Appendix D. Thermal Modelling of Luna 27 Landing Site. Hannah Rana Vito Laneve Philipp Hager Thierry Tirolien (ESA/ESTEC, The Netherlands)
|
|
|
- Bethany Merritt
- 5 years ago
- Views:
Transcription
1 47 Appendix D Thermal Modelling of Luna 27 Landing Site Hannah Rana Vito Laneve Philipp Hager Thierry Tirolien (ESA/ESTEC, The Netherlands)
2 48 Thermal Modelling of Luna 27 Landing Site Abstract Luna 27, also known as the Lunar Resource Lander, is the Russian-ESA collaborative mission to the permanently shadowed craters at the south pole of the moon. In this study, the thermal environment of the potential landing site of the lander is assessed with the use of ESATAN-TMS. A series of modelling approaches are explored in order to address the different factors that may impact the thermal environment affecting the lander, namely surface infrared, direct impingent solar flux, the transient cases of sunrise and sunset, and the lunar topography. The effect of the orientation of the lander was further considered with regards to the on-board European units PILOT and PROSPECT. The models were then assessed in light of theoretical flux balances, empirical lunar regolith temperature correlations, and data from NASA s Lunar Reconnaissance Orbiter.
3 Thermal Modelling of Luna 27 Landing Site 49 Thermal Modelling of Luna 27 Landing Site Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien European Space Agency ESA UNCLASSIFIED - For Official Use Background Luna-27: ESA-Russia collaboration Scheduled for flight in 2025 Landing site: 82.7 o S, 33.5 o E European technology on-board: PILOT (Precise Intelligent Landing using On board Technology) PROSPECT (Platform for Resource Observation and in-situ Prospecting in support of Exploration, Commercial Exploitation & Transportation). Searching for volatiles (CHON compounds) à access to lunar subsurface & sample capability testing à ensure stringent K constraint for sample preservation Aitken basin Drill ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 2
4 50 Thermal Modelling of Luna 27 Landing Site Thermal Modelling Drivers Light & dark phases Sunrise/Sunset cases Topographical impact of landing region Verify ESATAN-TMS capability for lunar surface model ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 3 Initial Assessment of Landing Site Phase B1 of project Thermo-optical properties of lunar surface regolith ε=0.97, α=0.93 IR steady state flux of 707 W/m 2 for hot case ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 4
5 51 Thermal Modelling of Luna 27 Landing Site Disc Model Lander Multi-node 30m radius disc Scaled down horizon Planet Surface in ESATAN-TMS Defining moon as planetary body Surface without capacity; only positioning in space Optical Finish IR Emissivity Solar Absorptivity Lunar Regolith MLI Black Surface ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 5 Lunar Topography Several mountains in region; might radiate heat to lander Lunar surface close to black body 90o incident angle of sun; surface heating to K (right) Southern pole slopes Mountains km may be significant Concerned with temperature development of samples being drilled ESA UNCLASSIFIED - For Official Use 31st European Space Thermal Analysis Workshop Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide October 2017
6 52 Thermal Modelling of Luna 27 Landing Site Sunrise to Sunset 198 W/m W/m 2 ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 7 Model Validation Control method: FIXED RAYS Surface criticality: NORMAL Number of rays for REF and HF: 10,000 Theoretical vs computed: 0.37% maximum difference Maximum sun elevation (245.6K; 27.6 o C) Direct Solar Flux (W/m 2 ) ESATAN Theoretical Azimuth Angle ( o ) ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 8
