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Mars Reconnaissance Orbiter
Chapter 6 Mars Reconnaissance Orbiter Jim Taylor, Dennis K. Lee, and Shervin Shambayati 6.1 Mission Overview The Mars Reconnaissance Orbiter (MRO) [1, 2] has a suite of instruments making observations at Mars, and it provides data-relay services for Mars landers and rovers. MRO was launched on August 12, 2005. The orbiter successfully went into orbit around Mars on March 10, 2006 and began reducing its orbit altitude and circularizing the orbit in preparation for the science mission. The orbit changing was accomplished through a process called aerobraking, in preparation for the “science mission” starting in November 2006, followed by the “relay mission” starting in November 2008. MRO participated in the Mars Science Laboratory touchdown and surface mission that began in August 2012 (Chapter 7). MRO communications has operated in three different frequency bands: 1) Most telecom in both directions has been with the Deep Space Network (DSN) at X-band (~8 GHz), and this band will continue to provide operational commanding, telemetry transmission, and radiometric tracking. 2) During cruise, the functional characteristics of a separate Ka-band (~32 GHz) downlink system were verified in preparation for an operational demonstration during orbit operations. After a Ka-band hardware anomaly in cruise, the project has elected not to initiate the originally planned operational demonstration (with yet-to-be used redundant Ka-band hardware). 201 202 Chapter 6 3) A new-generation ultra-high frequency (UHF) (~400 MHz) system was verified with the Mars Exploration Rovers in preparation for the successful relay communications with the Phoenix lander in 2008 and the later Mars Science Laboratory relay operations. -
Mro High Resolution Imaging Science Experiment (Hirise)
Sixth International Conference on Mars (2003) 3287.pdf MROHIGHRESOLUTIONIMAGINGSCIENCEEXPERIMENT(HIRISE): INSTRUMENTDEVELOPMENT.AlanDelamere,IraBecker,JimBergstrom,JonBurkepile,Joe Day,DavidDorn,DennisGallagher,CharlieHamp,JeffreyLasco,BillMeiers,AndrewSievers,Scott StreetmanStevenTarr,MarkTommeraasen,PaulVolmer.BallAerospaceandTechnologyCorp.,PO Box1062,Boulder,CO80306 Focus Introduction:Theprimaryfunctionalre- Mechanism PrimaryMirror quirementoftheHiRISEimager,figure1isto PrimaryMirrorBaffle 2nd Fold allowidentificationofbothpredictedandun- Mirror knownfeaturesonthesurfaceofMarstoa muchfinerresolutionandcontrastthanprevi- ouslypossible[1],[2].Thisresultsinacam- 1st Fold erawithaverywideswathwidth,6kmat Mirror 300kmaltitude,andahighsignaltonoise ratio,>100:1.Generationofterrainmaps,30 Filters cmverticalresolution,fromstereoimages Focal requiresveryaccurategeometriccalibration. Plane Theprojectlimitationsofmass,costand schedulemakethedevelopmentchallenging. FocalPlane SecondaryMirror Inaddition,thespacecraftstability[3]must Electronics TertiaryMirror SecondaryMirrorBaffle notbeamajorlimitationtoimagequality. Thenominalorbitforthesciencephaseofthe missionisa3pmorbitof255by320kmwith Figure1Cameraopticalpathoptimizedforlowmass periapsislockedtothesouthpole.Thetrack Integration(TDI)tocreateveryhigh(100:1)signalnoise velocityisapproximately3,400m/s. ratioimages. HiRISEFeatures:TheHiRISEinstrumentperformance Theimagerdesignisanall-reflectivethreemirrorastig- goalsarelistedinTable1.Thedesignfeaturesa50cm matictelescopewithlight-weightedZeroduropticsanda -
Sirius Astronomer
September 2015 Free to members, subscriptions $12 for 12 issues Volume 42, Number 9 Jeff Horne created this image of the crater Copernicus on September 13, 2005 from his observing site in Irvine. September 19 is International Observe The Moon Night, so get out there and have a look at a source of light pollution we really don’t mind! OCA MEETING STAR PARTIES COMING UP The free and open club meeng will The Black Star Canyon site will open on The next session of the Beginners be held September 18 at 7:30 PM in September 5. The Anza site will be open on Class will be held at the Heritage Mu‐ the Irvine Lecture