Phobos First: a Mission to Settle Mars
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International Space Exploration Strategy Group International Space Exploration
INTERNATIONAL SPACE EXPLORATION STRATEGY GROUP INTERNATIONAL SPACE EXPLORATION. STRATEGY GROUP ADVANCING THE EXPLORATION FRONTIER For the last forty years, human In recent years multiple reports define exploration in the coming space exploration has made have recommended international decades. significant progress through partners come together for The group will bring together the international collaboration. The strategic planning activities. interests of all human spaceflight Apollo-Soyuz Test Project and However, many national partners, rather than national Shuttle-Mir Programs marked government planning activities interests subject to changing the end of the Space Race, are severely limited in their political influences. and advanced long duration consideration of international This project provides a unique spaceflight. The International partners. Furthermore, opportunity for current and Space Station (ISS) is now in its government and industry recent graduate student second decade as a continuously planners may not have access researchers to collaborate with occupied human outpost in Low- to the latest technologies being others from around the world. Earth Orbit (LEO). While we developed at leading research Most importantly, participants expect productive utilization of institutions around the world. will have the opportunity to ISS through at least 2020, there We believe an international influence the government and is currently no internationally graduate student working group industry decision makers that recognized program for human is well-suited to generate and define future human exploration exploration beyond LEO. communicate the ideas that will strategy. 3 INTERNATIONAL SPACE EXPLORATION. STRATEGY GROUP INTERNATIONAL SPACE EXPLORATION. STRATEGY GROUP LEADERSHIP Edward Crawley is President of the Skolkovo Institute of Science and Technology (Skoltech). -
Of 13 Human Mars Mission Design – the Ultimate Systems Challenge
Human Mars Mission Design – The Ultimate Systems Challenge John F. Connolly a, B. Kent Joostenb, Bret Drakec, Steve Hoffmanc, Tara Polsgroved, Michelle Ruckera, Alida Andrewsc, Nehemiah Williamsa a NASA Johnson Space Center, 2101 NASA Parkway, Houston, Texas 77058, john.connolly- [email protected], [email protected], [email protected] b Consultant,2383 York Harbour Ct., League City, TX 77573, [email protected] c The Aerospace Corporation, 2310 E El Segundo Blvd, El Segundo, California 90245, [email protected], [email protected], [email protected] d NASA Marshall Space Flight Center, Redstone Arsenal, Huntsville, Alabama 35812, [email protected] Abstract A human mission to Mars will occur at some time in the coming decades. When it does, it will be the end result of a complex network of interconnected design choices, systems analyses, technical optimizations, and non-technical compromises. This mission will extend the technologies, engineering design, and systems analyses to new limits, and may very well be the most complex undertaking in human history. It can be illustrated as a large menu, or as a large decision tree. Whatever the visualization tool, there are numerous design decisions required to assemble a human Mars mission, and many of these interconnect with one another. This paper examines these many decisions and further details a number of choices that are highly interwoven throughout the mission design. The large quantity of variables and their interconnectedness results in a highly complex systems challenge, and the paper illustrates how a change in one variable results in ripples (sometimes unintended) throughout many other facets of the design. -
Isolated and Confined Environments
