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Differences in Energy and Nutritional Content of Menu Items Served By
RESEARCH ARTICLE Differences in energy and nutritional content of menu items served by popular UK chain restaurants with versus without voluntary menu labelling: A cross-sectional study ☯ ☯ Dolly R. Z. TheisID *, Jean AdamsID Centre for Diet and Activity Research, MRC Epidemiology Unit, University of Cambridge, Cambridge, United a1111111111 Kingdom a1111111111 ☯ These authors contributed equally to this work. a1111111111 * [email protected] a1111111111 a1111111111 Abstract Background OPEN ACCESS Poor diet is a leading driver of obesity and morbidity. One possible contributor is increased Citation: Theis DRZ, Adams J (2019) Differences consumption of foods from out of home establishments, which tend to be high in energy den- in energy and nutritional content of menu items sity and portion size. A number of out of home establishments voluntarily provide consumers served by popular UK chain restaurants with with nutritional information through menu labelling. The aim of this study was to determine versus without voluntary menu labelling: A cross- whether there are differences in the energy and nutritional content of menu items served by sectional study. PLoS ONE 14(10): e0222773. https://doi.org/10.1371/journal.pone.0222773 popular UK restaurants with versus without voluntary menu labelling. Editor: Zhifeng Gao, University of Florida, UNITED STATES Methods and findings Received: February 8, 2019 We identified the 100 most popular UK restaurant chains by sales and searched their web- sites for energy and nutritional information on items served in March-April 2018. We estab- Accepted: September 6, 2019 lished whether or not restaurants provided voluntary menu labelling by telephoning head Published: October 16, 2019 offices, visiting outlets and sourcing up-to-date copies of menus. -
Lunar Space Elevator Infrastructure
Lunar Space Elevator Infrastructure A Cost Saving Approach to Human Spaceflight within a 15-year Constrained NASA Budget White Paper Submitted at the Open Invitation of the National Research Council 2013 Lunar Space Elevator Infrastructure In Response to the National Research Council’s Study on the Benefits, Challenges and Ramifications of America’s Human Spaceflight Program. LiftPort Group presents a Cost-Effective Approach to Human Spaceflight within a 15-year Constrained NASA Budget. | MICHAEL LAINE – PRESIDENT, LIFTPORT GROUP | CHARLES RADLEY MSC., – ADVISOR, LIFTPORT GROUP | MARSHALL EUBANKS MSC., – ADVISOR, LIFTPORT GROUP | JEROME PEARSON MSC., – ADVISOR, LIFTPORT GROUP | PETER SWAN PHD., – ADVISOR, LIFTPORT GROUP | LEE GRAHAM (NASA – HIS VIEWS DO NOT REFLECT HIS EMPLOYER) | | 8 JULY 2013 | LIFTPORT GROUP | 1307 Dogwood Hill RD SW, Port Orchard, WA, 98366 | www.liftport.com | (862) 438-5383 | [email protected] LiftPort’s Lunar Space Elevator Infrastructure: Affordable Response to Human Spaceflight What are the important benefits provided to the United States and other countries by human spaceflight endeavors? The ability to place humans in space is exciting to the public, and demonstrates the technological maturity and stature of each spacefaring nation. Such a visible and peaceful demonstration of cutting edge technology fosters foreign policy by showing Page | 1 strength without engaging in conflicti. Human spaceflight sparks the imagination and serves an instinctive need to explore. Astronauts are ambassadors for all of humanity in a very personal way. Men and women in space suits inspire people – of all cultures and demographics – to achieve excellence, to believe in a common cause and to pursue a noble goal. -
Mary Holy Mother Of
