DOCSLIB.ORG

What's Inside... in Brief

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
What's Inside... in Brief National Aeronautics and Space Administration What’s inside... 2 Features 5 Integration and Testing 4 1 3 2 2015 6 Picture Place 7 Other News 8 Schedule & Miscellanea Sounding Rockets Program Office 46.012 UO Koehler - RockSat-X was succesfully launched In Brief... from Wallops Island on August 12, 2015. The new Black Brant Mk 4 vehicle will fly for the first time in October 2015 from Wallops Island. The payload carries several technology test experi- ments and instruments. Payload teams are preparing for the coming Norway campaign. Two rockets will be launched from Andoya with the launch window opening on November 27. The Multiple User Suborbital Instru- ment Carrier (MUSIC) payload will be launched from Wallops Island in Oc- tober on a Terrier-Improved Malemute rocket. The sounding rockets program will cel- ebrate 45-years at Wallops on Novem- ber 30, 2015. More on page 7. A very busy flight schedule is in prog- ress. The Sounding Rockets Program has 11 missions on schedule during the Students from Hawaii with their experiment after the successful flight. period September through November. The 46.012 UO RockSat-X mission was launched from Wallops Island, VA on Au- Three have been successfully complet- gust 12, 2015. RockSat-X is the most advanced of three student flight programs ed and eight remain. managed by Colorado Space Grant Consortium and supported by NASA. RockSat- X provides participating University faculty and students an opportunity to build, RockSat-X continued... test and fly an experiment of their own University Of Hawaii Community College design onboard a Terrier-Improved System University of Nebraska Lincoln (UNL) Malemute sounding rocket and in- Project Imua The experiment from the University of cludes full featured sounding rocket The primary mission goal for Project Nebraska Lincoln compared buoyant support systems, such as telemetry, Imua is to encourage UHCC students to convection on the ground in the pres- attitude control and recovery. explore and enter STEM-based careers ence of gravity to the expected absence Prior to their RockSat-X flight, partici- by engaging in team-oriented, problem- of buoyant convection in the micrograv- pants have flown two less advanced solving activities that emphasize the in- ity environment. Additionally the experi- types of experiments, RockOn and tegration process involved in the design, ment characterized crystal growth in mi- RockSat-C. development, construction, testing and crogravity through the study of buoyant documentation of launch-ready Cube- convection in a supersaturated solution The following schools participated in Sats and scientific payloads. The sci- of Sodium Acetate Trihydrate (SAT). the 2015 RockSat-X mission: ence goal of the experiment was to make The experiment provides more data on direct measurements of solar spectrum crystal formation in microgravity, specifi- UV components without atmospheric cally addressing the question why crys- absorption. Contribution of UV varia- tals grown in space are larger and purer tion in the 200 to 400nm range to total than ones formed on the ground. solar irradiance is highly uncertain. Data Video cameras recorded the reactions. will contribute to understanding of solar A thermal tracer was used to visualize dynamics. The experiment collected one buoyant effects during crystallization. full spectral sweep (at 2ms integration The crystallization reaction began via a time: 4.096 s/sweep) of data between seed crystal planted into a sodium ac- 200-600 nm with 0.4 nm resolution. etate trihydrate (SAT) solution by a linear actuator. A thermal tracer was used to visualize buoyant effects during crystal- lization. Capitol Technology University (CTU) Project Hermes The project goal was to test OSH- Comm (Onboard Satellite Hotspot Communications) System using TCP/ IP Protocol by tapping into an exist- ing network of communications satel- lites. The project uses Commercial Off the Shelf (COTS) components and the Iridium satellite network. A web-based interface is used to receive telemetry, Virginia Tech (VT) send commands, see data transfer and Virginia Tech students successfully Northwest Nazarene University (NNU) monitor health and safety information completed a 3D print in the space envi- Experiments from Northwest Nazarene Additionally, the experiment captured ronment and collected data on how to University were designed to demonstrate an image during the flight and sent it improve the shortcomings of the VT 3D the usefulness of flexible electronics through the Iridium network. printer design. This is a proof of concept when applied to data collection and stor- mission for 3D printing in space and col- age in space-flight applications. 