Proton Mission Planner's Guide (PMPG)
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Annotated List of Works Cited Primary Sources Newspapers “Apollo 11 se Vraci na Zemi.” Rude Pravo [Czechoslovakia] 22 July 1969. 1. Print. This was helpful for us because it showed how the U.S. wasn’t the only ones effected by this event. This added more to our project so we had views from outside the US. Barbuor, John. “Alunizaron, Bajaron, Caminaron, Trabajaron: Proeza Lograda.” Excelsior [Mexico] 21 July 1969. 1. Print. The front page of this newspaper was extremely helpful to our project because we used it to see how this event impacted the whole world not just America. Beloff, Nora. “The Space Race: Experts Not Keen on Getting a Man on the Moon.” Age [Melbourne] 24 April 1962. 2. Print. This was an incredibly important article to use in out presentation so that we could see different opinions. This article talked about how some people did not want to go to the moon; we didn’t find many articles like this one. In most everything we have read it talks about the advantages of going to the moon. This is why this article was so unique and important. Canadian Press. “Half-billion Watch the Moon Spectacular.” Gazette [Montreal] 21 July 1969. 4. Print. This source gave us a clear idea about how big this event really was, not only was it a big deal in America, but everywhere else in the world. This article told how Russia and China didn’t have TV’s so they had to find other ways to hear about this event like listening to the radio. -
Space Launch System (Sls) Motors
Propulsion Products Catalog SPACE LAUNCH SYSTEM (SLS) MOTORS For NASA’s Space Launch System (SLS), Northrop Grumman manufactures the five-segment SLS heavy- lift boosters, the booster separation motors (BSM), and the Launch Abort System’s (LAS) launch abort motor and attitude control motor. The SLS five-segment booster is the largest solid rocket motor ever built for flight. The SLS booster shares some design heritage with flight-proven four-segment space shuttle reusable solid rocket motors (RSRM), but generates 20 percent greater average thrust and 24 percent greater total impulse. While space shuttle RSRM production has ended, sustained booster production for SLS helps provide cost savings and access to reliable material sources. Designed to push the spent RSRMs safely away from the space shuttle, Northrop Grumman BSMs were rigorously qualified for human space flight and successfully used on the last fifteen space shuttle missions. These same motors are a critical part of NASA’s SLS. Four BSMs are installed in the forward frustum of each five-segment booster and four are installed in the aft skirt, for a total of 16 BSMs per launch. The launch abort motor is an integral part of NASA’s LAS. The LAS is designed to safely pull the Orion crew module away from the SLS launch vehicle in the event of an emergency on the launch pad or during ascent. Northrop Grumman is on contract to Lockheed Martin to build the abort motor and attitude control motor—Lockheed is the prime contractor for building the Orion Multi-Purpose Crew Vehicle designed for use on NASA’s SLS. -
Measurements of Π , K , P and ¯P Spectra in Proton-Proton
EUROPEAN ORGANISATION FOR NUCLEAR RESEARCH (CERN) Submitted to: Eur. Phys. J. C CERN-EP-2017-066 September 28, 2017 Measurements of π±,K±, p and ¯p spectra in proton-proton interactions at 20, 31, 40, 80 and 158 GeV=c with the NA61/SHINE spectrometer at the CERN SPS The NA61/SHINE Collaboration Measurements of inclusive spectra and mean multiplicities of π±,K±, p and p¯ produced in =c inelasticp p+p interactions at incident projectile momenta of 20, 31, 40, 80 and 158 GeV ( s = 6.3, 7.7, 8.8, 12.3 and 17.3 GeV, respectively) were performed at the CERN Super Proton Synchrotron using the large acceptance NA61/SHINE hadron spectrometer. Spectra are presented as function of rapidity and transverse momentum and are compared to predictions of current models. The measurements serve as the baseline in the NA61/SHINE study of the properties of the onset of deconfinement and search for the critical point of strongly interacting matter. arXiv:1705.02467v2 [nucl-ex] 27 Sep 2017 © 2017 CERN for the benefit of the NA61/SHINE Collaboration. Reproduction of this article or parts of it is allowed as specified in the CC-BY-4.0 license. 1. Introduction This paper presents experimental results on inclusive spectra and mean multiplicities of π±,K±, p and p¯ produced in inelastic p+p interactions at 20, 31, 40, 80 and 158 GeV=c. The measurements were performed by the multi-purpose NA61/SHINE experiment [1, 2] at the CERN Super Proton Synchrotron (SPS). The new measurements complement previously published results from the same datasets on π− production [3] obtained without particle identification as well as on fluctuations of charged particles [4]. -
