans Committee 1 SEEKING A HUMAN SPACEFLIGHT PROGRAM WORTHY OF A GREAT NATION 2 Review of U.S. Human Spaceflight Plans Committee SEEKING A HUMAN SPACEFLIGHT PROGRAM WORTHY OF A GREAT NATION “We choose...to do [these] things, not because they are easy, but because they are hard...” John F. Kennedy September 12, 1962 Review of U.S. Human Spaceflight Plans Committee 3 SEEKING A HUMAN SPACEFLIGHT PROGRAM WORTHY OF A GREAT NATION Table of Contents Preface .......................... ...................................................................................................................................... 7 Executive Summary ..... ...................................................................................................................................... 9 Chapter 1.0 Introduction ............................................................................................................................... 19 Chapter 2.0 U.S. Human Spaceflight: Historical Review ............................................................................ 27 Chapter 3.0 Goals and Future Destinations for Exploration ........................................................................ 33 3.1 Goals for Exploration ............................................................................................................... 33 3.2 Overview of Destinations and Approach ................................................................................. -
Analysis on Plasma Sheath Formation and Its Effects on Radio Communications
Analysis on Plasma Sheath Formation and its Effects on Radio Communications a project presented to The Faculty of the Department of Aerospace Engineering San José State University in partial fulfillment of the requirements for the degree Master of Science in Aerospace Engineering by Jared Delatorre Wakefield Sagaga May 2018 approved by Dr. Nikos Mourtos Faculty Advisor Table of Contents Chapter 1. Literature Review ................................................................................................. 3 1.0 Project Objective ................................................................................................................... 3 1.1 Introduction .......................................................................................................................... 3 1.2 Background ............................................................................................................................ 6 1.3 Methodology ........................................................................................................................10 Chapter 2. Analysis .............................................................................................................. 12 2.0 Analytical ..............................................................................................................................12 2.0.1 Euler Equations .........................................................................................................13 2.0.2 Navier-Stokes Equations ...........................................................................................14 -
Augustine Report”
Joint ESPI-DGAP-FRS-IFRI-SWP-ISPL Policy Memorandum Europe’s Reaction to the “Augustine Report” October 2009 1. Introduction The Summary Report of the Review of U.S. Human Space Flight Plans Committee, (“Augustine Report”), released in mid-September, 1 has received considerable attention in the space policy community and in public debate. Its findings directly impact U.S. partnership with Europe. Therefore, Europe must be prepared to respond to any possible consequences. This Joint Memorandum by European think tanks aims to analyse the context and content of the Augustine Report, evaluate the echo it received and sketch a suitable way forward for Europe in reaction to any implementation of the Report’s findings. 2. The Augustine Report and its political context In May 2009, the White House had charged a committee of high ranking experts, headed by former Lockheed Martin CEO Norman Augustine, to assess U.S. human spaceflight plans and to generate appropriate options. The so-called Augustine Report is a summary to be followed by the Committee’s final report, which is not yet available. The review is part of a broader political effort to evaluate the current situation of U.S. space plans, with other assessments going on in the field of security. This includes an interagency effort led by U. S. NSC to release a new Quadrennial Defense Review (QDR), a new Nuclear Posture Review and a new National Space Policy in 2010. The White House is also looking at a reform of the ITAR rules. 1 Summary Report of the Review of U.S. -