2 On the weblects at:information http://sites.wff.nasa.gov/code810/ on the effects of chang- ing gravitational loads on 3D printing. mass while in microgravity. The pow- dered aluminum indium mixture was melted via induction heating and the sample created in microgravity will be compared to ground samples after the flight. This experiment Investigates the effect of solidification in microgravity on the microstructure. Early results, imaged below, from the University of Puerto Rico (UPR) Virginia Tech and Colorado University The University of Puerto Rico experiments were available immediately experiment attempted to col- on payload return to Wallops. Complete lect micrometeorites using two analysis is still in progress. deployed collection panels. The collection panels are sealed to withstand re-entry conditions and final astrogenomic analysis to be conducted in a lab setting. Additionally, the experiment’s impact detection system served as a collector for organic ma- terials, which will be analyzed using Next Generation Genomics in order to study the possible origins of life as stated in the Virginia Tech logo printed in space during the flight of 46.012. Panspermia Theory. Ultra high definition video was recorded looking outwards from the aft end of the experiment section where micrometeorites were to be collected from. University of Colorado - Boulder X-HD Experiment Deck The X-HD Experiment Deck recorded HD video of the flight and all experiments providing Alloy created during the RockSat-X flight onboard the experiment from University of Colo- a flight demonstration of new rado Boulder. experiment hardware for use For more information about RockSat-X, visit: on RockOn, RockSat-C/-X. The http://spacegrant.colorado.edu/national- deck includes eight GoPro cam- programs/rs-x-2015-home eras, four of which are deployed and retracted on a track system for viewing down the length of the experiment section and four are stationary and pointed per- pendicular to the thrust vector. In addition to the X-HED ex- periment Univeristy of Colorado students flew an experiment to generate a sample of an immis- cible alloy composed of 80% Aluminum and 20% Indium by On the web at: http://sites.wff.nasa.gov/code810/ 3 Images by Berit Bland 36.291US Winebarger - Chro- CLASP. Stable pointing of the payload was critical to achieve the science mea- mospheric Lyman-Alpha surements. Spectro-Polarimeter (CLASP) “This is an achievement many of us launched successfully on Sep- have been anxiously waiting decades to see,” says Dr. Moses/NASA HQ Program tember 3, 2015. Executive. * http://adsabs.harvard.edu/abs/2011AGUFM. The Science goals of CLASP were: P14C..05K • detection of atomic polarization of the Lyman-alpha line from the solar 36.282 US Kankelborg - Multi- 39.012 DR Bernhardt - Charged chromosphere. Aerosol Release Experiment Order Solar EUV Spectrograph • detection of the Hanle effect polar- (MOSES) 2 launched success- ization. (CARE) II launched successfully fully on August 27, 2015. on September 16, 2015 MOSES-2 investigated the transition region of the sun using an imaging spectrograph and the Hα guide tele- scope. MOSES takes measurements in the extreme UV part of the spectrum and this mission focused on obtaining line intensity images for Ciii 459.3A and Ne vii 465.2A at 1.2” resolution over a NASA MSFC Image CLASP in a clean room at Marshall Space Flight Center. 20’ X 10’ field of view with reasonable cadence (approx. 45 s). Additionally the The aim of the CLASP mission was to investigation set out to obtain simulta- achieve the first measurement of mag- neous line width and doppler shifts for netic field in the upper chromosphere the Ne vii line. and transition region of the Sun through the detection and measurement of Hanle effect polarization of the Lyman alpha line. The Hanle effect (i.e. the magnetic field induced modification of the linear polarization due to scattering processes in spectral lines) is believed to be a Photo by Chris Perry powerful tool for measuring the magnetic field in the upper chromosphere, as it is The CARE II payload was launched more sensitive to weaker magnetic fields from Andoya Rocket Range, Norway on NASA image September 16, 2015. The CARE II mis- MOSES payload integration at White Sands. than the Zeeman effect, and also sensi- tive to magnetic fields tangled at spatial sion examined the effect of artificially- scales too small to be resolved. The created, charged-particulate layers on For more information on the MOSES mis- Lyman-alpha (121.567 nm) line has been the scatter of UHF, L-Band and S-Band sion, see: http://www.nasa.gov/feature/ chosen because it is a chromospheric/ radars. The artificial particles were cre- goddard/nasa-funded-moses-2-sound- transition-region line, and because the ated from 37 CRV7 C14 motors ignited ing-rocket-to-investigate-coronal-heat- Hanle effect polarization of the Lyman- in the ionosphere. CARE II studied the ing alpha line is predicted to be sensitive to exhaust plume physics including Mag- 10-250 Gauss, encompassing the range netohydrodynamic (MHD) waves and of interest.* electric fields. The optical signature was measured from scattered sunlight According to Dr. Winebarger initial and ion-molecule-electron reactions. results indicate that breakthrough sci- This mission included a total of 44 ence, detection of scattering polarization rocket motors in one vehicle, a record of Lyman-alpha, was accomplished by for sounding rockets.