Hall of the Hashing‐ September 12. Members are encouraged to seum of Orange County at 3101 West er Science Center at Chapman Univer‐ check the website calendar for the latest Harvard Street in Santa Ana on Sep‐ sity in Orange. This month, JPL’s Dr. updates on star pares and other events. tember 4. The following class will be Dave Doody will discuss the Grand held October 2. Finale of the historic Cassini mission to Please check the website calendar for the Saturn in 2017! outreach events this month! Volunteers are GOTO SIG: TBA always welcome! Astro‐Imagers SIG: Sept. 8, Oct. 13 NEXT MEETINGS: October 9, Novem‐ Remote Telescopes: TBA You are also reminded to check the web ber 13 Astrophysics SIG: Sept. 11, Oct. 16 site frequently for updates to the calendar Dark Sky Group: TBA of events and other club news. -
Chaos in the Inert Oort Cloud
EPSC Abstracts Vol. 13, EPSC-DPS2019-1303-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Chaos in the inert Oort cloud Melaine Saillenfest (1), Marc Fouchard (1), and Arika Higuchi (2) (1) IMCCE, Observatoire de Paris, France, (2) RISE Project Office/NAOJ, Mitaka, Tokyo, Japan e-mail: [email protected] µ 16 Abstract 2 εP − εG ÝÖ 14 2 We investigate the orbital dynamics of small bodies in aÙ 9 12 the intermediate regime between the Kuiper belt and − 10 the Oort cloud, i.e. where the planetary perturbations ´ 10 and the galactic tides have the same order of magni- 8 tude. We show that this region is far less inert than it could appear at first sight, despite very weak orbital 6 perturbations. Ô eÖØÙÖbaØiÓÒ 4 Øhe Óf 2 1. Introduction ×iÞe 0 0 500 1000 1500 2000 2500 3000 aÜi× ´aÙµ The orbits of distant trans-Neptunian objects are sub- ×eÑi¹Ña jÓÖ a ject to internal perturbations from the planets, and ex- ternal perturbations from the galactic tides. A distinc- Figure 1: Size of the small parameters appearing in tion is generally made between the Kuiper belt and the the Hamiltonian function (Eq. 1) with respect to the Oort cloud, which are thought to have been initially semi-major axis of the small body. The red curve rep- populated through distinct mechanisms (see e.g. the resents the planetary perturbations, and the blue curve recent review by [4]). However, there is no dynamical represents the galactic tides. boundary between the two populations, and numerical simulations show a continuous transfer of objects in 2. -
NOAO Hosts “Colors of Nature” Summer Academy
On the Cover The cover shows an 8 × 9 arcminutes image of a portion of the Milky Way galactic bulge, obtained as part of the Blanco DECam Bulge Survey (BDBS) using the Dark Energy Camera (DECam) on the CTIO Blanco 4-m telescope. In this image, red, green, and blue (RGB) pixels correspond to DECam’s Y, z and i filters, respectively. The inset image shows the 2 × 3 array of monitors at the “observer2” workstation in the Blanco control room. The six chips shown here represent only 10% of the camera’s field of view. For more information about the BDBS and their experiences observing with DECam, see the “The Blanco DECam Bulge Survey (BDBS)” article in the Science Highlights section of this Newsletter. (Image credit: Will Clarkson, University of Michigan-Dearborn; Kathy Vivas, NOAO; R. Michael Rich, UCLA; and the BDBS team.) NOAO Newsletter NATIONAL OPTICAL ASTRONOMY OBSERVATORY ISSUE 110 — SEPTEMBER 2014 Director’s Corner Under Construction: A Revised KPNO Program Emerges ................ 2 CTIO Instruments Available for 2015A ......................................... 18 Gemini Instruments Available for 2015A ..................................... 19 Science Highlights KPNO Instruments Available for 2015A........................................ 20 The Survey of the MAgellanic Stellar History (SMASH) ................... 3 AAT Instruments Available for 2015A .......................................... 21 Two’s Company in the Inner Oort Cloud ......................................... 5 CHARA Instruments Available for 2015 ....................................... -
An Implementation Concept for the ASPIRE Mission
