A New Frontiers Uranus Orbiter Mission Concept Study
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THE PLANETARY REPORT FAREWELL, SEPTEMBER EQUINOX 2017 VOLUME 37, NUMBER 3 CASSINI Planetary.Org CELEBRATING a LEGACY of DISCOVERIES
THE PLANETARY REPORT FAREWELL, SEPTEMBER EQUINOX 2017 VOLUME 37, NUMBER 3 CASSINI planetary.org CELEBRATING A LEGACY OF DISCOVERIES ATMOSPHERIC CHANGES C DYNAMIC RINGS C COMPLICATED TITAN C ACTIVE ENCELADUS ABOUT THIS ISSUE LINDA J. SPILKER is Cassini project scientist at the Jet Propulsion Laboratory. IN 2004, Cassini, the most distant planetary seafloor. As a bonus, it has revealed jets of orbiter ever launched by humanity, arrived at water vapor and ice particles shooting out of Saturn. For 13 years, through its primary and fractures at the moon’s south pole. two extended missions, this spacecraft has These discoveries have fundamentally been making astonishing discoveries, reshap- altered many of our concepts of where life ing and changing our understanding of this may be found in our solar system. Cassini’s unique planetary system within our larger observations at Enceladus and Titan have made system of unique worlds. A few months ater exploring these ocean worlds a major focus for arrival, Cassini released Huygens, European planetary science. New insights from these dis- Space Agency’s parachuted probe built to coveries also have implications for potentially study the atmosphere and surface of Titan habitable worlds beyond our solar system. and image its surface for the very first time. In this special issue of The Planetary Report, a handful of Cassini scientists share some results from their studies of Saturn and its moons. Because there’s no way to fit every- thing into this slim volume, they’ve focused on a few highlights. Meanwhile, Cassini continues performing its Grand Finale orbits between the rings and the top of Saturn’s atmosphere, circling the planet once every 6.5 days. -
Passive Microwave Radiometer Channel Selection Based on Cloud and Precipitation Information Content Estimation
475 Passive Microwave Radiometer Channel Selection Based on Cloud and Precipitation Information Content Estimation Sabatino Di Michele and Peter Bauer Research Department Submitted to Q. J. Royal Meteor. Soc. July 2005 Series: ECMWF Technical Memoranda A full list of ECMWF Publications can be found on our web site under: http://www.ecmwf.int/publications/ Contact: [email protected] c Copyright 2005 European Centre for Medium-Range Weather Forecasts Shinfield Park, Reading, RG2 9AX, England Literary and scientific copyrights belong to ECMWF and are reserved in all countries. This publication is not to be reprinted or translated in whole or in part without the written permission of the Director. Appropriate non-commercial use will normally be granted under the condition that reference is made to ECMWF. The information within this publication is given in good faith and considered to be true, but ECMWF accepts no liability for error, omission and for loss or damage arising from its use. Microwave Channel Selection from Precipitation Information Content Abstract The information content of microwave frequencies between 5 and 200 GHz for rain, snow and cloud wa- ter retrievals over ocean and land surfaces was evaluated using optimal estimation theory. The study was based on large datasets representative of summer and winter meteorological conditions over North Amer- ica, Europe, Central Africa, South America and the Atlantic obtained from short-range forecasts with the operational ECMWF model. The information content was traded off against noise that is mainly produced by geophysical variables such as surface emissivity, land surface skin temperature, atmospheric temperature and moisture. The estimation of the required error statistics was based on ECMWF model forecast error statistics. -
Juno Spacecraft Description