Load more

Recommended publications
  • 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.
    [Show full text]
  • Performance Modelling and Simulation of a 100 Km Hybrid Sounding Rocket
    PERFORMANCE MODELLING AND SIMULATION OF A 100 KM HYBRID SOUNDING ROCKET Fiona Kay Leverone Submitted in fulfilment of the academic requirements for the degree of Master of Science in Mechanical Engineering, College of Agriculture, Engineering and Science, University of KwaZulu-Natal Supervisor: Mr Michael Brooks Co-Supervisor: Mr Jean-François Pitot de la Beaujardiere Co-Supervisor: Prof Lance Roberts December 2013 2. DECLARATION 1 - PLAGIARISM I, Fiona Leverone, declare that 1. The research reported in this thesis, except where otherwise indicated, is my original research. 2. This thesis has not been submitted for any degree or examination at any other university. 3. This thesis does not contain other persons’ data, pictures, graphs or other information, unless specifically acknowledged as being sourced from other persons. 4. This thesis does not contain other persons’ writing, unless specifically acknowledged as being sourced from other researchers. Where other written sources have been quoted, then: a. Their words have been re-written but the general information attributed to them has been referenced b. Where their exact words have been used, then their writing has been placed inside quotation marks, and referenced. 5. This thesis does not contain text, graphics or tables copied and pasted from the Internet, unless specifically acknowledged, and the source being detailed in the thesis and in the References sections. Signed ________________________ Date ___________ Miss Fiona Leverone As the candidate’s supervisor I have approved this dissertation for submission. Signed ________________________ Date ___________ Mr. Michael Brooks As the candidates co-supervisor I have approved this dissertation for submission. Signed ________________________ Date ___________ Mr.
    [Show full text]
  • Space Planes and Space Tourism: the Industry and the Regulation of Its Safety
    Space Planes and Space Tourism: The Industry and the Regulation of its Safety A Research Study Prepared by Dr. Joseph N. Pelton Director, Space & Advanced Communications Research Institute George Washington University George Washington University SACRI Research Study 1 Table of Contents Executive Summary…………………………………………………… p 4-14 1.0 Introduction…………………………………………………………………….. p 16-26 2.0 Methodology…………………………………………………………………….. p 26-28 3.0 Background and History……………………………………………………….. p 28-34 4.0 US Regulations and Government Programs………………………………….. p 34-35 4.1 NASA’s Legislative Mandate and the New Space Vision………….……. p 35-36 4.2 NASA Safety Practices in Comparison to the FAA……….…………….. p 36-37 4.3 New US Legislation to Regulate and Control Private Space Ventures… p 37 4.3.1 Status of Legislation and Pending FAA Draft Regulations……….. p 37-38 4.3.2 The New Role of Prizes in Space Development…………………….. p 38-40 4.3.3 Implications of Private Space Ventures…………………………….. p 41-42 4.4 International Efforts to Regulate Private Space Systems………………… p 42 4.4.1 International Association for the Advancement of Space Safety… p 42-43 4.4.2 The International Telecommunications Union (ITU)…………….. p 43-44 4.4.3 The Committee on the Peaceful Uses of Outer Space (COPUOS).. p 44 4.4.4 The European Aviation Safety Agency…………………………….. p 44-45 4.4.5 Review of International Treaties Involving Space………………… p 45 4.4.6 The ICAO -The Best Way Forward for International Regulation.. p 45-47 5.0 Key Efforts to Estimate the Size of a Private Space Tourism Business……… p 47 5.1.