An Implementation Concept for the ASPIRE Mission. W. D. Deininger* ([email protected]), W. Purcell,* P. Atcheson,*G. Mills,* S. A Sandford,** R. P. Hanel,** M. McKelvey,** and R. McMurray** *Ball Aerospace & Technologies Corp. (BATC) P. O. Box 1062 Boulder, CO, USA 80306-1062 **NASA Ames Research Center Moffett Field, CA, USA 94035 Abstract—The Astrobiology Space Infrared Explorer complex and tied to the cyclic process whereby these (ASPIRE) is a Probe-class mission concept developed as elements are ejected into the diffuse interstellar medium part of NASA’s Astrophysics Strategic Mission Concept (ISM) by dying stars, gathered into dense clouds and studies. 1 2 ASPIRE uses infrared spectroscopy to explore formed into the next generation of stars and planetary the identity, abundance, and distribution of molecules, systems (Figure 1). Each stage in this cycle entails chemical particularly those of astrobiological importance throughout alteration of gas- and solid-state species by a diverse set of the Universe. ASPIRE’s observational program is focused astrophysical processes: hocks, stellar winds, radiation on investigating the evolution of ices and organics in all processing by photons and particles, gas-phase neutral and phases of the lifecycle of carbon in the universe, from ion chemistry, accretion, and grain surface reactions. These stellar birth through stellar death while also addressing the processes create new species, destroy old ones, cause role of silicates and gas-phase materials in interstellar isotopic enrichments, shuffle elements between chemical organic chemistry. ASPIRE achieves these goals using a compounds, and drive the universe to greater molecular Spitzer-derived, cryogenically-cooled, 1-m-class telescope complexity. -
PUBLIC OPEN EVENING Outreach — 17 January 2017 — A
Institute of Astronomy PUBLIC OPEN EVENING outreach — 17 January 2017 — A Clean water ice hiding just below TONIGHT’S SPEAKER the surface of Mars The talk schedule for this term can be viewed at: this term can be viewed talk schedule for The Matt Bothwell The biggest galaxy in the Universe? Our weekly welcome ELCOME to our weekly public Wopen evenings for the 2017/18 season. Each night there will be a half-hour talk which begins promptly Erosion on Mars has uncovered large, steep cross-sections of clean, subterranean ice. In this at 7.15pm: tonight Matt Bothwell will false color image captured by NASA’s HiRISE camera, one of eight recently discovered stripes be giving us his talk The biggest appears dark blue against the Martian terrain. Credit: NASA/JPL/Uni. Of Arizona/USGS galaxy in the Universe? The talk is followed by an oppor- IT’S GOOD news for future Martian scientists have discovered this in no tunity to observe if (and only if!) the www.ast.cam.ac.uk/public/public_observing/current colonists – NASA has just discovered less than eight different places across weather is clear. The IoA’s historical plenty of easy-to-access water just Mars, in both hemispheres. Northumberland and Thorrowgood under Mars’s surface. The new photographs were taken by Astronomers have known for ‘HiRISE’, a powerful camera attached telescopes, along with our modern decades that water exists on Mars, but to NASA’s Mars Reconnaissance Orbit- 16-inch telescope, will be open just how easy it is to get at (and use) er, and the purity of the hidden water for observations. -
Arxiv:1706.07447V1 [Astro-Ph.EP] 22 Jun 2017 Periods
Origin and Evolution of Short-Period Comets David Nesvorn´y1, David Vokrouhlick´y2, Luke Dones1, Harold F. Levison1, Nathan Kaib3, Alessandro Morbidelli4 (1) Department of Space Studies, Southwest Research Institute, 1050 Walnut St., Suite 300, Boulder, CO 80302, USA (2) Institute of Astronomy, Charles University, V Holeˇsoviˇck´ach2, CZ{18000 Prague 8, Czech Republic (3) HL Dodge Department of Physics and Astronomy, University of Oklahoma, Norman, OK 73019, USA (4) D´epartement Cassiop´ee,University of Nice, CNRS, Observatoire de la C^oted'Azur, Nice, 06304, France ABSTRACT Comets are icy objects that orbitally