Planning a Mission to the Lunar South Pole
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The Surrender Software
Scientific image rendering for space scenes with the SurRender software Scientific image rendering for space scenes with the SurRender software R. Brochard, J. Lebreton*, C. Robin, K. Kanani, G. Jonniaux, A. Masson, N. Despré, A. Berjaoui Airbus Defence and Space, 31 rue des Cosmonautes, 31402 Toulouse Cedex, France [email protected] *Corresponding Author Abstract The autonomy of spacecrafts can advantageously be enhanced by vision-based navigation (VBN) techniques. Applications range from manoeuvers around Solar System objects and landing on planetary surfaces, to in -orbit servicing or space debris removal, and even ground imaging. The development and validation of VBN algorithms for space exploration missions relies on the availability of physically accurate relevant images. Yet archival data from past missions can rarely serve this purpose and acquiring new data is often costly. Airbus has developed the image rendering software SurRender, which addresses the specific challenges of realistic image simulation with high level of representativeness for space scenes. In this paper we introduce the software SurRender and how its unique capabilities have proved successful for a variety of applications. Images are rendered by raytracing, which implements the physical principles of geometrical light propagation. Images are rendered in physical units using a macroscopic instrument model and scene objects reflectance functions. It is specially optimized for space scenes, with huge distances between objects and scenes up to Solar System size. Raytracing conveniently tackles some important effects for VBN algorithms: image quality, eclipses, secondary illumination, subpixel limb imaging, etc. From a user standpoint, a simulation is easily setup using the available interfaces (MATLAB/Simulink, Python, and more) by specifying the position of the bodies (Sun, planets, satellites, …) over time, complex 3D shapes and material surface properties, before positioning the camera. -
SPECIAL Comet Shoemaker-Levy 9 Collides with Jupiter
SL-9/JUPITER ENCOUNTER - SPECIAL Comet Shoemaker-Levy 9 Collides with Jupiter THE CONTINUATION OF A UNIQUE EXPERIENCE R.M. WEST, ESO-Garching After the Storm Six Hectic Days in July eration during the first nights and, as in other places, an extremely rich data The recent demise of comet Shoe ESO was but one of many profes material was secured. It quickly became maker-Levy 9, for simplicity often re sional observatories where observations evident that infrared observations, es ferred to as "SL-9", was indeed spectac had been planned long before the critical pecially imaging with the far-IR instru ular. The dramatic collision of its many period of the "SL-9" event, July 16-22, ment TIMMI at the 3.6-metre telescope, fragments with the giant planet Jupiter 1994. It is now clear that practically all were perfectly feasible also during day during six hectic days in July 1994 will major observatories in the world were in time, and in the end more than 120,000 pass into the annals of astronomy as volved in some way, via their telescopes, images were obtained with this facility. one of the most incredible events ever their scientists or both. The only excep The programmes at most of the other predicted and witnessed by members of tions may have been a few observing La Silla telescopes were also successful, this profession. And never before has a sites at the northernmost latitudes where and many more Gigabytes of data were remote astronomical event been so ac the bright summer nights and the very recorded with them. -
The Cold Traps Near South Pole of the Moon