17 Isolated and Confined Environments Carole Tafforin Ethospace, Toulouse, France Characteristics of space analogue environments with regard to human per- formance concern the crew adaptation in a socio-psychological context and in a temporal dynamics. Isolation, confinement and time are major features on Earth to reproduce an extra-terrestrial environment for manned mission simulations. In the current space missions (low Earth orbit, LEO) and in the perspective of interplanetary missions (near-Earth asteroid, Moon, Mars), men and women will have to adapt to social constraints (crew size, multinationality, mixed-gender) and spatial restrictions (volume, multi-chambers, life-support) on short-term, medium-term and long-term durations. The crewmembers also will have to perform intra-vehicular activities (IVA)and extra-vehicular activ- ities (EVA). For training, preventing and optimizing such tasks, simulations of living and working together in isolated and confined environments, and simulations of operating with a space suit on geological surfaces are the new requirements. During the two decades (1991–2011), space simulators (confinement) and analogue settings (isolation) were adequately developed on Earth with the ultimate goal of walking on Mars. Time periods extended up to 500 days. Space analogue environments are located worldwide (Canada, United States, Russia, Europe, Antarctica and Arctic). Mission durations in space analogue environments cover days, weeks and years. Isolation and confinement facilities implemented for such simulations are listed in Table 17.1. Over a 7-day duration, the Canadian Astronaut Program Space Unit Life Simulation (CAPSULS) was an Earth-based initiative that simulated a typical space shuttle or space station mission [1]. CAPSULS provided the Canadian astronaut participants with space mission training. -
Planetary Report Report
The PLANETARYPLANETARY REPORT REPORT Volume XXIX Number 1 January/February 2009 Beyond The Moon From The Editor he Internet has transformed the way science is On the Cover: Tdone—even in the realm of “rocket science”— The United States has the opportunity to unify and inspire the and now anyone can make a real contribution, as world’s spacefaring nations to create a future brightened by long as you have the will to give your best. new goals, such as the human exploration of Mars and near- In this issue, you’ll read about a group of amateurs Earth asteroids. Inset: American astronaut Peggy A. Whitson who are helping professional researchers explore and Russian cosmonaut Yuri I. Malenchenko try out training Mars online, encouraged by Mars Exploration versions of Russian Orlan spacesuits. Background: The High Rovers Project Scientist Steve Squyres and Plane- Resolution Camera on Mars Express took this snapshot of tary Society President Jim Bell (who is also head Candor Chasma, a valley in the northern part of Valles of the rovers’ Pancam team.) Marineris, on July 6, 2006. Images: Gagarin Cosmonaut Training This new Internet-enabled fun is not the first, Center. Background: ESA nor will it be the only, way people can participate in planetary exploration. The Planetary Society has been encouraging our members to contribute Background: their minds and energy to science since 1984, A dust storm blurs the sky above a volcanic caldera in this image when the Pallas Project helped to determine the taken by the Mars Color Imager on Mars Reconnaissance Orbiter shape of a main-belt asteroid. -
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur To cite this version: Alex Soumbatov-Gur. Phobos, Deimos: Formation and Evolution. [Research Report] Karpov institute of physical chemistry. 2019. hal-02147461 HAL Id: hal-02147461 https://hal.archives-ouvertes.fr/hal-02147461 Submitted on 4 Jun 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur The moons are confirmed to be ejected parts of Mars’ crust. After explosive throwing out as cone-like rocks they plastically evolved with density decays and materials transformations. Their expansion evolutions were accompanied by global ruptures and small scale rock ejections with concurrent crater formations. The scenario reconciles orbital and physical parameters of the moons. It coherently explains dozens of their properties including spectra, appearances, size differences, crater locations, fracture symmetries, orbits, evolution trends, geologic activity, Phobos’ grooves, mechanism of their origin, etc. The ejective approach is also discussed in the context of observational data on near-Earth asteroids, main belt asteroids Steins, Vesta, and Mars. The approach incorporates known fission mechanism of formation of miniature asteroids, logically accounts for its outliers, and naturally explains formations of small celestial bodies of various sizes. -