Paper Session IA-Shuttle-C Heavy-Lift Vehicle of the 90'S
The Space Congress® Proceedings 1989 (26th) Space - The New Generation Apr 25th, 2:00 PM Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's Robert G. Eudy Manager, Shuttle-C Task Team, Marshall Space Flight Center Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Eudy, Robert G., "Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's" (1989). The Space Congress® Proceedings. 5. https://commons.erau.edu/space-congress-proceedings/proceedings-1989-26th/april-25-1989/5 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. SHUTTLE-C HEAVY-LIFT VEHICLE OF THE 90 ' S Mr. Robert G. Eudy, Manager Shuttle-C Task Team Marshall Space Flight Center ABSTRACT United States current and planned space activities identify the need for increased payload capacity and unmanned flight to complement the existing Shuttle. To meet this challenge the National Aeronautics and Space Administration is defining an unmanned cargo version of the Shuttle that can give the nation early heavy-lift capability. Called Shuttle-C, this unmanned vehicle is a natural, low-cost evolution of the current Space Shuttle that can be flying 100,000 to 170,000 pound payloads by late 1994. At the core of Shuttle-C design philosophy is the principle of evolvement from the United State's Space Transportation System. -
View / Download
www.arianespace.com www.starsem.com www.avio Arianespace’s eighth launch of 2021 with the fifth Soyuz of the year will place its satellite passengers into low Earth orbit. The launcher will be carrying a total payload of approximately 5 518 kg. The launch will be performed from Baikonur, in Kazakhstan. MISSION DESCRIPTION 2 ONEWEB SATELLITES 3 Liftoff is planned on at exactly: SOYUZ LAUNCHER 4 06:23 p.m. Washington, D.C. time, 10:23 p.m. Universal time (UTC), LAUNCH CAMPAIGN 4 00:23 a.m. Paris time, FLIGHT SEQUENCES 5 01:23 a.m. Moscow time, 03:23 a.m. Baikonur Cosmodrome. STAKEHOLDERS OF A LAUNCH 6 The nominal duration of the mission (from liftoff to separation of the satellites) is: 3 hours and 45 minutes. Satellites: OneWeb satellite #255 to #288 Customer: OneWeb • Altitude at separation: 450 km Cyrielle BOUJU • Inclination: 84.7degrees [email protected] +33 (0)6 32 65 97 48 RUAG Space AB (Linköping, Sweden) is the prime contractor in charge of development and production of the dispenser system used on Flight ST34. It will carry the satellites during their flight to low Earth orbit and then release them into space. The dedicated dispenser is designed to Flight ST34, the 29th commercial mission from the Baikonur Cosmodrome in Kazakhstan performed by accommodate up to 36 spacecraft per launch, allowing Arianespace and its Starsem affiliate, will put 34 of OneWeb’s satellites bringing the total fleet to 288 satellites Arianespace to timely deliver the lion’s share of the initial into a near-polar orbit at an altitude of 450 kilometers. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
GLONASS Spacecraft
INNO V AT IO N The task of designing and developing the GLONASS GLONASS spacecraft fell to the Scientific Production Association of Applied Mechan ics (Nauchno Proizvodstvennoe Ob"edinenie Spacecraft Prikladnoi Mekaniki or NPO PM) , located near Krasnoyarsk in Siberia. This major aero Nicholas L. Johnson space industrial complex was established in 1959 as a division of Sergei Korolev 's Kaman Sciences Corporation Expe1imental Design Bureau (Opytno Kon struktorskoe Byuro or OKB). (Korolev , among other notable achievements , led the Fourteen years after the launch of the effort to develop the Soviet Union's first first test spacecraft, the Russian Global Nav launch vehicle - the A launcher - which igation Satellite System (Global 'naya Navi placed Sputnik 1 into orbit.) The founding gatsionnaya Sputnikovaya Sistema or and current general director and chief GLONASS) program remains viable and designer is Mikhail Fyodorovich Reshetnev, essentially on schedule despite the economic one of only two still-active chief designers and political turmoil surrounding the final from Russia's fledgling 1950s-era space years of the Soviet Union and the emergence program. of the Commonwealth of Independent States A closed facility until the early 1990s, (CIS). By the summer of 1994, a total of 53 NPO PM has been responsible for all major GLONASS spacecraft had been successfully Russian operational communications, navi Despite the significant economic hardships deployed in nearly semisynchronous orbits; gation, and geodetic satellite systems to associated with the breakup of the Soviet Union of the 53 , nearly 12 had been normally oper date. Serial (or assembly-line) production of and the transition to a modern market economy, ational since the establishment of the Phase I some spacecraft, including Tsikada and Russia continues to develop its space programs, constellation in 1990. -