7 Thermal Modelling of Luna 27 Landing Site 53 Topography Model 1km x 1km 1 km x 1 km from LRO (maximum sun elevation) Lander modelled as black cube PROSPECT Node (facing away from sun) considered Comparable results to disc model - Q s and Q IR impingent on lander SUN Heat Load Surface - Disc Surface - Topography Q S 6.38 W W Q IR W W ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 9 Topography Model 30km x 30km Limited number of surface nodes with view factor to cube node Small dimensions of cube vs scale of topography ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 10
8 54 Thermal Modelling of Luna 27 Landing Site Topography Model 30km x 30km 30m radius comparable to disc model Heat Load Surface Disc (30m radius) Surface Topography (1 km x 1 km) Surface Topography (30 km x 30 km) Q S 6.38 W W 4.94 W Q IR W W W ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 11 Discussion Demonstrated feasibility of ESATAN-TMS for modelling lunar surface environment. Effect of mountains located 20-30km away negligible. 1km x 1km heat load presents highest heat loads; useful for specifying worst hot case conditions. All results specific for 82.7 o S and 33.5 o E. ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 12
9 Thermal Modelling of Luna 27 Landing Site 55 Thank you for your attention! Thanks to Vito Laneve & Philipp Hager Supervisor Thierry Tirolien Conference Organiser Harrie Rooijackers ESA UNCLASSIFIED - For Official Use Hannah Rana, Vito Laneve, Philipp Hager, Thierry Tirolien 24/10/2017 Slide 13
10 56
Upgraded Program of Russian Lunar Landers: Studying of Lunar Poles
Upgraded Program of Russian Lunar Landers: Studying of Lunar Poles I.G.Mitrofanov, L.M.Zelenyi and V.I.Tret yakov Institute for Space Research, Moscow, Russia Slide - 1 Main Goals of the Program: 1. To
Appendix C. Mercury Retro-Reflection Modelling and Effects on MPO Solar Array. Anja Frey Giulio Tonellotto (ESA/ESTEC, The Netherlands)
51 Appendix C Mercury Retro-Reflection Modelling and Effects on MPO Solar Array Anja Frey Giulio Tonellotto (ESA/ESTEC, The Netherlands) 9 th European Space Thermal Analysis Workshop 3 November 15 5 Mercury
Mini-RF: An Imaging Radar for the Moon. Ben Bussey The Johns Hopkins University Applied Physics Laboratory
Mini-RF: An Imaging Radar for the Moon Ben Bussey The Johns Hopkins University Applied Physics Laboratory Paul D. Spudis President s Commission on Implementation of United States Space Exploration Policy
NASA: BACK TO THE MOON
NASA: BACK TO THE MOON Don Campbell Cornell University "I believe that this nation should commit itself to achieving the goal, before this decade is out, of landing a man on the moon and returning him
Appendix G. Solar Orbiter SPICE Thermal Design, Analysis and Testing. Samuel Tustain (RAL Space, United Kingdom)
137 Appendix G Solar Orbiter SPICE Thermal Design, Analysis and Testing Samuel Tustain (RAL Space, United Kingdom) 138 Solar Orbiter SPICE Thermal Design, Analysis and Testing Abstract 1 The Spectral Imaging
1. Weather and climate.
Lecture 31. Introduction to climate and climate change. Part 1. Objectives: 1. Weather and climate. 2. Earth s radiation budget. 3. Clouds and radiation field. Readings: Turco: p. 320-349; Brimblecombe:
CRaTER Thermal Analysis
CRaTER Thermal Analysis Huade Tan Contents System Overview Design & Requirements Inputs and Assumptions Power Dissipations Environment and Orbit Current Model Results Instrument temperatures Orbital temperature
Plans for an International Lunar Network
Science Mission Directorate Plans for an International Lunar Network Tom Morgan May 2008 ROBOTIC LUNAR EXPLORATION Starting no later than 2008, initiate a series of robotic missions to the Moon to prepare
Lunar Exploration Requirements and Data Acquisition Architectures
Lunar Exploration Requirements and Data Acquisition Architectures J. Plescia P. Spudis B. Bussey Johns Hopkins University / Applied Physics Laboratory 2005 International Lunar Conference The Vision and
Thermal Correlation of BepiColombo MOSIF 10 Solar Constants Simulation Test. Savino De Palo Tiziano Malosti (ThalesAlenia Space, Italy)
271 Appendix Q Thermal Correlation of BepiColombo MOSIF 10 Solar Constants Simulation Test Savino De Palo Tiziano Malosti (ThalesAlenia Space, Italy) Gianluca Filiddani (Sofiter System Eng., Italy) 272