Juno Spacecraft Description By Bill Kurth 2012-06-01 Juno Spacecraft (ID=JNO) Description The majority of the text in this file was extracted from the Juno Mission Plan Document, S. Stephens, 29 March 2012. [JPL D-35556] Overview For most Juno experiments, data were collected by instruments on the spacecraft then relayed via the orbiter telemetry system to stations of the NASA Deep Space Network (DSN). Radio Science required the DSN for its data acquisition on the ground. The following sections provide an overview, first of the orbiter, then the science instruments, and finally the DSN ground system. Juno launched on 5 August 2011. The spacecraft uses a deltaV-EGA trajectory consisting of a two-part deep space maneuver on 30 August and 14 September 2012 followed by an Earth gravity assist on 9 October 2013 at an altitude of 559 km. Jupiter arrival is on 5 July 2016 using two 53.5-day capture orbits prior to commencing operations for a 1.3-(Earth) year-long prime mission comprising 32 high inclination, high eccentricity orbits of Jupiter. The orbit is polar (90 degree inclination) with a periapsis altitude of 4200-8000 km and a semi-major axis of 23.4 RJ (Jovian radius) giving an orbital period of 13.965 days. The primary science is acquired for approximately 6 hours centered on each periapsis although fields and particles data are acquired at low rates for the remaining apoapsis portion of each orbit. Juno is a spin-stabilized spacecraft equipped for 8 diverse science investigations plus a camera included for education and public outreach. -
IMPLEMENTATION of TRIDENT: a DISCOVERY-CLASS MISSION to TRITON. K. L. Mitchell1 , L. M. Prockter2, W. E. Frazier1, W. D. Smythe1, B
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 3200.pdf IMPLEMENTATION OF TRIDENT: A DISCOVERY-CLASS MISSION TO TRITON. K. L. Mitchell1 , L. M. Prockter2, W. E. Frazier1, W. D. Smythe1, B. M. Sutin1, D. A. Bearden1, and the Trident Team. 1Jet Propulsion Laboratory ([email protected]), Pasadena, CA 91109-8099, United States, 2Lunar and Planetary Insti- tute/USRA, Houston, TX, United States. Overview: Trident is an exciting mission concept to Why Now?: By launching during 2026, Trident investigate Neptune’s large moon Triton, an exotic can- takes advantage of a rare, efficient gravity-assist align- didate ocean world at 30 AU (Prockter et al., this meet- ment, to capitalize on a narrow – but closing – observa- ing). The concept is responsive to recommendations of tional window that enables assessment of changes in the recent NASA Roadmap to Ocean Worlds study Triton’s plume activity and surface characteristics since (Hendrix et al., 2019), and to the 2013 Planetary Deca- Voyager 2’s encounter one Neptune-Triton season ago. dal Survey’s habitability and workings themes (Squyres Conclusion: This mission design allows Trident to et al., 2011). A rare, low Δv trajectory (Fig. 1) enables accomplish a scientifically rich yet radically cost-effec- an MMRTG-powered spacecraft fitting under the Dis- tive investigation of an unusual icy world, dramatically covery cost cap. The spacecraft has a robust design and expanding the horizons of NASA’s Discovery Program. uses high heritage instruments (table 1) with minimal References: [1] Prockter L. M. et al. (2019) LPS L, development costs. -
Instruments for Earth Science Measurements
NASA SBIR 2004 Phase I Solicitation E1 Instruments for Earth Science Measurements NASA's Earth Science Enterprise (ESE) is studying how our global environment is changing. Using the unique perspective available from space and airborne platforms, NASA is observing, documenting, and assessing large- scale environmental processes with emphasis on atmospheric composition, climate, carbon cycle and ecosystems, the Earth’s surface and interior, the water and energy cycles, and weather. A major objective of the ESE instrument development programs is to implement science measurement capabilities with small or more affordable spacecraft so development programs can meet multiple mission needs and therefore, make the best use of limited resources. The rapid development of small, low cost remote sensing and in situ instruments is essential to achieving this objective. Consequently, the objective of the Instruments for Earth Science Measurements SBIR topic is to develop and demonstrate instrument component and subsystem technologies that reduce the risk, cost, size, and development time of Earth observing instruments, and enable new Earth observation measurements. The following subtopics are concomitant with this objective and are organized by measurement technique. Subtopics E1.01 Passive Optics Lead Center: LaRC Participating Center(s): ARC, GSFC The following technologies are of interest to NASA in the remote sensing subtopic “passive optics.” Passive optical remote sensing generally requires that deployed devices have large apertures and large throughput. NASA is interested primarily in instrument technologies suitable for aircraft or space flight platforms, and these inherently also prefer low mass, low power, fast measurement times, and a high degree of robustness to survive vibrations in flight or at launch. -