Pastor Reverend Don H. Bender Parochial Vicar/Campus Minister Saint Patrick Church Reverend Tiburtius Antony Raja Reverend Gregory D’Emma, Retired Parish Manager Parish Office George Ehgartner (717) 243-4411, ext. 201 152 East Pomfret Street Principal, Saint Patrick School Carlisle, PA 17013 Antoinette Oliverio (717) 249-4826 Office Hours: Parish Financial Manager Heather Hall (717) 243-4411, ext. 202 9:00 a.m. to 4:00 p.m. Pastoral Associate Monday-Friday Heidi Lynch (717) 243-4411, ext. 203 717-243-4411 Parish Office Manager Fax: 717-258-9281 Star Wiskeman (717) 243-4411, ext. 200 www.saintpatrickchurch.org Director of Music Saint Patrick Shrine Church Saint Patrick Marsh Drive Church Dr. David O’Donnell 152 East Pomfret Street 85 Marsh Drive, (717) 243-4411, 204 Carlisle, PA 17013 Carlisle, PA 17015 Director of Religious Education Maggie Gruschow (717) 243-4891, ext. 300 www.saintpatrickchurch.org Youth Ministry Coordinator Heather Howie (717-243-4411, ext. 205 Daily Mass Schedule Sunday Mass Schedule Adult Faith Formation Coordinator Pomfret Street Church Marsh Drive Church Gail Chaudrue (717) 243-4891, ext. 302 Monday and Saturday - 8:30 a.m. Saturday, 5:15 PM Parish Facilities/Scheduling Manager Tuesday, Wednesday, Thursday - 6:45 a.m. Sunday, 9:00 a.m. 11:00 a.m., 5:00 p.m. Robin Lees (717)-243-4411, ext. 207 Friday - Marsh Drive - 8:30 a.m. Pomfret Street - 8:00 AM Special Projects Coordinator/ (during the school year) Interim Cemetery Manager Steve Mellen (717) 243-4411, ext. 509 Sacrament of Penance Saturday, 4:00-5:00 p.m. -
National Retailer & Restaurant Expansion Guide Spring 2016
National Retailer & Restaurant Expansion Guide Spring 2016 Retailer Expansion Guide Spring 2016 National Retailer & Restaurant Expansion Guide Spring 2016 >> CLICK BELOW TO JUMP TO SECTION DISCOUNTER/ APPAREL BEAUTY SUPPLIES DOLLAR STORE OFFICE SUPPLIES SPORTING GOODS SUPERMARKET/ ACTIVE BEVERAGES DRUGSTORE PET/FARM GROCERY/ SPORTSWEAR HYPERMARKET CHILDREN’S BOOKS ENTERTAINMENT RESTAURANT BAKERY/BAGELS/ FINANCIAL FAMILY CARDS/GIFTS BREAKFAST/CAFE/ SERVICES DONUTS MEN’S CELLULAR HEALTH/ COFFEE/TEA FITNESS/NUTRITION SHOES CONSIGNMENT/ HOME RELATED FAST FOOD PAWN/THRIFT SPECIALTY CONSUMER FURNITURE/ FOOD/BEVERAGE ELECTRONICS FURNISHINGS SPECIALTY CONVENIENCE STORE/ FAMILY WOMEN’S GAS STATIONS HARDWARE CRAFTS/HOBBIES/ AUTOMOTIVE JEWELRY WITH LIQUOR TOYS BEAUTY SALONS/ DEPARTMENT MISCELLANEOUS SPAS STORE RETAIL 2 Retailer Expansion Guide Spring 2016 APPAREL: ACTIVE SPORTSWEAR 2016 2017 CURRENT PROJECTED PROJECTED MINMUM MAXIMUM RETAILER STORES STORES IN STORES IN SQUARE SQUARE SUMMARY OF EXPANSION 12 MONTHS 12 MONTHS FEET FEET Athleta 46 23 46 4,000 5,000 Nationally Bikini Village 51 2 4 1,400 1,600 Nationally Billabong 29 5 10 2,500 3,500 West Body & beach 10 1 2 1,300 1,800 Nationally Champs Sports 536 1 2 2,500 5,400 Nationally Change of Scandinavia 15 1 2 1,200 1,800 Nationally City Gear 130 15 15 4,000 5,000 Midwest, South D-TOX.com 7 2 4 1,200 1,700 Nationally Empire 8 2 4 8,000 10,000 Nationally Everything But Water 72 2 4 1,000 5,000 Nationally Free People 86 1 2 2,500 3,000 Nationally Fresh Produce Sportswear 37 5 10 2,000 3,000 CA -
Modular Spacecraft with Integrated Structural Electrodynamic Propulsion
NAS5-03110-07605-003-050 Modular Spacecraft with Integrated Structural Electrodynamic Propulsion Nestor R. Voronka, Robert P. Hoyt, Jeff Slostad, Brian E. Gilchrist (UMich/EDA), Keith Fuhrhop (UMich) Tethers Unlimited, Inc. 11807 N. Creek Pkwy S., Suite B-102 Bothell, WA 98011 Period of Performance: 1 September 2005 through 30 April 2006 Report Date: 1 May 2006 Phase I Final Report Contract: NAS5-03110 Subaward: 07605-003-050 Prepared for: NASA Institute for Advanced Concepts Universities Space Research Association Atlanta, GA 30308 NAS5-03110-07605-003-050 TABLE OF CONTENTS TABLE OF CONTENTS.............................................................................................................................................1 TABLE OF