Methods of Oabservation at Sea Meteorological Soundings in The
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Hohonu Volume 5 (PDF)
HOHONU 2007 VOLUME 5 A JOURNAL OF ACADEMIC WRITING This publication is available in alternate format upon request. TheUniversity of Hawai‘i is an Equal Opportunity Affirmative Action Institution. VOLUME 5 Hohonu 2 0 0 7 Academic Journal University of Hawai‘i at Hilo • Hawai‘i Community College Hohonu is publication funded by University of Hawai‘i at Hilo and Hawai‘i Community College student fees. All production and printing costs are administered by: University of Hawai‘i at Hilo/Hawai‘i Community College Board of Student Publications 200 W. Kawili Street Hilo, Hawai‘i 96720-4091 Phone: (808) 933-8823 Web: www.uhh.hawaii.edu/campuscenter/bosp All rights revert to the witers upon publication. All requests for reproduction and other propositions should be directed to writers. ii d d d d d d d d d d d d d d d d d d d d d d Table of Contents 1............................ A Fish in the Hand is Worth Two on the Net: Don’t Make me Think…different, by Piper Seldon 4..............................................................................................Abortion: Murder-Or Removal of Tissue?, by Dane Inouye 9...............................An Etymology of Four English Words, with Reference to both Grimm’s Law and Verner’s Law by Piper Seldon 11................................Artifacts and Native Burial Rights: Where do We Draw the Line?, by Jacqueline Van Blarcon 14..........................................................................................Ayahuasca: Earth’s Wisdom Revealed, by Jennifer Francisco 16......................................Beak of the Fish: What Cichlid Flocks Reveal About Speciation Processes, by Holly Jessop 26................................................................................. Climatic Effects of the 1815 Eruption of Tambora, by Jacob Smith 33...........................Columnar Joints: An Examination of Features, Formation and Cooling Models, by Mary Mathis 36.................... -
Suborbital Platforms and Range Services (SPARS)
Suborbital Capabilities for Science & Technology Small Missions Workshop @ Johns Hopkins University June 10, 2019 Mike Hitch, Giovanni Rosanova Goddard Space Introduction Flight Center AGENDAWASP OPIS ▪ Purpose ▪ History & Importance of Suborbital Carriers to Science ▪ Suborbital Platforms ▪ Sounding Rockets ▪ Balloons (brief) ▪ Aircraft ▪ SmallSats ▪ WFF Engineering ▪ Q & A P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 2 Goddard Space Purpose of the Meeting Flight Center Define theWASP OPISutility of Suborbital Carriers & “Small” Missions ▪ Sounding rockets, balloons and aircraft (manned and unmanned) provide a unique capability to scientists and engineers to: ▪ Allow PIs to enhance and advance technology readiness levels of instruments and components for very low relative cost ▪ Provide PIs actual science flight opportunities as a “piggy-back” on a planned mission flight at low relative cost ▪ Increase experience for young and mid-career scientists and engineers by allowing them to get their “feet wet” on a suborbital mission prior to tackling the much larger and more complex orbital endeavors ▪ The Suborbital/Smallsat Platforms And Range Services (SPARS) Line Of Business (LOB) can facilitate prospective PIs with taking advantage of potential suborbital flight opportunities P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 3 Goddard Space Value of Suborbital Research – What’s Different? Flight Center WASP OPIS Different Risk/Mission Assurance Strategy • Payloads are recovered and refurbished. • Re-flights are inexpensive (<$1M for a balloon or sounding rocket vs >$10M - 100M for a ELV) • Instrumentation can be simple and have a large science impact! • Frequent flight opportunities (e.g. “piggyback”) • Development of precursor instrument concepts and mature TRLs • While Suborbital missions fully comply with all Agency Safety policies, the program is designed to take Higher Programmatic Risk – Lower cost – Faster migration of new technology – Smaller more focused efforts, enable Tiger Team/incubator experiences. -
Measurements of Auroral Particles by Means of Sounding Rockets of Mother-Daughter Type A
