Structure of the South Pole-Aitken Basin from KAGUYA Selenodesy Data
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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. -
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 . -
Planning a Mission to the Lunar South Pole
Lunar Reconnaissance Orbiter: (Diviner) Audience Planning a Mission to Grades 9-10 the Lunar South Pole Time Recommended 1-2 hours AAAS STANDARDS Learning Objectives: • 12A/H1: Exhibit traits such as curiosity, honesty, open- • Learn about recent discoveries in lunar science. ness, and skepticism when making investigations, and value those traits in others. • Deduce information from various sources of scientific data. • 12E/H4: Insist that the key assumptions and reasoning in • Use critical thinking to compare and evaluate different datasets. any argument—whether one’s own or that of others—be • Participate in team-based decision-making. made explicit; analyze the arguments for flawed assump- • Use logical arguments and supporting information to justify decisions. tions, flawed reasoning, or both; and be critical of the claims if any flaws in the argument are found. • 4A/H3: Increasingly sophisticated technology is used Preparation: to learn about the universe. Visual, radio, and X-ray See teacher procedure for any details. telescopes collect information from across the entire spectrum of electromagnetic waves; computers handle Background Information: data and complicated computations to interpret them; space probes send back data and materials from The Moon’s surface thermal environment is among the most extreme of any remote parts of the solar system; and accelerators give planetary body in the solar system. With no atmosphere to store heat or filter subatomic particles energies that simulate conditions in the Sun’s radiation, midday temperatures on the Moon’s surface can reach the stars and in the early history of the universe before 127°C (hotter than boiling water) whereas at night they can fall as low as stars formed. -
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. -
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. -
The Peaks of Eternal Light
The Peaks of Eternal Light: a Near-term Property Issue on the Moon Martin Elvis a,1, Tony Milligan b, Alanna Krolikowskic a Harvard-Smithsonian Center for Astrophysics, 60 Garden St., Cambridge MA 02138, USA; [email protected]; b Department of Theology and Religious Studies, King’s College London, Virginia Wolf Building, 22 Kingsway, London WC2B 6NR. c Georg-August Universität Göttingen, Heinrich-Düker-Weg 14, 37073, Göttingen, Germany; [email protected] ABSTRACT The Outer Space Treaty makes it clear that the Moon is the ‘province of all mankind’, with the latter ordinarily understood to exclude state or private appropriation of any portion of its surface. However, there are indeterminacies in the Treaty and in space law generally over the issue of appropriation. These indeterminacies might permit a close approximation to a property claim or some manner of ‘quasi-property’. The recently revealed highly inhomogeneous distribution of lunar resources changes the context of these issues. We illustrate this altered situation by considering the Peaks of Eternal Light. They occupy about one square kilometer of the lunar surface. We consider a thought experiment in which a Solar telescope is placed on one of the Peaks of Eternal Light at the lunar South pole for scientific research. Its operation would require non- disturbance, and hence that the Peak remain unvisited by others, effectively establishing a claim of protective exclusion and de facto appropriation. Such a telescope would be relatively easy to emplace with today’s technology and so poses a near-term property issue on the Moon. While effective appropriation of a Peak might proceed without raising some of the familiar problems associated with commercial development (especially lunar mining), the possibility of such appropriation nonetheless raises some significant issues concerning justice and the safeguarding of scientific practice on the lunar surface. -
Antarctic Treaty Handbook