evolve from the trans-Neptunian region into the inner Solar System, where they are heated by solar radiation and be- come active due to sublimation of water ice. Here we perform simulations in which cometary reservoirs are formed in the early Solar System and evolved over 4.5 Gyr. The gravitational effects of Planet 9 (P9) are included in some sim- ulations. Different models are considered for comets to be active, including a simple assumption that comets remain active for Np(q) perihelion passages with perihelion distance q < 2:5 au. The orbital distribution and number of active comets produced in our model is compared to observations. The orbital distri- bution of ecliptic comets (ECs) is well reproduced in models with Np(2:5) ' 500 and without P9. With P9, the inclination distribution of model ECs is wider than the observed one. We find that the known Halley-type comets (HTCs) have a nearly isotropic inclination distribution. The HTCs appear to be an exten- sion of the population of returning Oort-cloud comets (OCCs) to shorter orbital arXiv:1706.07447v1 [astro-ph.EP] 22 Jun 2017 periods. -
Composition of Mars, Michelle Wenz
The Composition of Mars Michelle Wenz Curiosity Image NASA Importance of minerals . Role in transport and storage of volatiles . Ex. Water (adsorbed or structurally bound) . Control climatic behavior . Past conditions of mars . specific pressure and temperature formation conditions . Constrains formation and habitability Curiosity Rover at Mount Sharp drilling site, NASA image Missions to Mars . 44 missions to Mars (all not successful) . 21 NASA . 18 Russia . 1 ESA . 1 India . 1 Japan . 1 joint China/Russia . 1 joint ESA/Russia . First successful mission was Mariner 4 in 1964 Credit: Jason Davis / astrosaur.us, http://utprosim.com/?p=808 First Successful Mission: Mariner 4 . First image of Mars . Took 21 images . No evidence of canals . Not much can be said about composition Mariner 4, NASA image Mariner 4 first image of Mars, NASA image Viking Lander . First lander on Mars . Multispectral measurements Viking Planning, NASA image Viking Anniversary Image, NASA image Viking Lander . Measured dust particles . Believed to be global representation . Computer generated mixtures of minerals . quartz, feldspar, pyroxenes, hematite, ilmenite Toulmin III et al., 1977 Hubble Space Telescope . Better resolution than Mariner 6 and 7 . Viking limited to three bands between 450 and 590 nm . UV- near IR . Optimized for iron bearing minerals and silicates Hubble Space Telescope NASA/ESA Image featured in Astronomy Magazine Hubble Spectroscopy Results . 1994-1995 . Ferric oxide absorption band 860 nm . hematite . Pyroxene 953 nm absorption band . Looked for olivine contributions . 1042 nm band . No significant olivine contributions Hubble Space Telescope 1995, NASA Composition by Hubble . Measure of the strength of the absorption band . Ratio vs. -
Mars Reconnaissance Orbiter's High Resolution Imaging Science
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 112, E05S02, doi:10.1029/2005JE002605, 2007 Click Here for Full Article Mars Reconnaissance Orbiter’s High Resolution Imaging Science Experiment (HiRISE) Alfred S. McEwen,1 Eric M. Eliason,1 James W. Bergstrom,2 Nathan T. Bridges,3 Candice J. Hansen,3 W. Alan Delamere,4 John A. Grant,5 Virginia C. Gulick,6 Kenneth E. Herkenhoff,7 Laszlo Keszthelyi,7 Randolph L. Kirk,7 Michael T. Mellon,8 Steven W. Squyres,9 Nicolas Thomas,10 and Catherine M. Weitz,11 Received 9 October 2005; revised 22 May 2006; accepted 5 June 2006; published 17 May 2007. [1] The HiRISE camera features a 0.5 m diameter primary mirror, 12 m effective focal length, and a focal plane system that can acquire images containing up to 28 Gb (gigabits) of data in as little as 6 seconds. HiRISE will provide detailed images (0.25 to 1.3 m/pixel) covering 1% of the Martian surface during the 2-year Primary Science Phase (PSP) beginning November 2006. Most images will include color data covering 20% of the potential field of view. A top priority is to acquire 1000 stereo pairs and apply precision geometric corrections to enable topographic measurements to better than 25 cm vertical precision. We expect to return more than 12 Tb of HiRISE data during the 2-year PSP, and use pixel binning, conversion from 14 to 8 bit values, and a lossless compression system to increase coverage. HiRISE images are acquired via 14 CCD detectors, each with 2 output channels, and with multiple choices for pixel binning and number of Time Delay and Integration lines. -