MEASUREMENTS OF AURORAL PARTICLES BY MEANS OF SOUNDING ROCKETS OF MOTHER-DAUGHTER TYPE A. Falck KGI REPORT 192 NOVEMBER 1985 KIRUNA U-OI'HYSICAL INSTITITK MKINA N\X|1>I\ MEASUREMENTS OF AURORAL PARTICLES BY MEANS OF SOUNDING ROCKETS OF MOTHER-DAUGHTER TYPE by A. Falck Kiruna Geophysical Institute P.O. Box 704, S-981 27 KIRUNA, Sweden KGI Report 192 November 1985 Printed in Sweden Kiruna Geophysical Institute Kiruna 19^5 ISSN 034/-f 405 Contents Page 1. Presentation of the S17 payioads 3 1.1 The scientific objective of the sounding rockets S17 3 1.2 S17 experiments 3 1.3 Physical characteristics of the payioads 3 1.4 Physical characteristics of the Nike-Tomahawk rocket 5 1.5 Nominal characteristics of flight events 7 1.6 Attitude measurements 8 1.7 Separation of the two payload units 20 1.8 Telemetry and data analyzing technique 33 2. Description of the instrumentation for the particle experiments in the S17 payioads 38 2.1 General theory of CEM - detectors 38 2.2 Calibration of th* CEM - detectors 42 2.3 Solid state detectors in SI7 payioads 44 2.4 Mounting of the detectors 48 2.5 The efficiency of channel multipliers 48 3. Review of the geophysical conditions during the SI7 flights and presentation of some supporting observations 51 j.1 The auroral situation during S17 flights 51 :• 2 Magnetic activity 51 .'.3 Other supporting observations 56 .4 The lowlightlevel-TV-system 56 'K Particle fluxes and electric currents coupling the magnetosphere and the ionosphere during a magnetospheric substorm 66 4.1 Review of some substorm terminology and definitions 66 4.2 Reference and comparisons of SI7-2 measure- ments with the results of the IMS-study 75 4.3 Comparison of simultaneous particle observa- tions at low ionospheric altitude (S17-1) and at the magnetic equatorial region (ATS-6) 91 4.4 Summary and conclusions 99 5. -
Summary of a Program Review Held at Huntsville, Alabama October 19-21, 1982
Summary of a program review held at Huntsville, Alabama October 19-21, 1982 - TECH LIBRARY KAFEI, NM lllllllsllllllRlRllffllilrml OOSSE!?b NASA Conference Publication 2259 NASA/MSFCFY-82 Atmospheric Processes Research Review Compiled by Robert E. Turner George C. Marshall Space Flight Center Marshall Space Flight Center, Alabama Summary of a program review held at Huntsville, Alabama October 19-21, 1982 National Aeronautics and Space Administration Sclontlflc and Tochnlcal InformatIon Branch 1983 ACKNOWLEDGMENTS The productive inputs and comments from the participants and attendees in the Atmospheric Processes Research Review contributed very much to the success of the review. The opportunity provided for everyone to become better acquainted with the work of other investigators and to see how the research relates to the overall objective of NASA's Atmospheric Processes Research Program was an important aspect of the review. Appreciation is expressed to all those who participated in the review. The organizers trust that participation will provide each with a better frame of reference from which to proceed with the next year's research activities. ii PREFACE Each year NASA supports research in various disciplinary program areas. The coordination and exchange of information among those sponsored by NASA to conduct research studies are important elements of each program. The Office of Space Science and Applications and the Office of Aeronautics and Space Technology, via Announcements of Opportunity (AO), Application Notices (AN),etc., invites interested investigators throughout the country to communicate their research ideas within NASA and in institutions. The proposals in the Atmospheric Processes Research area selected and assigned to the NASA Marshall Space Flight Center's (MSFC's) Atmospheric Sciences Division for technical monitorship, together with the research efforts included in the FY-82 MSFC Research and Technology Operating Plan (RTOP1 I are the source of principal focus for the NASA/MSFC FY-82 Atmospheric Processes Research Review. -
The Stratopause Evolution During Different Types of Sudden Stratospheric Warming Event
Clim Dyn DOI 10.1007/s00382-014-2292-4 The stratopause evolution during different types of sudden stratospheric warming event Etienne Vignon · Daniel M. Mitchell Received: 18 February 2014 / Accepted: 5 August 2014 © The Author(s) 2014. This article is published with open access at Springerlink.com Abstract Recent work has shown that the vertical struc- Keywords Stratopause · Sudden stratospheric warming · ture of the Arctic polar vortex during different types of MERRA data · Polar vortex · sudden stratospheric warming (SSW) events can be very Middle atmospheric circulation distinctive. Specifically, SSWs can be classified into polar vortex displacement events or polar vortex splitting events. This paper aims to study the Arctic stratosphere during 1 Introduction such events, with a focus on the stratopause