The Mystery of Methane on Mars and Titan
The Mystery of Methane on Mars & Titan By Sushil K. Atreya MARS has long been thought of as a possible abode of life. The discovery of methane in its atmosphere has rekindled those visions. The visible face of Mars looks nearly static, apart from a few wispy clouds (white). But the methane hints at a beehive of biological or geochemical activity underground. Of all the planets in the solar system other than Earth, own way, revealing either that we are not alone in the universe Mars has arguably the greatest potential for life, either extinct or that both Mars and Titan harbor large underground bodies or extant. It resembles Earth in so many ways: its formation of water together with unexpected levels of geochemical activ- process, its early climate history, its reservoirs of water, its vol- ity. Understanding the origin and fate of methane on these bod- canoes and other geologic processes. Microorganisms would fit ies will provide crucial clues to the processes that shape the right in. Another planetary body, Saturn’s largest moon Titan, formation, evolution and habitability of terrestrial worlds in also routinely comes up in discussions of extraterrestrial biology. this solar system and possibly in others. In its primordial past, Titan possessed conditions conducive to Methane (CH4) is abundant on the giant planets—Jupiter, the formation of molecular precursors of life, and some scientists Saturn, Uranus and Neptune—where it was the product of chem- believe it may have been alive then and might even be alive now. ical processing of primordial solar nebula material. On Earth, To add intrigue to these possibilities, astronomers studying though, methane is special. -
A Future Mars Environment for Science and Exploration
Planetary Science Vision 2050 Workshop 2017 (LPI Contrib. No. 1989) 8250.pdf A FUTURE MARS ENVIRONMENT FOR SCIENCE AND EXPLORATION. J. L. Green1, J. Hol- lingsworth2, D. Brain3, V. Airapetian4, A. Glocer4, A. Pulkkinen4, C. Dong5 and R. Bamford6 (1NASA HQ, 2ARC, 3U of Colorado, 4GSFC, 5Princeton University, 6Rutherford Appleton Laboratory) Introduction: Today, Mars is an arid and cold world of existing simulation tools that reproduce the physics with a very thin atmosphere that has significant frozen of the processes that model today’s Martian climate. A and underground water resources. The thin atmosphere series of simulations can be used to assess how best to both prevents liquid water from residing permanently largely stop the solar wind stripping of the Martian on its surface and makes it difficult to land missions atmosphere and allow the atmosphere to come to a new since it is not thick enough to completely facilitate a equilibrium. soft landing. In its past, under the influence of a signif- Models hosted at the Coordinated Community icant greenhouse effect, Mars may have had a signifi- Modeling Center (CCMC) are used to simulate a mag- cant water ocean covering perhaps 30% of the northern netic shield, and an artificial magnetosphere, for Mars hemisphere. When Mars lost its protective magneto- by generating a magnetic dipole field at the Mars L1 sphere, three or more billion years ago, the solar wind Lagrange point within an average solar wind environ- was allowed to directly ravish its atmosphere.[1] The ment. The magnetic field will be increased until the lack of a magnetic field, its relatively small mass, and resulting magnetotail of the artificial magnetosphere its atmospheric photochemistry, all would have con- encompasses the entire planet as shown in Figure 1. -
Mars Scenario-Based Visioning: Logisitical Optimization of Transportation Architectures
MARS SCENARIO-BASED VISIONING: LOGISITICAL OPTIMIZATION OF TRANSPORTATION ARCHITECTURES GEORGIA INSTITUTE OF TECHNOLOGY Contributors: Ashraf Charania Kris Cowart Brad St. Germain Tadashi Sakai Roberto Salinas Kirk Sorensen Jeffrey Tooley Shannan Wilson Advisor: Dr. John R. Olds Assistant Professor, School of Aerospace Engineering Director, Space Systems Design Lab (SSDL) Georgia Institute of Technology ABSTRACT The purpose of this conceptual design investigation is to examine transportation forecasts for future human missions to Mars. Scenario-Based Visioning is used to generate possible future demand projections. These scenarios are then coupled with availability, cost, and