Luna Resource / Glob Missions: Starting list of potential landing sites
Luna Resource / Glob Missions: Starting list of potential landing sites A.T. Basilevsky, A.M. Abdrakhimov, M.A. Ivanov, R.O. Kuzmin, E.N. Slyuta Vernadsky Institute of Geochemistry & Analytical Chemistry,
Appendix B. A proposition for updating the environmental standards using real Earth Albedo and Earth IR Flux for Spacecraft Thermal Analysis
19 Appendix B A proposition for updating the environmental standards using real Earth Albedo and Earth IR Romain Peyrou-Lauga (ESA/ESTEC, The Netherlands) 31 st European Space Thermal Analysis Workshop
LRO-LOLA: Measurements of Lunar Altimetry and Surface Conditions
LRO-LOLA: Measurements of Lunar Altimetry and Surface Conditions David E. Smith, MIT Maria T. Zuber, MIT Gregory A. Neumann, GSFC Erwan Mazarico, GSFC and the LOLA Science Team Lunar-Glob Mission International
An Overview of BepiColombo Thermal Analysis
An Overview of BepiColombo Thermal Analysis Presented by Ian Renouf, Astrium UK ESTEC 9-10 th Summary About BepiColombo Thermal Design Issues Required Thermal Analysis Thermal Modelling Issues Proposed
Conducting Subsurface Surveys for Water Ice using Ground Penetrating Radar and a Neutron Spectrometer on the Lunar Electric Rover Never Stop
Conducting Subsurface Surveys for Water Ice using Ground Penetrating Radar and a Neutron Spectrometer on the Lunar Electric Rover LPI/Kring Never Stop Exploring David A. Kring Lunar and Planetary Institute
Ludwig Combrinck HartRAO 3rd Space Geodesy Workshop 16 March 2009 Matjiesfontein
Space Geodesy and Space Science Ludwig Combrinck HartRAO 3rd Space Geodesy Workshop 16 March 2009 Matjiesfontein DST s Concept of Space Science SA Space Agency, commercial applications, CSIR Satellite
PROSPECT: ESA s Package for Resource Observation and In-Situ Prospecting for Exploration, Commercial Exploitation and Transportation
PROSPECT: ESA s Package for Resource Observation and In-Situ Prospecting for Exploration, Commercial Exploitation and Transportation E. Sefton-Nash, J. Carpenter and the PROSPECT Team LRO/LROC/ASU Lunar
The Moon's Dark, Icy Poles
1 of 5 posted June 4, 2003 The Moon's Dark, Icy Poles --- Permanently shadowed regions on the Moon--where frozen water could be trapped--are more abundant and more widely distributed than originally thought.
Overview of Lunar Science Objectives. Opportunities and guidelines for future missions.
Overview of Lunar Science Objectives. Opportunities and guidelines for future missions. Chip Shearer Institute of Meteoritics University of New Mexico Albuquerque, New Mexico 87131 A rich scientific target
Thermal Design of the Solar Array in a Low Earth Orbit Satellite by Analytical and Numerical Methods
Thermal Design of the Solar Array in a Low Earth Orbit Satellite by Analytical and Numerical Methods Korea Aerospace Research Institute Hui-Kyung Kim*, Jang-Joon Lee, Bum-Seok Hyun and Cho-Young Han Background
LEAG Illumination Modeling at the Lunar Poles and its Benefits to Exploration and Science Investigations
LEAG 2015 2015.10.21 Illumination Modeling at the Lunar Poles and its Benefits to Exploration and Science Investigations Erwan Mazarico and J.B. Nicholas NASA GSFC Erwan Mazarico - LEAG - October 21, 2015
Lunar Satellite Attitude Determination System
Lunar Satellite Attitude Determination System SENIOR DESIGN PROPOSAL PRESENTATION TEAM EPOCH KUPOLUYI, TOLULOPE (LEAD DEVELOPER) SONOIKI, OLUWAYEMISI (LEAD RESEARCHER) WARREN, DANAH (PROJECT MANAGER) NOVEMBER
SOLAR FURNACE. By Heiko Ritter JOURNEY TO THE INNER
SOLAR FURNACE 88 Seite 1 By Heiko Ritter JOURNEY TO THE INNER THERMAL TESTS FOR Seite 2 SOLAR SYSTEM B E P I C O L O M B O T he European Space Agency, ESA, is currently developing a mission to the planet
THE SUN-EARTH-MOON SYSTEM
Date Period Name THE SUN-EARTH-MOON SYSTEM SECTION 27.1 Tools of Astronomy In your textbook, read about electromagnetic radiation and telescopes. Use each of the terms below just once to complete the passage.