Annex Proposed Renumbering of Antarctic Protected Areas Existing SPA’s Existing Site Proposed Year Annex V No. New Site Management Plan No. Adopted ‘Taylor Rookery 1 101 1992 Rookery Islands 2 102 1992 Ardery Island and Odbert Island 3 103 1992 Sabrina Island 4 104 Beaufort Island 5 105 Cape Crozier [redesignated as SSSI no.4] - - Cape Hallet 7 106 Dion Islands 8 107 Green Island 9 108 Byers Peninsula [redesignated as SSSI no. 6] - - Cape Shireff [redesignated as SSSI no. 32] - - Fildes Peninsula [redesignated as SSSI no.5] - - Moe Island 13 109 1995 Lynch Island 14 110 Southern Powell Island 15 111 1995 Coppermine Peninsula 16 112 Litchfield Island 17 113 North Coronation Island 18 114 Lagotellerie Island 19 115 New College Valley 20 116 1992 Avian Island (was SSSI no. 30) 21 117 ‘Cryptogram Ridge’ 22 118 Forlidas and Davis Valley Ponds 23 119 Pointe-Geologic Archipelago 24 120 1995 Cape Royds 1 121 Arrival Heights 2 122 Barwick Valley 3 123 Cape Crozier (was SPA no. 6) 4 124 Fildes Peninsula (was SPA no. 12) 5 125 Byers Peninsula (was SPA no. 10) 6 126 Haswell Island 7 127 Western Shore of Admiralty Bay 8 128 Rothera Point 9 129 Caughley Beach 10 116 1995 ‘Tramway Ridge’ 11 130 Canada Glacier 12 131 Potter Peninsula 13 132 Existing SPA’s Existing Site Proposed Year Annex V No. New Site Management Plan No. Adopted Harmony Point 14 133 Cierva Point 15 134 North-east Bailey Peninsula 16 135 Clark Peninsula 17 136 North-west White Island 18 137 Linnaeus Terrace 19 138 Biscoe Point 20 139 Parts of Deception Island 21 140 ‘Yukidori Valley’ 22 141 Svarthmaren 23 142 Summit of Mount Melbourne 24 118 ‘Marine Plain’ 25 143 Chile Bay 26 144 Port Foster 27 145 South Bay 28 146 Ablation Point 29 147 Avian Island [redesignated as SPA no. -
Lunar Exploration Efforts
Module 3 – Nautical Science Unit 4 – Astronomy Chapter 13 - The Moon Section 1 – The Moon What You Will Learn to Do Demonstrate understanding of astronomy and how it pertains to our solar system and its related bodies: Moon, Sun, stars and planets Objectives 1. Recognize basic facts about the Moon such as size, distance from Earth and atmosphere 2. Describe the geographical structure of the Moon 3. Describe the surface features of the Moon 4. Explain those theories that describe Moon craters and their formations Objectives 5. Describe the mountain ranges and riles on the surface of the Moon 6. Explain the effect moonquakes have on the Moon 7. Describe how the Moon’s motion causes its phases 8. Explain the basic reasons for Moon exploration Key Terms CPS Key Term Questions 1 - 12 Key Terms Maria - Mare or Maria (plural); Any of the several dark plains on the Moon and Mars; Latin word for “Sea” Reflectance - The ratio of the intensity of reflected radiation to that of the radiation that initially hits the surface. Key Terms Impact Crater - The cup shaped depression or cavity on the surface of the Earth or other heavenly bodies. Breccia - Rock composed of angular fragments of older rocks melded together as a result of a meteor impact. Regolith - The layer of disintegrated rock fragments (dust), just above the solid rock of the Moon’s crust. Key Terms Rilles - Cracks in the lunar surface similar to shallow, meandering river beds on the Earth. Phases The Moon’s motion in its orbit (of the Moon) - causes its phases (progressive changes in the visible portion of the Moon). -
Redacted for Privacy Abstract Approved: John V
AN ABSTRACT OF THE THESIS OF MIAH ALLAN BEAL for the Doctor of Philosophy (Name) (Degree) in Oceanography presented on August 12.1968 (Major) (Date) Title:Batymety and_Strictuof_thp..4rctic_Ocean Redacted for Privacy Abstract approved: John V. The history of the explordtion of the Central Arctic Ocean is reviewed.It has been only within the last 15 years that any signifi- cant number of depth-sounding data have been collected.The present study uses seven million echo soundings collected by U. S. Navy nuclear submarines along nearly 40, 000 km of track to construct, for the first time, a reasonably complete picture of the physiography of the basin of the Arctic Ocean.The use of nuclear submarines as under-ice survey ships is discussed. The physiography of the entire Arctic basin and of each of the major features in the basin are described, illustrated and named. The dominant ocean floor features are three mountain ranges, generally paralleling each other and the 40°E. 140°W. meridian. From the Pacific- side of the Arctic basin toward the Atlantic, they are: The Alpha Cordillera; The Lomonosov Ridge; andThe Nansen Cordillera. The Alpha Cordillera is the widest of the three mountain ranges. It abuts the continental slopes off the Canadian Archipelago and off Asia across more than550of longitude on each slope.Its minimum width of about 300 km is located midway between North America and Asia.In cross section, the Alpha Cordillera is a broad arch rising about two km, above the floor of the basin.The arch is marked by volcanoes and regions of "high fractured plateau, and by scarps500to 1000 meters high.The small number of data from seismology, heat flow, magnetics and gravity studies are reviewed.The Alpha Cordillera is interpreted to be an inactive mid-ocean ridge which has undergone some subsidence. -
Strategies for Detecting Biological Molecules on Titan