26.03.2021R. Średnioterminowe Scenariusze Rozwoju Przemysłu
1 ŚREDNIOTERMINOWE SCENARIUSZE ROZWOJU PRZEMYSŁU KOSMICZNEGO W POLSCE GRUDZIEŃ 2020 2 3 1. WPROWADZENIE Trzecia dekada XXI wieku zapowiada się wyjątkowo interesująco. Z pewnością globalny sektor kosmiczny zmieni swój kształt i zasięg w porównaniu z dwiema pierwszymi dekadami tego stulecia. Ponadto to właśnie w trakcie lat dwudziestych człowiek najpewniej powróci na Księżyc, tym razem na stałe i w „międzynarodowym składzie”. Dojdzie także do serii ambitnych misji marsjańskich, których zwieńczeniem będzie sprowadzenie próbek materii z Czerwonej Planety (około 2031 roku). Wiele wydarzy się również w bezpośrednim otoczeniu Ziemi: pojawią się megakonstelacje poszerzające możliwości telekomunikacyjne. Nowe państwa dołączą do grona operatorów własnych satelitów lub nawet systemów satelitarnych. Prywatne firmy oraz państwa będą realizować niezależne, ambitne plany, w tym rozwoju nowych rakiet, systemów obserwacji Ziemi, a nawet eksploracji przestrzeni BEO (Beyond Earth Orbit), w szczególności na Księżycu i wokół niego. Oczywiście jest możliwe, że wiele z tych planów nie zostanie zrealizowanych w zakładanym czasie. Pandemia koronawirusa SARS-CoV-2 (COVID-19), która „rozlała się” po całym świecie w 2020 roku, według wstępnych prognoz może wpłynąć na wysokość dostępnych funduszy. W konsekwencji istnieje poważne ryzyko opóźnienia niektórych z dużych programów kosmicznych, w tym tych eksploracyjnych. Czy w Polsce istnieje już świadomość tej zmiany branży kosmicznej? Jakie są możliwości wsparcia budowy innowacyjnych rozwiązań, które mogą być ważne z perspektywy Polski lub Europy? Co jest potrzebne, by krajowy sektor kosmiczny mógł wkroczyć na ścieżkę szybkiego rozwoju? W niniejszym studium pt. „Średniookresowe scenariusze rozwoju przemysłu kosmicznego w Polsce” zaprezentowane zostały wnioski i rekomendacje dotyczące możliwych kierunków rozwoju branży kosmicznej w Polsce. Zakres studium to 10 najbliższych lat, czyli do 2031 roku. -
Synergies of Robotic Asteroid Redirection Technologies and Human Space Exploration
Synergies of Robotic Asteroid Redirection Technologies and Human Space Exploration John R. Brophy , Jet Propulsion Laboratory, Caltech Louis Friedman ,Executive Director Emeritus, The Planetary Society Nathan J. Strange, Jet Propulsion Laboratory, Caltech Thomas A. Prince . Director, Keck Institute for Space Studies, Caltech Damon Landau, Jet Propulsion Laboratory, Caltech Thomas Jones . Florida Institute for Human and Machine Cognition Russell Schweickart , B612 Foundation Chris Lewicki , Planetary Resources, Inc. Martin Elvis , Harvard-Smithsonian Center for Astrophysics David Manzella ,NASA Glenn Research Center, USA 10/2/ 2014 Louis Friedman IAC 2014 1 3 Year Study (2011-2014) • Initial Study Results – ARM uniquely enables human exploration of a celestial body beyond the Moon by 2025 – Spacecraft and Mission are feasible within current program – Requires and develops Solar Electric Propulsion • Follow-on Study Results – SEP provides significant advantages for humans to Mars – A series of increasingly deep-space missions is enabled with asteroid redirection technology – Asteroid resources can be exploited for human space flight – Strong synergy exists with commercial and planetary defense objectives 10/2/ 2014 Louis Friedman IAC 2014 2 The ARM Spacecraft Capture a Small Asteroid Pick up a Boulder 10/2/ 2014 Louis Friedman IAC 2014 3 Asteroid Redirect Mission Design (NOTIONAL) 5) Asteroid Operations: rendezvous, characterize, deploy capture mechanism, capture, and despin (60 days) Asteroid Orbit 4) SEP low-thrust 6) SEP redirect cruise -
The First Human Asteroid Mission: Target Selection and Conceptual Mission Design