THE COLD TRAPS NEAR SOUTH POLE OF THE MOON. Berezhnoy A.A., Kozlova E.A., Shevchenko V.V. Sternberg State Astronomical Institute, Moscow University, Russia, Moscow, Universitetski pr., 13, 199992. [email protected] According to the data from “Lunar Let us note that NH3 content in the lunar Prospector” [1] the areas of high hydrogen regolith is relatively low, because the main N- content in the lunar south pole region coincide containing compound is molecular nitrogen here with the areas of such craters as Faustini (87.2º [5]. The stability of SO2 subsurface ice requires S, 75.8º E), Cabeus (85.2º S, 323º E) and other the diurnal surface temperature of less than 65 crates. We have allocated a number of craters K. However, volatile species may be which can be considered as "cold traps " in the chemisorbed by the dust particles at the surface. south pole region of the Moon (Figure 1). Some In this case we can expect the existence of from these craters has properties similar to those chemisorbed water, CO2, and SO2 at the content of the echo coming from icy satellites of Jupiter less than 0.1 wt%. and from the southern polar cap of Mars. Polar rovers or penetrators with mass We estimate the total permanently spectrometers can detect these species. For shadowed area in the lunar northern polar region solving the question of the origin of lunar polar at 28 260,2 km2. The total permanently volatiles we must determine isotopic shadowed area in the region of the south pole of composition of these species. -
Exploring the Bombardment History of the Moon
EXPLORING THE BOMBARDMENT HISTORY OF THE MOON Community White Paper to the Planetary Decadal Survey, 2011-2020 September 15, 2009 Primary Author: William F. Bottke Center for Lunar Origin and Evolution (CLOE) NASA Lunar Science Institute at the Southwest Research Institute 1050 Walnut St., Suite 300 Boulder, CO 80302 Tel: (303) 546-6066 [email protected] Co-Authors/Endorsers: Carlton Allen (NASA JSC) Mahesh Anand (Open U., UK) Nadine Barlow (NAU) Donald Bogard (NASA JSC) Gwen Barnes (U. Idaho) Clark Chapman (SwRI) Barbara A. Cohen (NASA MSFC) Ian A. Crawford (Birkbeck College London, UK) Andrew Daga (U. North Dakota) Luke Dones (SwRI) Dean Eppler (NASA JSC) Vera Assis Fernandes (Berkeley Geochronlogy Center and U. Manchester) Bernard H. Foing (SMART-1, ESA RSSD; Dir., Int. Lunar Expl. Work. Group) Lisa R. Gaddis (US Geological Survey) 1 Jim N. Head (Raytheon) Fredrick P. Horz (LZ Technology/ESCG) Brad Jolliff (Washington U., St Louis) Christian Koeberl (U. Vienna, Austria) Michelle Kirchoff (SwRI) David Kring (LPI) Harold F. (Hal) Levison (SwRI) Simone Marchi (U. Padova, Italy) Charles Meyer (NASA JSC) David A. Minton (U. Arizona) Stephen J. Mojzsis (U. Colorado) Clive Neal (U. Notre Dame) Laurence E. Nyquist (NASA JSC) David Nesvorny (SWRI) Anne Peslier (NASA JSC) Noah Petro (GSFC) Carle Pieters (Brown U.) Jeff Plescia (Johns Hopkins U.) Mark Robinson (Arizona State U.) Greg Schmidt (NASA Lunar Science Institute, NASA Ames) Sen. Harrison H. Schmitt (Apollo 17 Astronaut; U. Wisconsin-Madison) John Spray (U. New Brunswick, Canada) Sarah Stewart-Mukhopadhyay (Harvard U.) Timothy Swindle (U. Arizona) Lawrence Taylor (U. Tennessee-Knoxville) Ross Taylor (Australian National U., Australia) Mark Wieczorek (Institut de Physique du Globe de Paris, France) Nicolle Zellner (Albion College) Maria Zuber (MIT) 2 The Moon is unique. -
Project Selene: AIAA Lunar Base Camp
Project Selene: AIAA Lunar Base Camp AIAA Space Mission System 2019-2020 Virginia Tech Aerospace Engineering Faculty Advisor : Dr. Kevin Shinpaugh Team Members : Olivia Arthur, Bobby Aselford, Michel Becker, Patrick Crandall, Heidi Engebreth, Maedini Jayaprakash, Logan Lark, Nico Ortiz, Matthew Pieczynski, Brendan Ventura Member AIAA Number Member AIAA Number And Signature And Signature Faculty Advisor 25807 Dr. Kevin Shinpaugh Brendan Ventura 1109196 Matthew Pieczynski 936900 Team Lead/Operations Logan Lark 902106 Heidi Engebreth 1109232 Structures & Environment Patrick Crandall 1109193 Olivia Arthur 999589 Power & Thermal Maedini Jayaprakash 1085663 Robert Aselford 1109195 CCDH/Operations Michel Becker 1109194 Nico Ortiz 1109533 Attitude, Trajectory, Orbits and Launch Vehicles Contents 1 Symbols and Acronyms 8 2 Executive Summary 9 3 Preface and Introduction 13 3.1 Project Management . 