    [Show full text]
  • Desind Finding
    NATIONAL AIR AND SPACE ARCHIVES Herbert Stephen Desind Collection Accession No. 1997-0014 NASM 9A00657 National Air and Space Museum Smithsonian Institution Washington, DC Brian D. Nicklas © Smithsonian Institution, 2003 NASM Archives Desind Collection 1997-0014 Herbert Stephen Desind Collection 109 Cubic Feet, 305 Boxes Biographical Note Herbert Stephen Desind was a Washington, DC area native born on January 15, 1945, raised in Silver Spring, Maryland and educated at the University of Maryland. He obtained his BA degree in Communications at Maryland in 1967, and began working in the local public schools as a science teacher. At the time of his death, in October 1992, he was a high school teacher and a freelance writer/lecturer on spaceflight. Desind also was an avid model rocketeer, specializing in using the Estes Cineroc, a model rocket with an 8mm movie camera mounted in the nose. To many members of the National Association of Rocketry (NAR), he was known as “Mr. Cineroc.” His extensive requests worldwide for information and photographs of rocketry programs even led to a visit from FBI agents who asked him about the nature of his activities. Mr. Desind used the collection to support his writings in NAR publications, and his building scale model rockets for NAR competitions. Desind also used the material in the classroom, and in promoting model rocket clubs to foster an interest in spaceflight among his students. Desind entered the NASA Teacher in Space program in 1985, but it is not clear how far along his submission rose in the selection process. He was not a semi-finalist, although he had a strong application.
    [Show full text]
  • Seguranca.Pdf
    INPE-11476-RPQ/777 SEGURANÇA NO MANUSEIO DE FOGUETE Adauto Gouveia Motta INPE São José dos Campos 2004 SUMÁRIO LISTA DE FIGURAS .................................................................. v LISTA DE TABELAS .................................................................. vii MAIS ALGUMAS CONSIDERAÇÕES ............................................. ix INTRODUÇÃO .......................................................................... 01 CAPÍTULO 1 ............................................................................ 03 1.1 – A Busca ......................................................................... 03 1.2 – Plano de segurança de terra ............................................. 07 1.3 – Plano de segurança de vôo ............................................... 10 CAPÍTULO 2 – MOTOR FOGUETE ................................................ 15 2.1 – Propelentes sólidos .......................................................... 16 2.2 – Propelentes líquidos ......................................................... 19 2.3 – Foguetes híbridos ............................................................ 21 CAPÍTULO 3 – EXPLOSIVOS ...................................................... 23 3.1 – Explosivos como meio de propulsão .................................. 23 3.2 – Principais características dos explosivos ............................. 23 3.2.1 – Sensibilidade à iniciação por impacto .............................. 24 3.2.2 – Sensibilidade à iniciação por fricção ................................ 24 3.2.3 – Sensibilidade
    [Show full text]
  • MORABA Sounding Rocket Launch Vehicles
    MORABA Sounding Rocket Launch Vehicles Mobile Rocket Base German Aerospace Center Sounding Rocket Launch Vehicles 1.1. Introduction The research vehicles offered by MORABA have been used by a wide spectrum of payloads, differing in mass, complexity and transport requirements. In order to serve the needs of any payload and transport requirement, MORABA relies on a large portfolio of rocket motors that it uses in single stage as well as stacked configurations. MORABA constantly strives to enhance the portfolio of active rocket motors in order to improve its transport capacities or replace systems that run out of stock. Although the developments in liquid, gelled and hybrid propulsion are closely followed, the high power density, operational simplicity and safety of solid rocket motors have led to their exclusive use by MORABA so far. A large portion of the active portfolio is formed by motors with military heritage. These motors are conceded to MORABA or its partners from governments that tear down a fraction of their armory. As usually these motors have exceeded their shelf life, inspection and re-lifing efforts become necessary. Many successful missions prove the flight worthiness of these motors which are not least attractive due to their competitive price. The second group of the portfolio is made up by motors available from third parties. Here, MORABA is constantly evaluating potential candidates. A longstanding cooperation with the Brazilian Department of Aerospace Science and Technology (DCTA) has led to frequent use of its S31 and S30 rocket motor stages. At current, MORABA is also developing a solid motor stage with Bayern Chemie GmbH and acquiring some units of Magellan’s Black Brant V.