FIGURES.................................................................................................................................................2 I. PHASE I SUMMARY ........................................................................................................................................4 I.A. INTRODUCTION .............................................................................................................................................4 I.B. MOTIVATION .................................................................................................................................................4 I.C. ELECTRODYNAMIC PROPULSION...................................................................................................................5 I.D. INTEGRATED STRUCTURAL -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
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W, A. PaVJ-.:s VA -r,&2._~L NATIONAL ACADEMIES OF SCIENCE AND ENGINEERING NATIONAL RESEARCH COUNCIL of the UNITED STATES OF AMERICA UNITED STATES NATIONAL COMMITTEE International Union of Radio Science, National Radio Science Meeting 5-8 January 1993 Sponsored by USNC/URSI in cooperation with Institute of Electrical and Electronics Engineers University of Colorado Boulder, Colorado U.S.A. National Radio Science Meeting 5-8 January 1993 Condensed Technical Program Monday, 4 January 2000-2400 USNC-URSI Meeting Broker Inn Tuesday, 5 January 0835-1200 B-1 ANTENNAS CRZ-28 0855-1200 A-1 MICROWAVE MEASUREMENTS CRl-46 D-1 MICROWAVE, QUASisOPTICAL, AND ELECTROOPTICAL DEVICES CRl-9 G-1 COORDINATED CAMPAIGNS AND ACTIVE EXPERIMENTS CR0-30 J/H-1 RADIO AND RADAR ASTRONOMY OF THE SOLAR SYSTEM CRZ-26 1335-1700 B-2 SCATIERING CR2-28 F-1 SENSING OF ATMOSPHERE AND OCEAN CRZ-6 G-2 IONOSPHERIC PROPAGATION CHANNEL CR0-30 J/H-2 RADIO AND RADAR ASTRONOMY OF THE SOLAR SYSTEM CR2-26 1355-1700 A-2 EM FIELD MEASUREMENTS CRl-46 D-2 OPTOELECTRONICS DEVICES AND APPLICATION CRl-9 1700-1800 Commission A Business Meeting CRl-46 Commission C Business Meeting CRl-40 Commission D Business Meeting CRl-9 Commission G Business Meeting CR0-30 Wednesday, 6 January 0815-1200 PLENARY SESSION MATH 100 1335-1700 B-3 EM THEORY CRZ-28 D-3 MICROWAVE AND MILLIMETER AND RELATED DEVICES CRl-9 F-2 PROPAGATION MODELING AND SCATTERING CRZ-6 H-1 PLASMA WAYES IN THE IONOSPHERE AND THE MAGNETOSPHERE CRl-42 J-1 FIBER OPTICS IN RADIO ASTRONOMY CR2-26 1355-1700 E-1 HIGH POWER ELECTROMAGNETICS (HPE) AND INTERFERENCE PROBLEMS CRl-40 United States National Committee INTERNATIONAL UNION OF RADIO SCIENCE PROGRAM AND ABSTRACTS National Radio Science Meeting 5-8 January 1993 Sponsored by USNC/URSI in cooperation with IEEE groups and societies: Antennas and Propagation Circuits and Systems Communications Electromagnetic Compatibility Geoscience Electronics Information Theory ,. -
1998 Year in Review
Associate Administrator for Commercial Space Transportation (AST) January 1999 COMMERCIAL SPACE TRANSPORTATION: 1998 YEAR IN REVIEW Cover Photo Credits (from left): International Launch Services (1998). Image is of the Atlas 2AS launch on June 18, 1998, from Cape Canaveral Air Station. It successfully orbited the Intelsat 805 communications satellite for Intelsat. Boeing Corporation (1998). Image is of the Delta 2 7920 launch on September 8, 1998, from Vandenberg Air Force Base. It successfully orbited five Iridium communications satellites for Iridium LLP. Lockheed Martin Corporation (1998). Image is of the Athena 2 awaiting its maiden launch on January 6, 1998, from Spaceport Florida. It successfully deployed the NASA Lunar Prospector. Orbital Sciences Corporation (1998). Image is of the Taurus 1 launch from Vandenberg Air Force Base on February 10, 1998. It successfully orbited the Geosat Follow-On 1 military remote sensing satellite for the Department of Defense, two Orbcomm satellites and the Celestis 2 funerary payload for Celestis Corporation. Orbital Sciences Corporation (1998). Image is of the Pegasus XL launch on December 5, 1998, from Vandenberg Air Force Base. It successfully orbited the Sub-millimeter Wave Astronomy Satellite for the Smithsonian Astrophysical Observatory. 