13 3.2 Problem Definition . 14 3.2.1 Background and Motivation . 14 3.2.2 RFP and Description . 14 3.2.3 Project Scope . 15 3.2.4 Disciplines . 15 3.2.5 Societal Sectors . 15 3.2.6 Assumptions . 16 3.2.7 Relevant Capital and Resources . 16 4 Value System Design 17 4.1 Introduction . 17 4.2 Analytical Hierarchical Process . 17 4.2.1 Longevity . 18 4.2.2 Expandability . 19 4.2.3 Scientific Return . 19 4.2.4 Risk . 20 4.2.5 Cost . 21 5 Initial Concept of Operations 21 5.1 Orbital Analysis . 22 5.2 Launch Vehicles . 22 6 Habitat Location 25 6.1 Introduction . 25 6.2 Region Selection . 25 6.3 Locations of Interest . 26 6.4 Eliminated Locations . 26 6.5 Remaining Locations . 27 6.6 Chosen Location . -
Conceptual Human-System Interface Design for a Lunar Access Vehicle
Conceptual Human-System Interface Design for a Lunar Access Vehicle Mary Cummings Enlie Wang Cristin Smith Jessica Marquez Mark Duppen Stephane Essama Massachusetts Institute of Technology* Prepared For Draper Labs Award #: SC001-018 PI: Dava Newman HAL2005-04 September, 2005 http://halab.mit.edu e-mail: [email protected] *MIT Department of Aeronautics and Astronautics, Cambridge, MA 02139 TABLE OF CONTENTS 1 INTRODUCTION..................................................................................................... 1 1.1 THE GENERAL FRAMEWORK................................................................................ 1 1.2 ORGANIZATION.................................................................................................... 2 2 H-SI BACKGROUND AND MOTIVATION ........................................................ 3 2.1 APOLLO VS. LAV H-SI........................................................................................ 3 2.2 APOLLO VS. LUNAR ACCESS REQUIREMENTS ...................................................... 4 3 THE LAV CONCEPTUAL PROTOTYPE............................................................ 5 3.1 HS-I DESIGN ASSUMPTIONS ................................................................................ 5 3.2 THE CONCEPTUAL PROTOTYPE ............................................................................ 6 3.3 LANDING ZONE (LZ) DISPLAY............................................................................. 8 3.3.1 LZ Display Introduction................................................................................. -
Rare Astronomical Sights and Sounds
Jonathan Powell Rare Astronomical Sights and Sounds The Patrick Moore The Patrick Moore Practical Astronomy Series More information about this series at http://www.springer.com/series/3192 Rare Astronomical Sights and Sounds Jonathan Powell Jonathan Powell Ebbw Vale, United Kingdom ISSN 1431-9756 ISSN 2197-6562 (electronic) The Patrick Moore Practical Astronomy Series ISBN 978-3-319-97700-3 ISBN 978-3-319-97701-0 (eBook) https://doi.org/10.1007/978-3-319-97701-0 Library of Congress Control Number: 2018953700 © Springer Nature Switzerland AG 2018 This work is subject to copyright. All rights are reserved by the Publisher, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. The publisher, the authors, and the editors are safe to assume that the advice and information in this book are believed to be true and accurate at the date of publication. Neither the publisher nor the authors or the editors give a warranty, express or implied, with respect to the material contained herein or for any errors or omissions that may have been made. -
Impact Cratering in the Solar System