Chang'e 5 Samples (Mexag) (Head-Final)
Chang’E 5 Lunar Sample Return Mission Update James w. Head Department of Earth, Environmental and Planetary Sciences Brown University Providence, RI 02912 USA Extraterrestrial Materials Analysis Group (ExMAG) Spring Meeting: April 7 - 8, 2021. Extraterrestrial Materials Analysis Group (ExMAG) Spring Meeting Barbara Cohen, ExMAG Chair. 2/10/21 • 1. Please provide an update on the Chang'e 5 Sample Return Mission. • 2. What is known of the collection so far? • 3. Please provide an overview of allocation procedures. • 4. Since US federally-funded researchers cannot work directly with China - Who outside of China is working with the mission team? • 5. We'd also appreciate your thoughts on: What NASA might be able to do to enable the US analysis community to collaborate on this sample collection? Extraterrestrial Materials Analysis Group (ExMAG) Spring Meeting Barbara Cohen, ExMAG Chair. 2/10/21 • 1. Some Myths and Realities. • 2. Organization of the Chinese Space Program. • 3. Chinese Lunar Exploration Program (CLEP) context for Chang’e 5. • 4. Chang’e 5 Landing Site Selection, Global Context, Key Questions, Mission Operations and Sample Return. • 5. Returned Sample Location, Storage, Preliminary Analysis and Distribution. • 6. Opportunities for International Cooperation. Extraterrestrial Materials Analysis Group (ExMAG) Spring Meeting Barbara Cohen, ExMAG Chair. 2/10/21 • 1. Some Myths and Realities. • 2. Organization of the Chinese Space Program. • 3. Chinese Lunar Exploration Program (CLEP) context for Chang’e 5. • 4. Chang’e 5 Landing Site Selection, Global Context, Key Questions, Mission Operations and Sample Return. • 5. Returned Sample Location, Storage, Preliminary Analysis and Distribution. • 6. Opportunities for International Cooperation. -
Juno Magnetometer (MAG) Standard Product Data Record and Archive Volume Software Interface Specification
Juno Magnetometer Juno Magnetometer (MAG) Standard Product Data Record and Archive Volume Software Interface Specification Preliminary March 6, 2018 Prepared by: Jack Connerney and Patricia Lawton Juno Magnetometer MAG Standard Product Data Record and Archive Volume Software Interface Specification Preliminary March 6, 2018 Approved: John E. P. Connerney Date MAG Principal Investigator Raymond J. Walker Date PDS PPI Node Manager Concurrence: Patricia J. Lawton Date MAG Ground Data System Staff 2 Table of Contents 1 Introduction ............................................................................................................................. 1 1.1 Distribution list ................................................................................................................... 1 1.2 Document change log ......................................................................................................... 2 1.3 TBD items ........................................................................................................................... 3 1.4 Abbreviations ...................................................................................................................... 4 1.5 Glossary .............................................................................................................................. 6 1.6 Juno Mission Overview ...................................................................................................... 7 1.7 Software Interface Specification Content Overview ......................................................... -
Cubex: a Compact X-Ray Telescope Enables Both X-Ray Fluorescence Imaging Spectroscopy and Pulsar Timing Based Navigation