1998 YEAR IN REVIEW INTRODUCTION INTRODUCTION In 1998, U.S. launch service providers conducted In addition, 1998 saw continuing demand for 22 launches licensed by the Federal Aviation launches to deploy the world’s first low Earth Administration (FAA), an increase of 29 percent orbit (LEO) communication systems. In 1998, over the 17 launches conducted in 1997. Of there were 17 commercial launches to LEO, 14 these 22, 17 were for commercial or international of which were for the Iridium, Globalstar, and customers, resulting in a 47 percent share of the Orbcomm LEO communications constellations. -
Asteroid Retrieval Feasibility Study
Asteroid Retrieval Feasibility Study 2 April 2012 Prepared for the: Keck Institute for Space Studies California Institute of Technology Jet Propulsion Laboratory Pasadena, California 1 2 Authors and Study Participants NAME Organization E-Mail Signature John Brophy Co-Leader / NASA JPL / Caltech [email protected] Fred Culick Co-Leader / Caltech [email protected] Co -Leader / The Planetary Louis Friedman [email protected] Society Carlton Allen NASA JSC [email protected] David Baughman Naval Postgraduate School [email protected] NASA ARC/Carnegie Mellon Julie Bellerose [email protected] University Bruce Betts The Planetary Society [email protected] Mike Brown Caltech [email protected] Michael Busch UCLA [email protected] John Casani NASA JPL [email protected] Marcello Coradini ESA [email protected] John Dankanich NASA GRC [email protected] Paul Dimotakis Caltech [email protected] Harvard -Smithsonian Center for Martin Elvis [email protected] Astrophysics Ian Garrick-Bethel UCSC [email protected] Bob Gershman NASA JPL [email protected] Florida Institute for Human and Tom Jones [email protected] Machine Cognition Damon Landau NASA JPL [email protected] Chris Lewicki Arkyd Astronautics [email protected] John Lewis University of Arizona [email protected] Pedro Llanos USC [email protected] Mark Lupisella NASA GSFC [email protected] Dan Mazanek NASA LaRC [email protected] Prakhar Mehrotra Caltech [email protected] -
Integrated Lunar Transportation System
Integrated Lunar Transportation System Jerome Pearson1, John C. Oldson2, Eugene M. Levin3, and Harry Wykes4 Star Technology and Research, Inc., Mount Pleasant, SC, 29466 An integrated transportation system is proposed from the lunar poles to Earth orbit, using solar-powered electric vehicles on lunar tramways, highways, and a lunar space elevator. The system could transport large amounts of lunar resources to Earth orbit for construction, radiation shielding, and propellant depots, and could supply lunar equatorial, polar, and mining bases with manufactured items. We present a system for lunar surface transport using “cars, trucks, and trains,” and the infrastructure of “roads, highways, and tramways,” connecting with the lunar space elevator for transport to Earth orbit. The Apollo Lunar Rovers demonstrated a battery- powered range of nearly 50 kilometers, but they also uncovered the problems of lunar dust. For building dustless highways, it appears particularly attractive to create paved roads by using microwaves to sinter lunar dust into a hard surface. For tramways, tall towers can support high- strength ribbons that carry cable cars over the lunar craters; the ribbon might even be fabricated from lunar materials. We address the power and energy storage requirements for lunar transportation vehicles, the design and effectiveness of lunar tramways, and the materials requirements for the support ribbons of lunar tramways and lunar space elevators. 1. Introduction NASA is implementing a plan for a return to the Moon, which will build on and expand the capabilities demonstrated during the Apollo landings. The plan includes long-duration lunar stays, lunar outposts and bases, and exploitation of lunar resources on the Moon and in Earth orbit1. -