ASTROBIOLOGY Volume 18, Number 5, 2018 ª Mary Ann Liebert, Inc. DOI: 10.1089/ast.2017.1758 Strategies for Detecting Biological Molecules on Titan Catherine D. Neish,1 Ralph D. Lorenz,2 Elizabeth P. Turtle,2 Jason W. Barnes,3 Melissa G. Trainer,4 Bryan Stiles,5 Randolph Kirk,6 Charles A. Hibbitts,2 and Michael J. Malaska5 Abstract Saturn’s moon Titan has all the ingredients needed to produce ‘‘life as we know it.’’ When exposed to liquid water, organic molecules analogous to those found on Titan produce a range of biomolecules such as amino acids. Titan thus provides a natural laboratory for studying the products of prebiotic chemistry. In this work, we examine the ideal locales to search for evidence of, or progression toward, life on Titan. We determine that the best sites to identify biological molecules are deposits of impact melt on the floors of large, fresh impact craters, specifically Sinlap, Selk, and Menrva craters. We find that it is not possible to identify biomolecules on Titan through remote sensing, but rather through in situ measurements capable of identifying a wide range of biological molecules. Given the nonuniformity of impact melt exposures on the floor of a weathered impact crater, the ideal lander would be capable of precision targeting. This would allow it to identify the locations of fresh impact melt deposits, and/or sites where the melt deposits have been exposed through erosion or mass wasting. Determining the extent of prebiotic chemistry within these melt deposits would help us to understand how life could originate on a world very different from Earth. -
South Pole-Aitken Basin
Feasibility Assessment of All Science Concepts within South Pole-Aitken Basin INTRODUCTION While most of the NRC 2007 Science Concepts can be investigated across the Moon, this chapter will focus on specifically how they can be addressed in the South Pole-Aitken Basin (SPA). SPA is potentially the largest impact crater in the Solar System (Stuart-Alexander, 1978), and covers most of the central southern farside (see Fig. 8.1). SPA is both topographically and compositionally distinct from the rest of the Moon, as well as potentially being the oldest identifiable structure on the surface (e.g., Jolliff et al., 2003). Determining the age of SPA was explicitly cited by the National Research Council (2007) as their second priority out of 35 goals. A major finding of our study is that nearly all science goals can be addressed within SPA. As the lunar south pole has many engineering advantages over other locations (e.g., areas with enhanced illumination and little temperature variation, hydrogen deposits), it has been proposed as a site for a future human lunar outpost. If this were to be the case, SPA would be the closest major geologic feature, and thus the primary target for long-distance traverses from the outpost. Clark et al. (2008) described four long traverses from the center of SPA going to Olivine Hill (Pieters et al., 2001), Oppenheimer Basin, Mare Ingenii, and Schrödinger Basin, with a stop at the South Pole. This chapter will identify other potential sites for future exploration across SPA, highlighting sites with both great scientific potential and proximity to the lunar South Pole. -
Theoretical Study on Thermal Release of Helium-3 in Lunar Ilmenite
minerals Article Theoretical Study on Thermal Release of Helium-3 in Lunar Ilmenite Hongqing Song 1,*, Jie Zhang 1, Yueqiang Sun 2, Yongping Li 2, Xianguo Zhang 2, Dongyu Ma 1 and Jue Kou 1 1 School of Civil and Resource Engineering, University of Science and Technology Beijing, Beijing 100083, China; [email protected] (J.Z.); [email protected] (D.M.); [email protected] (J.K.) 2 National Space Science Center, Chinese Academy of Science, Beijing 100190, China; [email protected] (Y.S.); [email protected] (Y.L.); [email protected] (X.Z.) * Correspondence: [email protected]; Tel.: +86-010-82376239 Abstract: The in-situ utilization of lunar helium-3 resource is crucial to manned lunar landings and lunar base construction. Ilmenite was selected as the representative mineral which preserves most of the helium-3 in lunar soil. The implantation of helium-3 ions into ilmenite was simulated to figure out the concentration profile of helium-3 trapped in lunar ilmenite. Based on the obtained concentration profile, the thermal release model for molecular dynamics was established to investigate the diffusion and release of helium-3 in ilmenite. The optimal heating temperature, the diffusion coefficient, and the release rate of helium-3 were analyzed. The heating time of helium-3 in lunar ilmenite under actual lunar conditions was also studied using similitude analysis. The results show that after the implantation of helium-3 into lunar ilmenite, it is mainly trapped in vacancies and interstitials of ilmenite crystal and the corresponding concentration profile follows a Gaussian distribution.