SSC18-V-05 CubeX: A compact X-Ray Telescope Enables both X-Ray Fluorescence Imaging Spectroscopy and Pulsar Timing Based Navigation Jan Stupl, Monica Ebert, David Mauro SGT / NASA Ames NASA Ames Research Center, Moffett Field, CA; 650-604-4032 [email protected] JaeSub Hong Harvard University Cambridge, MA Suzanne Romaine, Almus Kenter, Janet Evans, Ralph Kraft Smithsonian Astrophysical Observatory Cambridge, MA Larry Nittler Carnegie Institution of Washington Washington, DC Ian Crawford Birkbeck College London, UK David Kring Lunar and Planetary Institute Houston, TX Noah Petro, Keith. Gendreau, Jason Mitchell, Luke Winternitz NASA Goddard Space Flight Center Greenbelt, MD Rebecca. Masterson, Gregory Prigozhin Massachusetts Institute of Technology Cambridge, MA Brittany Wickizer NASA Ames Research Center Moffett Field, CA Kellen Bonner, Ashley Clark, Arwen Dave, Andres Dono-Perez, Ali Kashani, Daniel Larrabee, Samuel Montez, Karolyn Ronzano, Tim Snyder MEI / NASA Ames Research Center Joel Mueting, Laura Plice Metis / NASA Ames Research Center NASA Ames Research Center, Moffett Field, CA Yueh-Liang Shen, Duy Nguyen Booz Allen Hamilton / NASA Ames NASA Ames Research Center, Moffett Field, CA Stupl 1 32nd Annual AIAA/USU Conference on Small Satellites ABSTRACT This paper describes the miniaturized X-ray telescope payload, CubeX, in the context of a lunar mission. The first part describes the payload in detail, the second part summarizes a small satellite mission concept that utilizes its compact form factor and performance. This instrument can be used for both X-ray fluorescence (XRF) imaging spectroscopy and X-ray pulsar timing-based navigation (XNAV). It combines high angular resolution (<1 arcminutes) Miniature Wolter-I X-ray optics (MiXO) with a common focal plane consisting of high spectral resolution (<150 eV at 1 keV) CMOS X-ray sensors and a high timing resolution (< 1 µsec) SDD X-ray sensor. -
N€WS 'RELEASE NATIONAL AERONAUTICS and SPACE Admln ISTRATION 400 MARYLAND AVENUE, SW, WASHINGTON 25, D.C
https://ntrs.nasa.gov/search.jsp?R=19630002483 2020-03-11T16:50:02+00:00Z b " N€WS 'RELEASE NATIONAL AERONAUTICS AND SPACE ADMlN ISTRATION 400 MARYLAND AVENUE, SW, WASHINGTON 25, D.C. TELEPHONES WORTH 2-4155-WORTH. 3-1110 RELEASE NO. 62-182 MARINER SPACECRAFT Mariner 2, the second of a series of spacecraft designed for planetary exploration,- will be launched within a few days (no earlier than August 17) from the Atlantic Missile Range, Cape Canaveral, Florida, by the National Aeronautics and Space Administration. Mariner 1, launched at 4:21 a.m. (EST) on July 22, 1962 from AMR, was destroyed by the Range Safety Officer after about 290 seconds of flight because of a deviation from the planned flight path. Measures have been taken to correct the difficulties experienced in the Mariner 1 launch. These measures include a more rigorous checkout of the Atlas rate beacon and revision of the data editing equation. The data editing equation Is designed as a guard against acceptance of faulty databy the ground guidance equipment. The Mariner 2 spacecraft and its mission are identical to the first Mariner. Mariner 2 will carry six experiments. Two of these instruments, infrared and microwave radiometers, will make measurements at close range as Mariner 2 flys by Venus and communicate this in€ormation over an interplanetary distance of 36 million miles, Four other experiments on the spacecraft -- a magnetometer, ion chamber and particle flux detector, cosmic dust detector and solar plasma spectrometer -- will gather Information on interplantetary phenomena during the trip to Venus and in the vicinity of the planet. -
OCEANUS (Organisms and Compounds of Europa – an Analysis Under the Surface) – Concept Mission De- Sign
49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083) 1871.pdf OCEANUS (Organisms and Compounds of Europa – an Analysis Under the Surface) – Concept Mission De- sign. M.V. Heemskerk1, G. de Zeeuw1, W. van Westrenen1, B. H. Foing1,2. 