capacity parameters for indigenously designed Mars Transfer Vehicles (solar electric, nuclear thermal, and chemical propulsion types) and Earth-to-Orbit launch vehicles (current, future, and indigenous) to provide a cost-conscious dual-phase launch manifest to meet such future demand. A simulator named M-SAT (Mars Scenario Analysis Tool) is developed using this method. This simulation is used to examine three specific transportation scenarios to Mars: a limited "flags and footprints" mission, a more ambitious scientific expedition similar to an expanded version of the Design Reference Mission from NASA, and a long-term colonization scenario. Initial results from the simulation indicate that chemical propulsion systems might be the architecture of choice for all three scenarios. With this mind, "what if" analyses were performed which indicated that if nuclear production costs were reduced by 30% for the colonization scenario, then the nuclear architecture would have a lower life cycle cost than the chemical. Results indicate that the most cost-effective solution to the Mars transportation problem is to plan for segmented development, this involves development of one vehicle at one opportunity and derivatives of that vehicle at subsequent opportunities. -
Design of a Human Settlement on Mars Using In-Situ Resources
46th International Conference on Environmental Systems ICES-2016-151 10-14 July 2016, Vienna, Austria Design of a Human Settlement on Mars Using In-Situ Resources Marlies Arnhof1 Vienna University of Technology, Vienna, 1040, Austria Mars provides plenty of raw materials needed to establish a lasting, self-sufficient human colony on its surface. Due to the planet's vast distance from Earth, it is neither possible nor economically reasonable to provide permanent, interplanetary supply. In-situ resource utilization (ISRU) will be necessary to keep the Earth launch burden and mission costs as low as possible, and to provide – apart from propellant and life support – a variety of construction material. However, to include outposts on other planets into the scope of human spaceflight also opens up new psychological and sociological challenges. Crews will live in extreme environments under isolated and confined conditions for much longer periods of time than ever before. Therefore, the design of a Mars habitat requires most careful consideration of physiological as well as psychosocial conditions of living in space. In this design for a Martian settlement, the author proposes that – following preliminary automated exploration – a basic surface base brought from Earth would be set up. Bags of unprocessed Martian regolith would be used to provide additional shielding for the habitat. Once the viability of the base and its production facilities are secured, the settlement would be expanded, using planetary resources. Martian concrete – processed regolith with a polymeric binder – would be used as main in-situ construction material. To provide optimum living and working conditions, the base would respond to the environment and the residents' number and needs, thereby evolving and growing continuously. -
An Impacting Descent Probe for Europa and the Other Galilean Moons of Jupiter
An Impacting Descent Probe for Europa and the other Galilean Moons of Jupiter P. Wurz1,*, D. Lasi1, N. Thomas1, D. Piazza1, A. Galli1, M. Jutzi1, S. Barabash2, M. Wieser2, W. Magnes3, H. Lammer3, U. Auster4, L.I. Gurvits5,6, and W. Hajdas7 1) Physikalisches Institut, University of Bern, Bern, Switzerland, 2) Swedish Institute of Space Physics, Kiruna, Sweden, 3) Space Research Institute, Austrian Academy of Sciences, Graz, Austria, 4) Institut f. Geophysik u. Extraterrestrische Physik, Technische Universität, Braunschweig, Germany, 5) Joint Institute for VLBI ERIC, Dwingelo, The Netherlands, 6) Department of Astrodynamics and Space Missions, Delft University of Technology, The Netherlands 7) Paul Scherrer Institute, Villigen, Switzerland. *) Corresponding author, [email protected], Tel.: +41 31 631 44 26, FAX: +41 31 631 44 05 1 Abstract We present a study of an impacting descent probe that increases the science return of spacecraft orbiting or passing an atmosphere-less planetary bodies of the solar system, such as the Galilean moons of Jupiter. The descent probe is a carry-on small spacecraft (< 100 kg), to be deployed by the mother spacecraft, that brings itself onto a collisional trajectory with the targeted planetary body in a simple manner. A possible science payload includes instruments for surface imaging, characterisation of the neutral exosphere, and magnetic field and plasma measurement near the target body down to very low-altitudes (~1 km), during the probe’s fast (~km/s) descent to the surface until impact. The science goals and the concept of operation are discussed with particular reference to Europa, including options for flying through water plumes and after-impact retrieval of very-low altitude science data. -