Pathways to Colonization David V
Pathways To Colonization David V. Smitherman, Jr. NASA, Marshall Space F’light Center, Mail CoLFDO2, Huntsville, AL 35812,256-961-7585, Abstract. The steps required for space colonization are many to grow fiom our current 3-person International Space Station,now under construction, to an inhstmcture that can support hundreds and eventually thousands of people in space. This paper will summarize the author’s fmdings fiom numerous studies and workshops on related subjects and identify some of the critical next steps toward space colonization. Findings will be drawn from the author’s previous work on space colony design, space infirastructure workshops, and various studies that addressed space policy. In cmclusion, this paper will note that siBnifcant progress has been made on space facility construction through the International Space Station program, and that si&icant efforts are needed in the development of new reusable Earth to Orbit transportation systems. The next key steps will include reusable in space transportation systems supported by in space propellant depots, the continued development of inflatable habitat and space elevator technologies, and the resolution of policy issues that will establish a future vision for space development A PATH TO SPACE COLONIZATION In 1993, as part of the author’s duties as a space program planner at the NASA Marshall Space Flight Center, a lengthy timeline was begun to determine the approximate length of time it might take for humans to eventually leave this solar system and travel to the stars. The thought was that we would soon discover a blue planet around another star and would eventually seek to send a colony to explore and expand our presence in this galaxy. -
1 Using Eletrodynamic Tethers to Perform Station
USING ELETRODYNAMIC TETHERS TO PERFORM STATION-KEEPING MANEUVERS IN LEO SATELLITES Thais Carneiro Oliveira(1), and Antonio Fernando Bertachini de Almeida Prado(2) (1)(2) National Institute for Space Research (INPE), Av. dos Astronautas 1758 São José dos Campos – SP – Brazil ZIP code 12227-010,+55 12 32086000, [email protected] and [email protected] Abstract: This paper analyses the concept of using an electrodynamic tether to provide propulsion to a space system with an electric power supply and no fuel consumption. The present work is focused on orbit maintenance and on re-boost maneuvers for tethered satellite systems. The analyses of the results will be performed with the help of a practical tool called “Perturbation Integrals” and an orbit integrator that can include many external perturbations, like atmospheric drag, solar radiation pressure and luni-solar perturbation. Keywords: Electromagnetic Tether, Station-Keeping Maneuver, Orbital Maneuver, Tether Systems, Disturbing Forces. 1. Introduction Space tether is a promising and innovating field of study, and many articles, technical reports, books and even missions have used this concept through the recent decades. An overview of the space tethered flight tests missions includes the Gemini tether experiments, the OEDIPUS flights, the TSS-1 experiments, the SEDS flights, the PMG, TiPs, ATEx missions, etc [1-6]. This paper analyses the potential of using an electrodynamic tether to provide propulsion to a space system with an electric power supply and no fuel consumption. The present work is focused on orbit maintenance and re-boosts maneuvers for tethered satellite systems (TSS). This type of system consists of two or more satellites orbiting around a planet linked by a cable or a tether [7].