    [Show full text]
  • Esa S -291 TR 9 Ooom — G*? A
    O esa s -291 TR 9 ooom — g*? a Proceedings of the Ninth ESA/PAC Symposium jointly organised by the Deutsche Forschungsanstalt furLuft- und Raumfahrt and the European Space Agency and held at Lahnstein, Federal Republic of Germany, on 3 - 7 April 1989. BMFT TO PREPARE FOR THE 21ST CENTURY esa sp-291 25 YEARS OF EUROPEAN COOPERATION IN SPACE June 1989 25 ANS DE COOPERATION SPATIALE EUROPEENNE POUR PREPARER LE 21EME SIECLE European Rocket and Balloon Programmes and Related Research* Proceedings of the Ninth ESA/PAC 89- Symposium jointly organised by the Deutsche Forschungsanstalt fur Luft- und Raumfahrt and the European Space Agency. and held at Lahnstein, Federal Republic of Germany, on 3 - 7 April 1989. european space agency / agence spatiale européenne 8-10, rue Mario-Nikis, 75738 PARIS CEDEX 15, France PROGRAMME COMMITTEE Chairman Dr. D. Huguenin, Mr. W.R. Burke, Observatoire de Genève, EPD/ESTEC, Professor U. von Zahn, Switzerland Noordwijk, Physikalisch Institut, The Netherlands University of Bonn, Dr. J.P. Jegou, FRG Centre National d'Etudes Mr. [. Stevenson, Spatiales, ESA/HQ, Members Paris, Paris, France France Dr. A. Brekke, University of Tromse, Mr. O. Rôhrig, Mr. L. Jansson, Norway Deutsche Forschungsanstalt fur ESA/HQ, Luft- und Raumfahrt, Paris, Dr. L. Eliasson, PT-TN, France Institute of Space Physics, Linder Hôhe, Kiruna, KoIn, Sweden FRG COLOPHON Proceedings published ESA Publications Division and distributed by ESTEC, Noordwijk, The Netherlands compiled by W.R. Burke printed in The Netherlands Cover by C. Haakman Price code E3 International Standard Serial Number ISSN 0379 - 6566 International Standard Book Number ISBN 92-9092-006-8 Copyright © 1988 by European Space Agency Ill CONTENTS Session 1: National Reports Chairman: M.
    [Show full text]
  • Arctic National Wildlife Refuge, Alaska, Coastal Plain Resource Assessment" and Legislative Environmental Impact Statement (LEIS)
    Comments from State and Local Governments (S) Page State of Alaska ................................................................................................. S- 1 Alaska State Legislature (Rep. Sam Cotten)................................................. 16 Arctic Village Council ....................................................................................... 17 California Department of Fish and Game ..................................................... 18 City of Kaktovik................................................................................................ 19 Massachusetts Department of Fisheries, Wildlife & Environmental Law Enforcement ................................................................. 20 North Slope Borough ...................................................................................... 22 University of Alaska, Geophysical Institute................................................... 37 Venetie Village................................................................................................... 41 I '; STEVE COWPER, GOVERNOR CENTRAL OFFICE P.O. BOX AW OFFICE OF THE GOVERNOR JUNEAU, ALASKA 99811-0165 PHONE: (907) 465-3562 OFFICE OF MANAGEMENT AND BUDGET DIVISION OF GOVERNMENTAL COORDINATION SOUTHEAST REGIONAL OFFICE SOUTHCENTRAL REGIONAL OFFICE NORTHERN REGIONAL OFFICE 431 NORTH FRANKLIN 2600 DENALI STREET 675 SEVENTH A VENUE P.O. BOX AW, SUITE 101 SUITE 700 STATION H JUNEAU, ALASKA 99811-0165 ANCHORAGE, ALASKA 99503-2798 FAIRBANKS, ALASKA 99701-4596 PHONE: (907) 465-3562 PHONE.· (907)
    [Show full text]
  • Our First Quarter Century of Achievement ... Just the Beginning I
    NASA Press Kit National Aeronautics and 251hAnniversary October 1983 Space Administration 1958-1983 >\ Our First Quarter Century of Achievement ... Just the Beginning i RELEASE ND: 83-132 September 1983 NOTE TO EDITORS : NASA is observing its 25th anniversary. The space agency opened for business on Oct. 1, 1958. The information attached sumnarizes what has been achieved in these 25 years. It was prepared as an aid to broadcasters, writers and editors who need historical, statistical and chronological material. Those needing further information may call or write: NASA Headquarters, Code LFD-10, News and Information Branch, Washington, D. C. 20546; 202/755-8370. Photographs to illustrate any of this material may be obtained by calling or writing: NASA Headquarters, Code LFD-10, Photo and Motion Pictures, Washington, D. C. 20546; 202/755-8366. bQy#qt&*&Mary G. itzpatrick Acting Chief, News and Information Branch Public Affairs Division Cover Art Top row, left to right: ffComnandDestruct Center," 1967, Artist Paul Calle, left; ?'View from Mimas," 1981, features on a Saturnian satellite, by Artist Ron Miller, center; ftP1umes,*tSTS- 4 launch, Artist Chet Jezierski,right; aeronautical research mural, Artist Bob McCall, 1977, on display at the Visitors Center at Dryden Flight Research Facility, Edwards, Calif. iii OUR FIRST QUARTER CENTER OF ACHIEVEMENT A-1 -3 SPACE FLIGHT B-1 - 19 SPACE SCIENCE c-1 - 20 SPACE APPLICATIQNS D-1 - 12 AERONAUTICS E-1 - 10 TRACKING AND DATA ACQUISITION F-1 - 5 INTERNATIONAL PROGRAMS G-1 - 5 TECHNOLOGY UTILIZATION H-1 - 5 NASA INSTALLATIONS 1-1 - 9 NASA LAUNCH RECORD J-1 - 49 ASTRONAUTS K-1 - 13 FINE ARTS PRQGRAM L-1 - 7 S IGN I F ICANT QUOTAT IONS frl-1 - 4 NASA ADvIINISTRATORS N-1 - 7 SELECTED NASA PHOTOGRAPHS 0-1 - 12 National Aeronautics and Space Administration Washington, D.C.