1VU University Amsterdam, de Boelelaan 1105, 1081 HZ Amsterdam, The Netherlands, ([email protected], [email protected], [email protected]) 2ESA ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands ([email protected]) Introduction: 1. Buildup of the ice crust and its ocean; Un- In 2022, ESA (European Space Agency) will launch derstanding how recent and/or current tidal an orbiter – JUICE (JUpiter ICy moon Explorer) – and geological processes are formed. which will collect atmospheric data of Jupiter and 2. Chemical composition; Characterizing the three of its Galilean moons; Ganymede, Europa and properties of the ocean and its crust to de- Callisto [1]. As this is but an orbiter, further explora- scry the origin of organic compounds. tion of the (sub)surface remains out of reach. As of 3. Geomorphology; Understanding the for- today, the most suitable prospect for the occurrence of extra-terrestrial life forms appears to be Europa. mation of surface features Europa contains liquid water [2], simple organic B. Model Instrument Payload: The lander payload compounds [3], a subsurface power source [4] and a consists of two high-definition reconnaissance camer- lot of ice. Convection and tidal flexure could also as, a magnetometer, an altimeter, a short-wave infra- give way to a possible zone for the emergence of life, red spectrometer, a gamma and X-ray detector, a ra- for the bottom of this subsurface ocean may house diation shielding, the ESS, and the ECMD. -
Operating Segments
OPERATING SEGMENTS Commercial Aircraft OEM Defense $ 399.6 M $ 183.6 M Commercial Business Aircraft Jets Aftermarket $ 38.6 M $ 113.1 M Military Military Aircraft Space Aircraft Aftermarket $ 182.5 M OEM $ 199.6 M $ 312.8 M FY 2016 SALES FY 2016 SALES $1,063.7 M $366.1 M AIRCRAFT CONTROLS SPACE AND DEFENSE • State-of-the-art technology in flight controls, engine controls, door drive controls, active • Multi-tier provider capable of components, systems and prime level integration vibration controls and engineered components • Thrust vector control actuation systems, avionics, propulsion controls and structures for • Complete flight control system design and integration capability missiles and launch vehicles • World-class manufacturing facilities and skilled, experienced, team-based workforce • Liquid rocket engines, tanks, chemical and electric propulsion systems, subsystems • Focused, highly-responsive global aftermarket support organization and components for spacecraft and launch vehicles • Satellite integrated avionics, solar array drives, antenna pointing mechanisms and Military Aircraft: vibration isolation systems • F-35, F-15, F/A-18E/F, EA-18G, F-16, KC-46, A400M, Korea T-50, C-27J, C-295, • Fin actuation systems, divert and attitude control components for missiles and CN-235, Eurofighter-Typhoon, JAS 39, India LCA, Japan XC-2, XP-1, Hawk AJT, M346 interceptors Commercial Airplanes: • Weapon Stores Management Systems (SMS) for the deployment of missiles, guns and rockets • Boeing 737, 747, 767, 777, 787 • Motion control systems -
Planetary Science
Mission Directorate: Science Theme: Planetary Science Theme Overview Planetary Science is a grand human enterprise that seeks to discover the nature and origin of the celestial bodies among which we live, and to explore whether life exists beyond Earth. The scientific imperative for Planetary Science, the quest to understand our origins, is universal. How did we get here? Are we alone? What does the future hold? These overarching questions lead to more focused, fundamental science questions about our solar system: How did the Sun's family of planets, satellites, and minor bodies originate and evolve? What are the characteristics of the solar system that lead to habitable environments? How and where could life begin and evolve in the solar system? What are the characteristics of small bodies and planetary environments and what potential hazards or resources do they hold? To address these science questions, NASA relies on various flight missions, research and analysis (R&A) and technology development. There are seven programs within the Planetary Science Theme: R&A, Lunar Quest, Discovery, New Frontiers, Mars Exploration, Outer Planets, and Technology. R&A supports two operating missions with international partners (Rosetta and Hayabusa), as well as sample curation, data archiving, dissemination and analysis, and Near Earth Object Observations. The Lunar Quest Program consists of small robotic spacecraft missions, Missions of Opportunity, Lunar Science Institute, and R&A. Discovery has two spacecraft in prime mission operations (MESSENGER and Dawn), an instrument operating on an ESA Mars Express mission (ASPERA-3), a mission in its development phase (GRAIL), three Missions of Opportunities (M3, Strofio, and LaRa), and three investigations using re-purposed spacecraft: EPOCh and DIXI hosted on the Deep Impact spacecraft and NExT hosted on the Stardust spacecraft.