using the Mod- ern Era-Restrospective analysis for Research and Applica- The stratopause is characterised by a reversal of the atmos- tions reanalysis data set. The reanalysis dataset is compared pheric lapse rate at around 50 km (~1 hPa). While strato- against two independent satellite reconstructions for valida- spheric ozone heating is responsible for the stratopause pres- tion purposes. During vortex displacement events, the strat- ence at sunlit latitudes, westward gravity wave drag (and to opause temperature and pressure exhibit a wave-1 structure a lesser extent, stationary gravity wave drag) maintains the and are in quadrature whereas during vortex splitting events stratopause in the polar night jet (Hitchman et al. 1989). they exhibit a wave-2 structure. For both types of SSW the Indeed, the westward and stationary gravity wave (GW) temperature anomalies at the stratopause are shown to be breaking induces a mesospheric meridional flow toward the generated by ageostrophic vertical motions. -
Colorado Space Grant Consortium
CO_FY16_Year2_APD Colorado Space Grant Consortium Lead Institution: University of Colorado Boulder Director: Chris Koehler Telephone Number: 303.492.3141 Consortium URL: http://spacegrant.colorado.edu Grant Number: NNX15AK04H Lines of Business (LOBs): NASA Internships, Fellowships, and Scholarships; Stem Engagement; Institutional Engagement; Educator Professional Development A. PROGRAM DESCRIPTION The National Space Grant College and Fellowship Program consists of 52 state-based, university- led Space Grant Consortia in each of the 50 states plus the District of Columbia and the Commonwealth of Puerto Rico. Annually, each consortium receives funds to develop and implement student fellowships and scholarships programs; interdisciplinary space-related research infrastructure, education, and public service programs; and cooperative initiatives with industry, research laboratories, and state, local, and other governments. Space Grant operates at the intersection of NASA’s interest as implemented by alignment with the Mission Directorates and the state’s interests. Although it is primarily a higher education program, Space Grant programs encompass the entire length of the education pipeline, including elementary/secondary and informal education. The Colorado Space Grant Consortium is a Designated Consortium funded at a level of $760,000 for fiscal year 2016. B. PROGRAM GOALS • Population of students engaged in COSGC hands-on programs (awardees and non- awardees) will be at least 40% women and 23.7% from ethnic minority populations underrepresented in STEM fields. • Maintain student hands-on programs at all 8 COSGC Minority Serving Institutions and engaged at least 30 students on MSI campuses. • 30% of COSGC NASA funds will be awarded directly to students. • Award 80 scholarships to support students working on hands-on projects. -
Earth's Atmospheric Layers
Earth's atmospheric layers Earth's atmospheric layers Lesson plan (Polish) Lesson plan (English) Earth's atmospheric layers Source: licencja: CC 0, [online], dostępny w internecie: www.pixabay.pl. Link to the lesson Before you start you should know what the place of the atmosphere is in relation to the lithosphere, hydrosphere, biosphere and pedosphere; that the Earth's atmosphere is the part of the Earth and moves with it. You will learn explain the term „atmosphere”; name gases that form the air and their percentage share; name permanent and variable components of atmospheric air; name the layers of the atmosphere; discuss the role of the ozone layer; characterize the effects of the ozone hole and the greenhouse effect. Nagranie dostępne na portalu epodreczniki.pl nagranie abstraktu What layers is the atmosphere built of? In the Earth's atmosphere we distinguish 5 main layers characterized by specific features and 4 intermediate layers called pauses. The boundaries between them are conventional and change depending on the geographical latitude, terrain and season of the year. The closest one to the surface of the earth is the troposphere. Its thickness ranges from 7 km (in winter) to 10 km (in summer) above the poles, and 15‐18 km above the equator. The main feature that allows determining the boundary of the troposphere is the drop in the air temperature with an increase of about 0,6°C per 100 m. In the upper layer of the troposphere, the temperature reaches -55°C (above arctic regions) to -70°C (above equatorial regions). Above this layer there is a thin tropopause with the constant temperature, and above it there is the stratosphere extending up to a height of about 50 km, in which the air temperature rises to reach 0°C. -