Marathon 2,500 Years Edited by Christopher Carey & Michael Edwards
MARATHON 2,500 YEARS EDITED BY CHRISTOPHER CAREY & MICHAEL EDWARDS INSTITUTE OF CLASSICAL STUDIES SCHOOL OF ADVANCED STUDY UNIVERSITY OF LONDON MARATHON – 2,500 YEARS BULLETIN OF THE INSTITUTE OF CLASSICAL STUDIES SUPPLEMENT 124 DIRECTOR & GENERAL EDITOR: JOHN NORTH DIRECTOR OF PUBLICATIONS: RICHARD SIMPSON MARATHON – 2,500 YEARS PROCEEDINGS OF THE MARATHON CONFERENCE 2010 EDITED BY CHRISTOPHER CAREY & MICHAEL EDWARDS INSTITUTE OF CLASSICAL STUDIES SCHOOL OF ADVANCED STUDY UNIVERSITY OF LONDON 2013 The cover image shows Persian warriors at Ishtar Gate, from before the fourth century BC. Pergamon Museum/Vorderasiatisches Museum, Berlin. Photo Mohammed Shamma (2003). Used under CC‐BY terms. All rights reserved. This PDF edition published in 2019 First published in print in 2013 This book is published under a Creative Commons Attribution-NonCommercial- NoDerivatives (CC-BY-NC-ND 4.0) license. More information regarding CC licenses is available at http://creativecommons.org/licenses/ Available to download free at http://www.humanities-digital-library.org ISBN: 978-1-905670-81-9 (2019 PDF edition) DOI: 10.14296/1019.9781905670819 ISBN: 978-1-905670-52-9 (2013 paperback edition) ©2013 Institute of Classical Studies, University of London The right of contributors to be identified as the authors of the work published here has been asserted by them in accordance with the Copyright, Designs and Patents Act 1988. Designed and typeset at the Institute of Classical Studies TABLE OF CONTENTS Introductory note 1 P. J. Rhodes The battle of Marathon and modern scholarship 3 Christopher Pelling Herodotus’ Marathon 23 Peter Krentz Marathon and the development of the exclusive hoplite phalanx 35 Andrej Petrovic The battle of Marathon in pre-Herodotean sources: on Marathon verse-inscriptions (IG I3 503/504; Seg Lvi 430) 45 V. -
Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft
Mars, Phobos, and Deimos Sample Return Enabled by ARRM Alternative Trade Study Spacecraft Jacob A. Englander,∗ Matthew A. Vavrina,† Bo Naasz ,‡ Raymond G. Merill,MinQu§ ¶ The Asteroid Robotic Redirect Mission (ARRM) has been the topic of many mission design studies since 2011.1 The reference ARRM spacecraft uses a powerful solar electric propulsion (SEP) system and a bag device to capture a small asteroid from an Earth-like orbit and redirect it to a distant retrograde orbit (DRO) around the moon. The ARRM Option B spacecraft uses the same propulsion system and multi-Degree of Freedom (DoF) manipulators device to retrieve a very large sample (thousands of kilograms) from a 100+ meter diameter farther-away Near Earth Asteroid (NEA). This study will demonstrate that the ARRM Option B spacecraft design can also be used to return samples from Mars and its moons - either by acquiring a large rock from the surface of Phobos or Deimos, and/or by rendezvousing with a sample-return spacecraft launched from the surface of Mars. I. Introduction The Asteroid Robotic Redirect Mission (ARRM) Option A concept, first introduced in 2011,1 is a mission design to capture and return a small near-Earth asteroid (NEA) to cislunar space. The ARRM Option B concept is a similar spacecraft, but designed to return a very large sample from a more difficult to reach NEA.2 In this work we show that the spacecraft designed for ARRM Option B is also well-suited to sample return from Mars and its moons. This work presents low-thrust interplanetary trajectories from cislunar space to Mars and back, including descent from the Martian sphere of influence (SOI) to the desired orbit altitude and ascent to the SOI after the sample retrieval is complete.