Mian Abbas, Jim Spann, Andre LeClair NASA Marshall Space Flight Center, Huntsville, AL
Lunar Dust Distributions From So Infrared Absorption Measurement With a Fourier Transform Spectrometer Mian Abbas, Jim Spann, Andre LeClair NASA Marshall Space Flight Center, Huntsville, AL John Brasunas,
Thermal Design and Analysis of the BroadBand Radiometer. Oliver Poyntz-Wright (Rutherford Appleton Laboratory, United Kingdom)
255 Appendix T Thermal Design and Analysis of the BroadBand Radiometer Oliver Poyntz-Wright (Rutherford Appleton Laboratory, United Kingdom) 256 Thermal Design and Analysis of the BroadBand Radiometer
Europe to the Moon. BHF 10 Feb 2005 SPC
Europe to the Moon V162 lift-off on 27 September 2003 at 23:14:39 UTC The launch was perfect SMART-1 separated at 23:56:03 into a GTO (656 x 35,881 km): perfect injection 100 s later telemetry was received
James Carpenter, Lunar Lander Office, Directorate of Human Spaceflight and Operations
The European Lunar Lander James Carpenter, Lunar Lander Office, Directorate of Human Spaceflight and Operations 1 International Context Apollo/Luna Era 1990-2006 2007-2012 2013-2020 Next Decade HITEN CLEMENTINE
NASA Planetary Science Programs
NASA Planetary Science Programs James L. Green NASA, Planetary Science Division February 19, 2015 Presentation at OPAG 1 Outline Mission events Passed FY15 Budget elements President s FY16 Budget Discovery
SMART-1 lunar highlights
SMART-1 lunar highlights Bernard H. Foing & SMART-1 Project & Operations team, SMART-1 Science Technology Working Team, SMART-1 Impact Campaign Team http://sci.esa.int/smart-1/, www.esa.int Europe to the
Presentation given to computer science undergraduate students at the University of Houston July 2007
Presentation given to computer science undergraduate students at the University of Houston July 2007 Machine Learning and Data Mining in Mars Tomasz F. Stepinski Lunar and Planetary Institute MARS/EARTH
International Lunar Observatory Association. International Lunar Observatory Association (ILOA) 2007
International Lunar Observatory Association (ILOA) 2007 Steve M. Durst, / ILOA Hawai`i and California, USA International Lunar Observatory Association (ILOA) 2007 Steve M. Durst, / ILOA Hawai`i and California,
NASA Lunar Science Activities. Lunar Science and Exploration
NASA Lunar Science Activities Lunar Science and Exploration James L. Green Director, Planetary Sciences Division Science Directorate Mission Directorate NASA In NASA s James Science L. Green Mission Presented
Lunar Discovery and Exploration program
Lunar Discovery and Exploration program Space Policy Directive-1 (December 11, 2017) amends the National Space Policy to include the following paragraph: Lead an innovative and sustainable program of exploration
Malapert Mountain: A Recommended Site for a South Polar Outpost
For presentation at the Rutgers Symposium on Lunar Settlements, June 4-8, 2007 Malapert Mountain: A Recommended Site for a South Polar Outpost Paul. D. Lowman Jr. Goddard Space Flight Center, Code 698
Lunar Precursor Robotics Program
National Aeronautics and Space Administration SCIENCE & MISSION SYSTEMS Lunar Precursor Robotics Program Michael J. Wargo, Sc.D. Chief Lunar Scientist for Exploration Systems Larry Hill LRO Mission Manager
Resource Allocation Planning and Scheduling Office. Deep Space Station-15 Out-of-Service Assessment Report. April 11, 2003
Resource Allocation Planning and Scheduling Office Deep Space Station-15 Out-of-Service Assessment Report April 11, 2003 Roger Bartoo Study Description This study describes a Deep Space Network (DSN) loading
Moon and Mercury 3/8/07
The Reading Assignment Chapter 12 Announcements 4 th homework due March 20 (first class after spring break) Reminder about term paper due April 17. Next study-group session is Monday, March 19, from 10:30AM-12:00Noon
Appendix B. GENETIK+ Near-real time thermal model correlation using genetic algorithm. Guillaume Mas (CNES, France)
19 Appendix B GENETIK+ Near-real time thermal model correlation using genetic algorithm Guillaume Mas (CNES, France) 20 GENETIK+ Near-real time thermal model correlation using genetic algorithm Abstract
Chapter 3: Cycles of the Sky
Chapter 3: Cycles of the Sky Motions of the Planets Mercury Venus Earth All planets in almost circular (elliptical) orbits around the sun, in approx. the same plane, the ecliptic plane. The Moon is orbiting
MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question.
ASTRO 102/104 Prelim 2 Name Section MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. 1) This is version E of the exam. Please fill in (E). A) This
MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question.