Importance Oi Thermistor Mount Configuration to Meteorological
James F. Morrissey importance oi and Andrew S. Carten, Jr. thermistor mount configuration A. F. Cambridge Research Laboratories to meteorological rocket Bedford, Mass. temperature measurements Abstract tions. Thus, we are receiving more data than ever be- A description is given of the original rocketsonde ther- fore—thanks to more successful firings and improved mistor mount, consisting of a 10-mil bead suspended signal reception—but data quality has stayed at a low between two metal posts. The difficulties encountered to medium level. Recent evidence, described later in this with this mount and the subsequent development of article, confirms our belief that caution is in order. the superior "thin-film" mount are also described. The Today's rocketsonde is, for the most part, a more uncertainties associated with the use of the latter mount rugged version of the standard radiosonde. This is only are outlined along with their effect on data acceptance. natural, considering both the effort which has gone into A different approach to the original problem is de- refining radiosonde and associated ground equipment scribed, which employs longer leads for dissipation of design and the success which has crowned that effort. heat conducted to the bead. The uncertainty associated In choosing a sensor for the rocketsonde, it was recog- with the long lead is shown to be minimal. Preliminary nized that the small bead thermistor has the necessary results of a series of 10 rocket flights are presented. response time to provide useful measurements to about These results tend to confirm the advantages of the 60 km. A 10-mil diameter bead, aluminized to minimize long lead mount. -
NASA Sounding Rockets Annual Report 2020
National Aeronautics andSpaceAdministration National Aeronautics NASA Sounding Rockets Annual Report 2020 science payload launched on a Terrier-Improved Malemute provided by NASA, experienced a vehicle failure and science data was not recorded. The Cusp Heating Investigation (CHI) for Dr. Larsen, Clemson University, measured neutral upwelling and high-resolution electric fields over an extended region in the cusp, and was a resound- ing success. Additionally, the Cusp-Region Experiment (C-REX) 2 for Dr. Conde, University of Alaska, was staged and ready to go at Andoya Space Center, Norway, however, science conditions did not materialize, and after 17 launch attempts the window of opportunity closed. C-REX 2 is currently on schedule for launch in December 2020. The final geospace science launch for fiscal year 2020 took place from Poker Flat Research Range, Alaska. Polar Night Nitric Oxide Message from the Chief Message Giovanni Rosanova, Jr. (PolarNOx), for Dr. Bailey, Virginia Tech, was successfully launched Chief, Sounding Rockets Program Office in January 2020. Data from PolarNOx will aid in the understanding of the abundance of NO in the polar atmosphere, and its impact on I will start this year’s message with expressing my gratitude to the peo- ozone. ple supporting the sounding rockets program. Through the challeng- ing time of the CoVid-19 pandemic, the outstanding efforts by the Technology development is a core aspects of the program. This year entire team have enabled us to continue meeting several milestones. we launched the eighth dedicated technology development flight, Our mission meetings have been held using virtual tools. Enhanced SubTEC-8. -
The Earth's Atmosphere
A Resource Booklet for SACE Stage 1 Earth and Environmental Science The following pages have been prepared by practicing teachers of SACE Earth and Environmental Science. The six Chapters are aligned with the six topics described in the SACE Stage 1 subject outline. They aim to provide an additional source of contexts and ideas to help teachers plan to teach this subject. For further information, including the general and assessment requirements of the course see: https://www.sace.sa.edu.au/web/earth-and-environmental- science/stage-1/planning-to-teach/subject-outline A Note for Teachers The resources in this booklet are not intended for ‘publication’. They are ‘drafts’ that have been developed by teachers for teachers. They can be freely used for educational purposes, including course design, topic and lesson planning. Each Chapter is a living document, intended for continuous improvement in the future. Teachers of Earth and Environmental Science are invited to provide feedback, particularly