Using Energia (Arduino)
Using Energia (Arduino) Introduction This chapter of the MSP430 workshop explores Energia, the Arduino port for the Texas Instruments Launchpad kits. After a quick definition and history of Arduino and Energia, we provide a quick introduction to Wiring – the language/library used by Arduino & Energia. Most of the learning comes from using the Launchpad board along with the Energia IDE to light LED’s, read switches and communicate with your PC via the serial connection. Learning Objectives, Requirements, Prereq’s Prerequisites & Objectives Prerequisites Basic knowledge of C language Basic understanding of using a C library and header files This chapter doesn’t explain clock, interrupt, and GPIO features in detail, this is left to the other chapters in the MSP430 workshop Requirements - Tools and Software Hardware Windows (XP, 7, 8) PC with available USB port MSP430F5529 Launchpad Software Already installed, if you Energia Download have installed CCSv5.x Launchpad drivers (Optional) MSP430ware / Driverlib Objectives Define ‘Arduino’ and describe what is was created for Define ‘Energia’ and explain what it is ‘forked’ from Install Energia, open and run included example sketches Use serial communication between the board & PC Add an external interrupt to an Energia sketch Modify CPU registers from an Energia sketch MSP430 Workshop - Using Energia (Arduino) 8 - 1 What is Arduino Chapter Topics Using Energia (Arduino) ............................................................................................................ -
Human Spaceflight Plans of Russia, China and India
Presentation to the ASEB Committee on NASA Technology Roadmaps Panel on Human Health and Surface Exploration June 1, 2011 by Marcia S. Smith Space and Technology Policy Group, LLC Russia Extensive experience in human spaceflight First animal in space (1957), first man in space (1961), first woman in space (1963), first spacewalk (1965), first space station (1971) Seven successful space stations (Salyut 1, 3, 4, 5, 6, 7 and Mir) before partnering in International Space Station (ISS) No people beyond low Earth orbit (LEO), however For earth orbit, continues to rely on Soyuz, first launched in 1967, but upgraded many times and is key to ISS operations Designed space shuttle, Buran, but launched only once in automated mode (no crew) in 1988 06-01-2011 2 Russia (2) Existing reliable launch vehicles Proton is largest: 21 tons to LEO; 5.5 tons to geostationary transfer orbit (GTO) Attempts to build Saturn V-equivalent in 1960s and 1970s failed (N1 failed four times in four attempts 1969-1972) Energiya booster in 1980s only flew twice (1987 with Polyus and 1988 with Buran). Abandoned for financial reasons. Was 100 tons to LEO; 18-20 tons to GTO; 32 tons to lunar trajectory. RD-170 engines for Energiya’s strap-ons live on today in other forms for Zenit, Atlas V, and Angara (under development) 06-01-2011 3 Russia (3) Robotic planetary space exploration mixed Excellent success at – Moon (Luna and Lunokhod series, plus Zond circumlunar flights) Venus (Venera series) Halley’s Comet (Vega 1 and 2—also Venus) Jinxed at Mars More than a dozen failures in 1960s - 1970s Partial success with Phobos 2 in 1988 (Phobos 1 failed) Mars 96 failed to leave Earth orbit Phobos-Grunt scheduled for later this year; designed as sample return from Phobos (includes Chinese orbiter) 06-01-2011 4 Russia (4) Grand statements over decades about sending people to the Moon and Mars, but never enough money to proceed. -
Proton Accident with GLONASS Satellites