ASTRO 102/104 Prelim 2 Name Section MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. 1) This is version B of the exam. Please fill in (B). A) This
THE EUROPEAN LUNAR LANDER: ROBOTIC OPERATIONS IN A HARSH ENVIRONMENT
THE EUROPEAN LUNAR LANDER: ROBOTIC OPERATIONS IN A HARSH ENVIRONMENT ESA/ESTEC, NOORDWIJK, THE NETHERLANDS / 12 14 APRIL 2011 Richard Fisackerly (1), James Carpenter (1), Diego De Rosa (1), Bérengère Houdou
Laboratory Studies of Lunar Dust Transport
Laboratory Studies of Lunar Dust Transport X. Wang, M. Horanyi and S. Robertson Colorado Center for Lunar Dust and Atmospheric Studies (CCLDAS) 4.15.2010 Lunar plasma Environment Evidence of electrostatic
a. 0.1 AU b. 10 AU c light years d light years
1 AST104 Sp2006: EXAM 1 Multiple Choice Questions: Mark the best answer choice on the bubble form. Read all answer choices before making selection. (No credit given when multiple answers are marked.) 1.
NEXT-LL-LES-ESA(HME)-0001
prepared by/préparé par ESA NEXT Team reference/réference issue/édition 1 revision/révision 0 date of issue/date d édition 20 February 2008 a NEXT - Lunar Environment Specification page ii of v APPROVAL
Where we are now. The Moon Chapters 8.2, 9. Topography. Outline
Where we are now Introduction Little things - comets, asteroids, KBOs Slightly larger things - Moon Larger still - Terrestrial planets Really large - Jovian planets Jovian moons + Pluto Extrasolar Planets
The Effects of Atmospheric Variations on the High Energy Radiation Environment at the Surface of Mars
The Effects of Atmospheric Variations on the High Energy Radiation Environment at the Surface of Mars A. Keating, Laboratório de Instrumentação e Física Experimental de Partículas, Lisbon, Portugal (keating@lip.pt)
Stas Barabash 1 Yoshifumi Futaana 1 and the SELMA Team. Swedish Institute of Space Physics Kiruna, Sweden. DAP, Boulder, January, 2017
Stas Barabash 1 Yoshifumi Futaana 1 and the SELMA Team 1 Swedish Institute of Space Physics Kiruna, Sweden DAP, Boulder, January, 2017 1 SELMA core team 2 SELMA main scientific questions SELMA (Surface,
Rationale of NASA Lunar Precursor Robotic Program (LPRP) for the VSE
Rationale of NASA Lunar Precursor Robotic Program (LPRP) for the VSE (vs. I don t need nuthin but a map) Jeff Plescia, Ben Bussey, Paul Spudis, Tony Lavoie Applied Physics Laboratory, Johns Hopkins University
Sunlight and its Properties Part I. EE 446/646 Y. Baghzouz
Sunlight and its Properties Part I EE 446/646 Y. Baghzouz The Sun a Thermonuclear Furnace The sun is a hot sphere of gas whose internal temperatures reach over 20 million deg. K. Nuclear fusion reaction
Europe-Japan Space Science Collaboration. Saku Tsuneta Institute of Space and Astronautical Science Japan Aerospace Exploration Agency
Europe-Japan Space Science Collaboration Saku Tsuneta Institute of Space and Astronautical Science Japan Aerospace Exploration Agency March 7, 2018 JAXA recent science missions HAYABUSA 2003-2010 Asteroid
SOLAR WIND VOLATILE PRESERVATION. Samantha R. Jacob Department of Geology and Geophysics University of Hawai i at Mānoa Honolulu, HI ABSTRACT
SOLAR WIND VOLATILE PRESERVATION Samantha R. Jacob Department of Geology and Geophysics University of Hawai i at Mānoa Honolulu, HI 96822 ABSTRACT Because the Moon has a negligible atmosphere and magnetosphere,
Lunar Flashlight Project
ABSTRACT Recent observations of the Moon with the Moon Mineralogy Mapper (M3), Lunar Crater Observation and Sensing Satellite (LCROSS), the Lunar Reconnaissance Orbiter (LRO) and other evidence suggest
RESERVE THALES ALENIA SPACE CHANGE RECORDS ISSUE DATE DESCRIPTION OF CHANGES AUTHOR
ISSUE : 1 Page : 2/35 CHANGE RECORDS ISSUE DATE DESCRIPTION OF CHANGES AUTHOR 1 03/10/07 Initial issue (MTG-TAF-SA-RS-39) J. VIEILLOT 1 20/09/10 Updated version for kick off : L.OUCHET New reference (MTG-TAF-SA-SS-0039)
Eight Years MOS-IRS Summary of Calibration Activities