Impact Cratering in the Solar System Michelle Kirchoff Lunar and Planetary Institute University of Houston - Clear Lake Physics Seminar March 24, 2008 Outline What is an impact crater? Why should we care about impact craters? Inner Solar System Outer Solar System Conclusions Open Questions What is an impact crater? Basically a hole in the ground… Barringer Meteor Crater (Earth) Bessel Crater (Moon) Diameter = 1.2 km Diameter = 16 km Depth = 200 m Depth = 2 km www.lpi.usra.edu What creates an “impact” crater? •Galileo sees circular features on Moon & realizes they are depressions (1610) •In 1600-1800’s many think they are volcanic features: look similar to extinct volcanoes on Earth; some even claim to see volcanic eruptions; space is empty (meteorites not verified until 1819 by Chladni) •G.K. Gilbert (1893) first serious support for lunar craters from impacts (geology and experiments) •On Earth Barringer (Meteor) crater recognized as created by impact by Barringer (1906) •Opik (1916) - impacts are high velocity, thus create circular craters at most impact angles Melosh, 1989 …High-Velocity Impacts! www.lpl.arizona.edu/SIC/impact_cratering/Chicxulub/Animation.gif Physics of Impact Cratering Understand how stress (or shock) waves propagate through material in 3 stages: 1. Contact and Compression 2. Excavation 3. Modification www.psi.edu/explorecraters/background.htm Hugoniot Equations Derived by P.H. Hugoniot (1887) to describe shock fronts using conservation of mass, momentum and energy across the discontinuity. equation (U-up) = oU of state P-Po = oupU E-Eo = (P+Po)(Vo-V)/2 P - pressure U - shock velocity up - particle velocity E - specific internal energy V = 1/specific volume) Understanding Crater Formation laboratory large simulations explosives (1950’s) (1940’s) www.nasa.gov/centers/ames/ numerical simulations (1960’s) www.lanl.gov/ Crater Morphology • Simple • Complex • Central peak/pit • Peak ring www3.imperial.ac. -
Icebreaker: a Lunar South Pole Exploring Robot Cmu-Ri-Tr-97-22
ICEBREAKER: A LUNAR SOUTH POLE EXPLORING ROBOT CMU-RI-TR-97-22 Matthew C. Deans Alex D. Foessel Gregory A. Fries Diana LaBelle N. Keith Lay Stewart Moorehead Ben Shamah Kimberly J. Shillcutt Professor: Dr. William Whittaker The Robotics Institute Carnegie Mellon University Pittsburgh PA 15213 Spring 1996-97 Executive Summary Icebreaker: A Lunar South Pole Exploring Robot Due to the low angles of sunlight at the lunar poles, craters and other depressions in the polar regions can contain areas which are in permanent darkness and are at cryogenic temperatures. Many scientists have theorized that these cold traps could contain large quantities of frozen volatiles such as water and carbon dioxide which have been deposited over billions of years by comets, meteors and solar wind. Recent bistatic radar data from the Clementine mission has yielded results consistent with water ice at the South Pole of the Moon however Earth based observations from the Arecibo Radar Observatory indicate that ice may not exist. Due to the controversy surrounding orbital and Earth based observations, the only way to definitively answer the question of whether ice exists on the Lunar South Pole is in situ analysis. The discovery of water ice and other volatiles on the Moon has many important benefits. First, this would provide a source of rocket fuel which could be used to power rockets to Earth, Mars or beyond, avoiding the high cost of Earth based launches. Secondly, water and carbon dioxide along with nitrogen from ammonia form the essential elements for life and could be used to help support human colonies on the Moon. -
LRO Makes a Temperature Map of the Lunar South Pole 42
LRO Makes a Temperature Map of the Lunar South Pole 42 The Lunar Reconnaissance Orbiter (LRO) has recently created the first surface temperature map of the south polar region of the moon using date taken between September and October, 2009 when south polar temperatures were close to their annual maximum values. The colorized map shows the locations of several intensely cold impact craters that are potential cold traps for water ice as well as a range of other icy compounds commonly observed in comets. The approximate maximum temperatures at which these compounds would be frozen in place for more than a billion years is shown on the scale to the right. The LCROSS spacecraft was targeted to impact one of the coldest of these craters, and many of these compounds were observed in the ejecta plume. (Courtesy: UCLA/NASA/JPL) Problem 1 - The width of this map is 500 km. What are the diameters of Crater A (Shackleton) and Crater B (Amundsen) in kilometers? Problem 2 - In which colored areas might an astronaut expect to find conditions cold enough to recover all of the elements and molecules indicated in the vertical temperature scale to the right? Problem 3 - The Shackleton Crater (Crater A) is cold enough to trap water and methanol. From Problem 1, and assuming that the thickness of the water deposit is 100 meters, and occupies 10% of the volume of the circular crater, how many cubic meters of water-ice might be present? Space Math http://spacemath.gsfc.nasa.gov Answer Key 42 Problem 1 - The width of this map is 500 km. -
Preliminary Science Report
7. Photographic Summary of Apollo 77 Mission James H. Sasser The geographical exploration of new frontiers mil Estar polyester base. Ektachrome EF S016S has usually occurred many years before scien- color film on a 2.5-mil Estar polyester base was tists visited and studied the areas in detail. For exposed on the lunar surface. Thc higher speed example, the existence of Antarctica as a conti- of this color film was expected to be more suit- nent was known from the time Charles Wilkes able for lunar surface photography because of explored 1500 miles of the coastline in 1840. tl~elow light levels anticipated and confirmed However, extensive Antarctic exploration did to exist on the lunar surface. Other color 70-mm not begin until the 20th century with the voy- exposures of the Earth and Moon were taken ages of Scott, Amundsen, Shackleton, and Byrd. on Ektachrome MS S036S color reversal film It was not until the International Geophysical on a 2.5-mil Estar polyester base. Year (July 1957 to December 1958) that scien- The 16-mm film taken during lunar module tists from 12 countries began conducting an (LM) descent provided the first accurate knowl- ambitious Antarctic research program. In this edge of the exact landing point on the lunar respect, the first manned lunar exploration was surface. The 70-mm photographs taken on the unique. The scientific experiments were care- lunar surface provided panoramic views of the fully planned, and the astronauts were trained surface near the landed LM and allowed de- as surrogates for scientists representing many tailed topographic mapping of the lunar surface disciplines. -
Sampling the SPA Basin Some Considerations Based on the Apollo Experience
Sampling the SPA Basin Some Considerations Based on the Apollo Experience Paul D. Spudis Applied Physics Laboratory Workshop on Science Associated with the Lunar Exploration Architecture February 27- March 2, 2007 How do you best sample the Moon? Samples without context have limited value Bulk planet properties, inventory of compositions Context requires either geologic field work or a simple regional setting Robotic missions tend to provide less context than human field study cf. Luna 20 and Apollo 16 Types of Exploratory Targets Reconnaissance Geologically simple sites where a “grab sample” of rocks and regolith can address and solve scientific issues Example: youngest mare lava flow, impact melt floor of fresh crater, regional pyroclastics Field Study Complex, multi-unit sites having a protracted evolution. Require human interaction, sampling, mapping, re-visiting field sites Examples: basin ejecta blanket, Aristarchus plateau, crater central peaks See Ryder et al., 1989, EOS, v. 70, n. 47, p. 1495; 1505-1520 Apollo Highlands Sampling Apollo 14 – Fra Mauro Sent to sample Fra Mauro Fm (Imbrium ejecta) Returned complex breccias; basaltic, KREEP-rich Which samples are Imbrium basin primary ejecta? Apollo 15 – Hadley-Apennines Sample front (deep Imbrium rim material) Anorthosite, KREEP basalts, mafic impact melts Which samples represent Imbrium basin melt? Apollo 16 – Descartes Sent to sample highland volcanic rocks Anorthositic debris, breccias, some mafic melts (VHA) Basin-related? If so, which ones? Apollo 17 – Taurus-Littrow Sample