The First Human Asteroid Mission: Target Selection and Conceptual Mission Design Daniel Zimmerman,∗ Sam Wagner,∗ and Bong Wiey Asteroid Deflection Research Center - Iowa State University, Ames, IA 50011-2271 President Obama has recently declared that NASA will pursue a crewed mission to an asteroid by 2025. This paper identifies the optimum target candidates of near-Earth objects (NEOs) for a first crewed mission between 2018 and 2030. Target asteroids in the NEO database with orbital elements that meet predetermined requirements are analyzed for mission design. System architectures are then proposed to meet the require- ments for five designated NEO candidates. Additional technology which can be applied to crewed NEO mis- sions in the future is also discussed, and a previous NEO target selection study is analyzed. Although some development of heavy launch vehicles is still required for the first NEO mission, design examples show that a first mission can be achieved by 2025. The Ares V and the Orion CEV are used as the baseline system architecture for this study. Nomenclature a Semi-major Axis (AU) AU Astronomical Unit BOM Burnout Mass CEV Crew Exploration Vehicle e Eccentricity EDS Earth Departure Stage EOR Earth Orbit Rendezvous H Absolute Magnitude i Inclination (deg) Isp Specific Impulse (s) ISS International Space Station JPL Jet Propulsion Laboratory LEO Low-Earth Orbit LH2 Liquid Hydrogen LOX Liquid Oxygen MWe Megawatt Electrical MT Metric Ton NASA National Aeronautics and Space Administration NEO Near-Earth Object OT V Orbital Transfer Vehicle RSRM Reusable Solid Rocket Motor SSME Space Shuttle Main Engine T LI Trans Lunar Injection V ASIMR Variable Specific Impulse Magnetoplasma Rocket ∆V Velocity Change (km/s) ∗Graduate Research Assistant, Dept. -
Institutional Path Dependence in NASA's
Institutional path dependence in NASA’s human spaceflight program: a case study of technological evolution and persistence by Trevor W. Waddell MPP Essay Submitted to Oregon State University In partial fulfillment of the requirements for the degree of Master of Public Policy Presented May 21, 2013 Commencement June 17, 2013 Master of Public Policy essay of Trevor W. Waddell presented on May 21, 2013. APPROVED: _________________________________________________________________ Denise Lach, representing Sociology _________________________________________________________________ Jacob Hamblin, representing History of Science _________________________________________________________________ Jack Higginbotham, representing College of Science, Space Programs _________________________________________________________________ Trevor Waddell, Author 2 3 Table of Contents 1. Introduction ................................................................................................................................ 7 2. Background ................................................................................................................................. 8 2.1. Overview of NASA and the U.S. Human Spaceflight Program ........................................... 8 2.2. Case Study History .............................................................................................................. 11 2.2.1 Vision for Space Exploration (VSE) ........................................................................ 11 2.2.2 Project Constellation ............................................................................................... -
10. Geospace Resource
The Sun and geospace Resource GS1 K. Endo/Nikkei Science BAS The aurora over the BAS Halley Research Station. Inset: Artist’s impression of the Sun and geospace (not to scale) illustrating how particles flowing radially from the Sun are deflected by the Earth’s magnetic field which forms a cavity in the particle stream, known as the magnetosphere. Solar wind – magnetosphere interaction Resource GS2 An illustration of the inter- action between the solar wind and magnetosphere. Solar wind streamlines are deflected by a shock wave to flow around the magnetosphere in a turbulent layer known as the magnetosheath. Some solar wind plasma leaks inside the magnetosphere. In the magnetosphere particles are guided in spiral helical trajectories along magnetic field lines. Some of these precipitate into the atmosphere to create the aurora. SUN BAS The aurora over Antarctica Resource GS3 Professor L.A. Frank (University of Iowa) A satellite view of Antarctica showing the aurora encircling it The effects of space weather on human activity Resource GS4 Effects on satellites radiation belts. Similarly, the continuous the Hubble Space Telescope. These boosts Satellites often operate in the space bombardment by atoms in the thin upper again add to costs. environment for many years. As a result, atmosphere can alter orbits and wear they can sustain long-term exposure surfaces away. Some materials become Effects on power systems effects in addition to special ‘space storm’ brittle from long-term exposure to solar Electric power systems on the ground problems. Depending upon their orbit, ultraviolet light above the protective can be affected by the enhanced satellite electronic components, solar absorbing atmosphere of Earth.