suggestions of new contexts, field-work and practical investigations that have been found to work well with students. Your suggestions for improvement would be greatly appreciated and should be directed to our project coordinator:: [email protected] Preparation of this booklet has been coordinated and funded by the Geoscience Pathways Project, under the sponsorship of the Geological Society of Australia (GSA) and the Teacher Earth Science Education Program (TESEP). In-kind support has been provided by the SA Department of Energy and Mining (DEM) and the Geological Survey of South Australia (GSSA). FAIR USE: The teachers named alongside each chapter of this document have researched available resources, selected and collated these notes and images from a wide range of sources. -
Investigation of the In-Flight Failure of the Stratos III Sounding Rocket
ISASI 2019 - Investigation of the in-flight failure of the Stratos III Sounding Rocket Rolf Wubben, Lead Investigator Eoghan Gilleran, General Investigator Krijn de Kievit, General Investigator Bart Kevers, Structural Analysis Maurits van Heijningen, Data Analysis Martin Christiaan Olde, RCA Methodology Delft Aerospace Rocket Engineering, Stevinweg 1 2628 CN Delft, South Holland, The Netherlands The Stratos III sounding rocket is a rocket developed by students from Delft Aerospace Rocket Engineering (DARE) at Delft University of Technology. It is the third generation of the Stratos rocket and was intended to break the European student altitude record of 33.5 km. However, 22.12 seconds into the flight of Stratos III an anomaly occurred, resulting in the loss of the vehicle. At this time, the rocket was travelling at approximately Mach 3 at an altitude of 10 km. An investigation was performed by the students of DARE with the help of Delft University of Technology personnel. The purpose of this report is to show how the investigation was performed, what the results are, how future anomalies can be prevented and how future investigations can be improved. After performing a root cause analysis (RCA) it was determined that inertial roll coupling was the main cause of the Stratos III anomaly. This could be concluded from data provided by on-board inertial measurement units (IMUs) as well as ground radar and Doppler data. This data shows divergence of the sideslip angles of the rocket during flight, until the limit values are reached at the disintegration event. Inertial roll coupling is a complex phenomenon that can be caused by a plethora of different factors, such as the large length to diameter ratio of the rocket or flexibility and misalignment of the rocket body, resulting in both a large effective thrust misalignment as well as an induced aerodynamic pitching moment. -
Sounding Rockets : Principle, Functioning and Applications
Sounding Rockets : Principle, Functioning and Applications Florimond Collette Yann Kempf BASI-P2, Université du Luxembourg Małgorzata Karaś Warsaw School of Economics Abstract Sounding rockets appeared in the mid-20th century and proved to be an extremely useful science tool in all fields of physics and even beyond. These rockets are conceived for sub-orbital flights, to take measurement and/or perform experiments in the high atmosphere, in near space and/or in micro-gravity conditions. They also allow to introduce young scientists to space sciences by undertaking a full-scale pedagogical science project with a relatively moderate cost. This paper presents the origins and principles of sounding rockets, how they work, as well as a few recent science applications. Introduction Sounding rockets are small rockets (vehicles powered by the high-speed ejection of matter through a nozzle) with one or several stages and solid, liquid or hybrid propellant. They perform sub-orbital flights at maximal altitudes ranging from less than 1 km to more than 1200 km. After a thrust phase, they generally have a ballistic flight phase before touching or splashing down. If they have the right equipment, they can be retrieved after the flight. Apart from the engines, sounding rockets comprise a payload made of science experiments performed during the flight, as well as a data processing system, either with real-time radio downlink, or on-board saving. The first case implies real-time tracking by one or more ground telemetry stations. The second case implies recovery of the rocket after the flight to extract the data. Sounding rockets are a privileged tool because they reach zones of the atmospheric and near-space environment that are unaccessible by other means.