Eight Years MOS-IRS Summary of Calibration Activities Workshop on Inter-Comparison of Large Scale Optical and Infrared Sensors 12 14 October 2004, ESA / ESTEC Noordwijk, The Netherlands Horst Schwarzer,
The greenhouse effect
16 Waves of amplitude of 1 m roll onto a beach at a rate of one every 12 s. If the wavelength of the waves is 120 m, calculate (a) the velocity of the waves (b) how much power there is per metre along
The Science Scenario of the SELENE-2 Mission
The Science Scenario of the SELENE-2 Mission Manabu Kato, Kohtaro Matsumoto, Tatsuaki Okada, Satoshi Tanaka, and Science Working Group for Post- SELENE Project Japan Aerospace Exploration Agency ISAS &
Expanding Science with SmallSats/CubeSats
National Aeronautics and Space Administration Expanding Science with SmallSats/CubeSats Outer Planets Analysis Group John D. Baker 2/2/2016 2016, Government Sponsorship Acknowledged National Aeronautics
The Moon. A look at our nearest neighbor in Space! Free powerpoints at
The Moon A look at our nearest neighbor in Space! Free powerpoints at http://www.worldofteaching.com What is the Moon? A natural satellite One of more than 96 moons in our Solar System The only moon of
Class Exercise. Today s Class: The Origin & Evolution of the Moon. Space in the News: NASA and Russia Partner Up for Crewed Deep-Space Missions
Today s Class: The Origin & Evolution of the Moon 1. 2. 3. 4. Homework. Read: Sections 9.2-9.3 in Cosmic Perspective. Next class is at Fiske Planetarium! Need volunteers for Space in the News. Exam #2
C) wavelength C) eastern horizon B) the angle of insolation is high B) increases, only D) thermosphere D) receive low-angle insolation
1. What is the basic difference between ultraviolet, visible, and infrared radiation? A) half-life B) temperature C) wavelength D) wave velocity 2. In New York State, the risk of sunburn is greatest between
TRANSIENT HEAT TRANSFER ANALYSIS ON A SATELLITE IN AN ORBIT
TRANSIENT HEAT TRANSFER 7/12/05 11:52 AM Page 50 TRANSIENT HEAT TRANSFER ANALYSIS ON A SATELLITE IN AN ORBIT C.W. Chan and C.P. Tso* *Faculty of Engineering and Technology, Multimedia University, Jalan
SATELLITES: ACTIVE WORLDS AND EXTREME ENVIRONMENTS. Jessica Bolda Chris Gonzalez Crystal Painter Natalie Innocenzi Tyler Vasquez.
SATELLITES: ACTIVE WORLDS AND EXTREME ENVIRONMENTS Jessica Bolda Chris Gonzalez Crystal Painter Natalie Innocenzi Tyler Vasquez. Areas of interest! How did the Satellites of the outer solar system form
Chandrayaan Mission Objectives and future lunar programs
Chandrayaan Mission Objectives and future lunar programs CHANDRAYAAN -I Paul Spudis, channeling J. N. Goswami Principal Scientist, Chandrayaan-1 Mission The Clementine & Lunar Prospector Missions to Moon
Using analogue missions to develop Lunar exploration strategies. Marianne Mader Carleton University, Ottawa, Canada
Using analogue missions to develop Lunar exploration strategies Marianne Mader Carleton University, Ottawa, Canada Space fairing Nations are developing their plans for space exploration: US Vision for
Data and formulas at the end. Exam would be Weds. May 8, 2008
ATMS 321: Science of Climate Practice Mid Term Exam - Spring 2008 page 1 Atmospheric Sciences 321 Science of Climate Practice Mid-Term Examination: Would be Closed Book Data and formulas at the end. Exam
Симпозиум Исследования Солнечной системы
Производство гамма и нейтронного излучения в приповерхностном слое Production of gamma and neutron radiation in the subsurface Определение элементного состава поверхности по гамма линиям Analysis of elemental
Appendix E. Development of a thermal control system for South Africa s next generation Earth observation satellite
51 Appendix E Development of a thermal control system for South Africa s next generation Earth observation satellite Daniël van der Merwe (DENEL Spaceteq, South Africa) 52 Development of a thermal control
The Earth's Moon. The Earth's Moon, in many ways, is prototypical of a substantial fraction of the objects in the Solar System.