3/29/2018 Proton accident with GLONASS satellites Previous Proton mission: SES6 PICTURE GALLERY A Proton rocket with the Block D 11S861 stage and 813GLN34 payload firing shortly before liftoff on July 2, 2013. Upcoming book on space exploration Read more and watch videos in: Site map Site update log About this site About the author The illfated Proton rocket lifts off on July 2, 2013, at 06:38:21.585 Moscow Time (July 1, 10:38 p.m. EDT). The rocket crashed approximately 32.682 seconds later, Roskosmos said on July 18, 2013. Mailbox Russia's Proton crashes with a trio of navigation satellites SUPPORT THIS SITE! Published: July 1; updated: July 2, 3, 4, 5, 9, 11, 15, 18, 19; 23; Aug. 11 Related pages: Russia's Proton rocket crashed less than a minute after its liftoff from Baikonur, Kazakhstan. A ProtonM vehicle No. 53543 with a Block DM03 (11S86103) upper stage lifted off as scheduled from Pad No. 24 at Site 81 (launch complex 8P882K) in Baikonur Cosmodrome on July 2, 2013, at 06:38:21.585 Moscow Time (on July 1, 10:38 p.m. EDT). The rocket started veering off course right after leaving the pad, deviating from the vertical path in various RD253/275 engines directions and then plunged to the ground seconds later nose first. The payload section and the upper stage were sheered off the vehicle moments before it impacted the ground and exploded. The flight lasted no more than 30 seconds. Searching for details: The Russian space agency's ground processing and launch contractor, TsENKI, was broadcasting the launch live and captured the entire process of the vehicle's disintegration and its crash. -
Ross University School of Medicine Annual Disclosure
Ross University School of Medicine 2020-2021 Annual Disclosure Student Right-to-Know and Campus Security (Clery Act) Annual Security Report Annual Fire Safety Report Sex and Gender Based Misconduct Response and Prevention Policy Alcohol & Substance Abuse Policy Student Rights under FERPA (The Family Educational Rights and Privacy Act) This document includes information for: Ross University School of Medicine, Barbados Campus, 2 mile Hill, St. Michael, Barbados December 15, 2020 The policies outlined in this document are current as of December 15, 2020. The most current versions of the policies are available online. 1 TABLE OF CONTENTS CAMPUS WATCH ............................................................................................ 4 REPORTING CRIMES AND EMERGENCIES ................................................ 4 ANNUAL SECURITY REPORT ....................................................................... 4 SIREN EMERGENCY ALERT SYSTEM ......................................................... 5 CAMPUS ACCESS, FACILITY SECURITY AND LAW ENFORCEMENT ............................................................................................... 5 MISSING STUDENT POLICY .......................................................................... 6 MISSING STUDENT PROCEDURES .............................................................. 7 SAFETY AND SECURITY ............................................................................... 7 FIRE SAFETY ................................................................................................... -
Igor AFANASYEV, Dmitry VORONTSOV Cosmonautics | Event
cosmonautics | event Andrey Morgunov Igor AFANASYEV, Dmitry VORONTSOV AANGARA’SNGARA’S FFIRSTIRST BBLASTOFFLASTOFF At 16.04 hrs Moscow time on 9 July 2014, the Plesetsk space launch centre saw the launching facility in February 2014 to the first launch of the Angara-1.2PP launch vehicle of the advanced space rocket practice its fuelling and the nose fairing was family being developed by the Khrunichev state space research and production fitted on the rocket in March. The successful ground tests were followed by the prelaunch centre. The maiden blastoff conducted as part of the Angara flight test programme preparations. was aimed at testing the solutions embodied in the design of the URM-1 and URM-2 The date of the launch was put off for versatile rocket modules and the Angara’s launch and technical facilities as well. 27 June 2014 due to extra checks required. In this connection, orbiting an actual spacecraft had not been considered, with On 9 June, Khrunichev hosted a session of an inseparable full-scale mock-up used as payload. The flight was suborbital to the Chief Designers Council, dedicated to prevent cluttering near-Earth orbit with space junk. the preparation of the Angara to its flight tests. The session pronounced the rocket fit To say the Angara’s first launch had been In spite of the hurdles, the developer, for the trials. anticipated for a long time would be an nevertheless, got in the stretch with the Angara The LV had been taken out of the assembly understatement: it was slated for 2005 under programme.