Descent Trajectory Reconstruction and Landing Site Positioning of Changâ
ARTICLE https://doi.org/10.1038/s41467-019-12278-3 OPEN Descent trajectory reconstruction and landing site positioning of Chang’E-4 on the lunar farside Jianjun Liu1,2, Xin Ren 1, Wei Yan 1, Chunlai Li 1,2, He Zhang 3, Yang Jia3, Xingguo Zeng1, Wangli Chen1, Xingye Gao1, Dawei Liu1, Xu Tan1, Xiaoxia Zhang1, Tao Ni1,2, Hongbo Zhang1, Wei Zuo 1, Yan Su1 & Weibin Wen1 Chang’E-4 (CE-4) was the first mission to accomplish the goal of a successful soft landing on 1234567890():,; the lunar farside. The landing trajectory and the location of the landing site can be effectively reconstructed and determined using series of images obtained during descent when there were no Earth-based radio tracking and the telemetry data. Here we reconstructed the powered descent trajectory of CE-4 using photogrammetrically processed images of the CE-4 landing camera, navigation camera, and terrain data of Chang’E-2. We confirmed that the precise location of the landing site is 177.5991°E, 45.4446°S with an elevation of −5935 m. The landing location was accurately identified with lunar imagery and terrain data with spatial resolutions of 7 m/p, 5 m/p, 1 m/p, 10 cm/p and 5 cm/p. These results will provide geodetic data for the study of lunar control points, high-precision lunar mapping, and subsequent lunar exploration, such as by the Yutu-2 rover. 1 Key Laboratory of Lunar and Deep Space Exploration, National Astronomical Observatories, Chinese Academy of Sciences, Beijing 100101, China. 2 School of Astronomy and Space Science, University of Chinese Academy of Sciences, Beijing 100049, China. -
Preliminary Cost Model for Space Telescopes
Preliminary Multi-Variable Parametric Cost Model for Space Telescopes H. Philip Stahl NASA MSFC, Huntsville, AL 35821; Todd Hendrichs Middle Tennessee State University; Space Telescopes and Instrumentation 2010: Optical, Infrared, and Millimeter Wave Conference, SPIE 7731, 2010 Parametric Cost Models Parametric cost models have several uses: • high level mission concept design studies, • identify major architectural cost drivers, • allow high-level design trades, • enable cost-benefit analysis for technology development investment, and • provide a basis for estimating total project cost. In the past 12 months Added JWST cost information for 2003, 2006, 2008 and 2009. Published two peer reviewed cost model papers: Stahl, H. Philip, Kyle Stephens, Todd Henrichs, Christian Smart, and Frank A. Prince, “Single Variable Parametric Cost Models for Space Telescopes”, Optical Engineering Vol.49, No.06, 2010 Stahl, H. Philip, “Survey of Cost Models for Space Telescopes”, Optical Engineering, Vol.49, No.05, 2010 Now working on developing multi-variable cost models. Objectives for Today • Review Data Collection Methodology • Define Statistical Analysis Methodology • Summarize Single Variable Results • Test Historical Models • Introduce Preliminary Multi-Variable Models Methodology Table 1: Cost Model Missions Database Data on 59 different variables X-Ray Telescopes Infrared Telescopes was acquired for 30 NASA, Chandra (AXAF) CALIPSO Einstein (HEAO-2) Herschel ESA, & commercial space ICESat telescopes using: UV/Optical Telescopes IRAS EUVE ISO • NAFCOM (NASA/ Air Force FUSE JWST Cost Model) database, GALEX SOFIA HiRISE Spitzer (SIRTF) • RSIC (Redstone Scientific HST TRACE HUT WIRE Information Center), IUE WISE Kepler • REDSTAR (Resource Data Copernicus (OAO-3) Microwave Telescopes Storage and Retrieval System), SOHO/EIT WMAP UIT • project websites, and interviews.