1 The Earth's Moon The Earth's Moon, in many ways, is prototypical of a substantial fraction of the objects in the Solar System. Like many other moons and planets it exhibits a heavily cratered surface
Stars, Galaxies & the Universe (29:50) Professor C.C. Lang Exam #1 - Fall 2010 Wednesday, September 22 nd FORM B - SOLUTIONS
Stars, Galaxies & the Universe (29:50) Professor C.C. Lang Exam #1 - Fall 2010 Wednesday, September 22 nd FORM B - SOLUTIONS Questions 1-6 are True/False questions (worth 4 pts each): 1. The Sun is a Red
Planetary Science Unit Map Grade 8
Planetary Science Unit Map Grade 8 Course Goal and Description: In Planetary Science students study the Earth as a celestial object before progressing to lunar science/exploration, and then to Solar System
HEOMD Overview March 16, 2015
National Aeronautics and Space Administration HEOMD Overview March 16, 2015 Ben Bussey Chief Exploration Scientist HEOMD, NASA HQ National Aeronautics and Space Administration NASA Strategic Plan Objective
Thermal Wadis: Using Regolith for Thermal Energy Management
Thermal Wadis: Using Regolith for Thermal Energy Management Kurt Sacksteder, NASA Glenn Research Center Robert Wegeng, Battelle Memorial Institute Nantel Suzuki, NASA Headquarters Annual Meeting of the
Scientific Contributions of Lunar Robotic Precursor Missions
Scientific Contributions of Lunar Robotic Precursor Missions Paul D. Spudis Johns Hopkins University Applied Physics Laboratory paul.spudis@jhuapl.edu www.spudislunarresources.com Presentation to LEAG
ANALYSIS OF MERCURIAN CRATERS BY MEANS OF CARTOGRAFIC METHOD.
ANALYSIS OF MERCURIAN CRATERS BY MEANS OF CARTOGRAFIC METHOD. Kozlova E.A. 1, Sitnikov B.D 1., Rodionova J.F. 1, Shevchenko V.V. 1 1. Sternberg State Astronomical Institute, Universitetskiy prospect 13,
ICE IN THE FAR-IR & DIVINER 3. Far-IR Subteam: Ben Greenhagen, Christopher Edwards, Dan McCleese Additional Contributions: Tim Schofield & Paul Hayne
ICE IN THE FAR-IR & DIVINER 3 Far-IR Subteam: Ben Greenhagen, Christopher Edwards, Dan McCleese Additional Contributions: Tim Schofield & Paul Hayne WHY FAR IR? ~45µm fundamental ice feature (e.g. Moore
E d. h, c o, k are all parameters from quantum physics. We need not worry about their precise definition here.
The actual form of Plank s law is: b db d b 5 e C C2 1 T 1 where: C 1 = 2hc o 2 = 3.7210 8 Wm /m 2 C 2 = hc o /k = 1.3910 mk Where: h, c o, k are all parameters from quantum physics. We need not worry
Lunar Reconnaissance Orbiter Camera Image Retrieval For the Big Moon Dig
Lunar Reconnaissance Orbiter Camera Image Retrieval For the Big Moon Dig Tom Riley TomRiley@WoodwareDesigns.com November 22, 2014 File: LROCameraRetrivalmmdddyy.docx Work in Progress LRO in orbit (artist
Response to Unified Theory of Climate
Response to Unified Theory of Climate Dr. Daniel M. Sweger National College Introduction During the last two years that I have been teaching Environmental Science and attempting to explain global warming
Data and formulas at the end. Real exam is Wednesday May 8, 2002
ATMS 31: Physical Climatology Practice Mid Term Exam - Spring 001 page 1 Atmospheric Sciences 31 Physical Climatology Practice Mid-Term Examination: Would be Closed Book Data and formulas at the end. Real
Exercise 1: Earth s Moon
PHYS1014 Physical Science Summer 2013 Professor Kenny L. Tapp Exercise 1: Earth s Moon Complete and submit this packet, securely stapled, at the beginning of Exam 1. PART I --- Online Video Lecture from
Radiative Equilibrium Models. Solar radiation reflected by the earth back to space. Solar radiation absorbed by the earth
I. The arth as a Whole (Atmosphere and Surface Treated as One Layer) Longwave infrared (LWIR) radiation earth to space by the earth back to space Incoming solar radiation Top of the Solar radiation absorbed
Mechanical Engineering Research Journal
Dept of Mech Eng CUET Published Online March 215 (http://wwwcuetacbd/merj/indexhtml) Mechanical Engineering Research Journal Vol 9, pp 79 85, 213 M E R J ISSN: 199-5491 THERMAL ANALYSES OF NANO- AND MICRO-
Practice Questions: Seasons #2
1. How many degrees does the Sun appear to move across the sky in four hours? A) 60 B) 45 C) 15 D) 4 Practice Questions: Seasons #2 2. Base your answer to the following question on the diagram below, which
Venus: NASA HQ Perspectives
Venus: NASA HQ Perspectives National Aeronautics and Space Administration Andrew Danztler Planetary Division Director Adriana Ocampo Venus Discipline Scientist Adriana.C.Ocampo@nasa.gov Pasadena, USA 1-2
UK lunar exploration: Current activities and future possibilities
UK lunar exploration: Current activities and future possibilities October 2007 Professor Alan Smith Director, Mullard Space Science Laboratory On behalf of: The British National Space Centre and The Science
Thermal Radiation Effects on Deep-Space Satellites Part 2
Thermal Radiation Effects on Deep-Space Satellites Part 2 Jozef C. Van der Ha www.vanderha.com Fundamental Physics in Space, Bremen October 27, 2017 Table of Contents Mercury Properties & Parameters Messenger
Motions of the Sun Model Exploration
Name Date Bell Motions of the Sun Model Exploration 1. Go to the University of Nebraska-Lincoln Motions of the Sun Simulator: http://astro.unl.edu/naap/motion3/animations/sunmotions.swf 2. This is what
10/24/2010. Venus Roman goddess of love. Bulk Properties. Summary. Venus is easier to observe than Mercury! Venus and Earth
Venus Roman goddess of love Birth of Venus Botticelli (1485) Bulk Properties Summary 1. Venus is 28% closer to the Sun having an orbital period of 225 Earth days 2. Venus is roughly 95% the size, 82% the
Life in the Solar System
Life in the Solar System Basic Requirements for Life 1. Chemical elements to make biological molecules. On Earth these are mostly C, H, O and N 2. Source of energy for metabolism. This can come from a
The Moon. Tides. Tides. Mass = 7.4 x 1025 g = MEarth. = 0.27 REarth. (Earth 5.5 g/cm3) Gravity = 1/6 that of Earth
The Moon Mass = 7.4 x 1025 g = 0.012 MEarth Radius = 1738 km = 0.27 REarth Density = 3.3 g/cm3 (Earth 5.5 g/cm3) Gravity = 1/6 that of Earth Dark side of the moon We always see the same face of the Moon.
Today s Class. Results for Exam #2 11/7/2017. Today s Class: Robotic & Human Exploration of Mars
11/7/2017 Today s Class: Robotic & Human Exploration of Mars Results for Exam #2 Homework: 1. Reading for Earth as a Planet: Section 9.4 of Cosmic Perspective. 2. Meet at Fiske on Thursday! Average Median
Thermal Systems Design
Thermal Systems Design Fundamentals of heat transfer Radiative equilibrium Surface properties Non-ideal effects Internal power generation Environmental temperatures Conduction Thermal system components
Space weather. Introduction to lectures by Dr John S. Reid. Image courtesy:
Space weather Introduction to lectures by Dr John S. Reid Image courtesy: http://www.astro-photography.com/ss9393.htm Sunspot 9393 First pass from late March to early April, 2001 See: Storms from the Sun
China s Chang E Program
China s Chang E Program --- Missions Objectives, Plans, Status, and Opportunity for Astronomy Maohai Huang Science and Application Research Center for Lunar and Deepspace Explorations National Astronomical
Aerobraking A mission enabling and fuel saving technique for orbit changes - Venus Express and ExoMars TGO. Håkan Svedhem ESA/ESTEC
ILEWG Aerobraking A mission enabling and fuel saving technique for orbit changes - Venus Express and ExoMars TGO Håkan Svedhem ESA/ESTEC ILEWG Earth Venus Trajectory 2 ILEWG Reducing Apocentre altitude
Life and habitability in the Solar System and beyond: the Roadmap
"There are more things in heaven and earth, Horatio, than are dreamt of in your philosophy." Hamlet (I, v, 166-167) Life and habitability in the Solar System and beyond: the Roadmap Lucia Marinangeli and
NASA s Planetary Science Program Status
NASA s Planetary Science Program Status Presentation to VEXAG James L. Green Director, Planetary Science Division October 28, 2009 1 Outline MSL status Announcements of Opportunity R&A International Agreements
Prospector-1: A Low-Cost Commercial Asteroid Mission Grant Bonin SmallSat 2016
Prospector-1: A Low-Cost Commercial Asteroid Mission Grant Bonin SmallSat 2016 About DSI A space technology and resources company Vision to enable the human space development by harvesting asteroid materials