    [Show full text]
  • Vehículos De Lanzamiento 1
    Vehículos de lanzamiento 1 Vehículos de Lanzamiento (Estados Unidos) Copyright © 2009 by Eladio Miranda Batlle. All rights reserved. Los textos, imágenes y tablas que se encuentran en esta cronología cuentan con la autorización de sus propietarios para ser publicadas o se hace referencia a la fuente de donde se obtuvieron los mismos. Eladio Miranda Batlle [email protected] Vehículos de lanzamiento 2 Vehículos de lanzamiento. EE.UU EE.UU. A-4 (US Modifications) Hermes-B Bumper Aerobee Aerobee (boosted) Aerobee-350 Amroc SET Ares-1 Ares-5 Asp Asp (boosted) Asp with upper stage Eladio Miranda Batlle [email protected] Vehículos de lanzamiento 3 Arcas Boosted Arcas Arcon Astrobee-D ATACMS (MGM-140) Astrobee-F ATACMS Booster ATB SRBM Atlas (CGM-16 / HGM-16) Atlas without upper Atlas Able Atlas Agena ICBM stage Eladio Miranda Batlle [email protected] Vehículos de lanzamiento 4 Atlas with solid-fuel Atlas Centaur Atlas-5 Black Armadillo upper stage Starfire-1 Black Sparrow Goddard New Shephard Bullpup with small upper Athena-H Castor-4A Castor-4B stage Eladio Miranda Batlle [email protected] Vehículos de lanzamiento 5 Corporal (MGM-5) Deacon / Cajun / Conestoga-1000 DC-X SRBM Apache Deacon / Cajun / Apache Deacon / Cajun / Apache ALSOR Delta-4 Clusters with upper stages Dolphin Falcon-1 Falcon-9 GBI-BV Eladio Miranda Batlle [email protected] Vehículos de lanzamiento 6 Ute / Paiute with upper Genie (AIR-2) AAM ALARR Astrobee-500 stages Hawk (MIM-23) SAM Aerobee-75 Orion HiRoc (MX-774) Honest John
    [Show full text]
  • Sounding Rocket Program Handbook (SRPH)
    Downloaded from http://www.everyspec.com Sounding Rocket Program Handbook (SRPH) Suborbital Projects and Operations Directorate Sounding Rockets ProgramOffice June 1, 1999 Goddard Space Flight Center National Aeronautics and Wallops Flight Facility Space Administration Wallops Island, Virginia 23337 Downloaded from http://www.everyspec.com Preface This Handbook describes the capabilities of the program, the design and technology applications to be considered, and the process NASA has established to integrate the customer (principal investigator/program user/scientist/experimenter) into the sounding rocket mission team to ensure the highest probability of a successful project. Neither the United States Government nor any person acting on the behalf of the Unites States Government assumes any liability resulting from the use of information contained in this document or warrants that the use will be free from privately owned rights. The use of a company name does not imply approval or recommendation of the product to the exclusion of others that may also be suitable. ii Downloaded from http://www.everyspec.com Sounding Rocket Program Handbook Table of Contents PREFACE .......................................................................II SECTION 1: NASA SOUNDING ROCKET PROGRAM........................... 2 1.1 INTRODUCTION ...................................................................................2 1.2 NASA ORGANIZATIONAL RESPONSIBILITIES ................................................1-3 1.3 SOUNDING ROCKET PROGRAM CUSTOMER’S
    [Show full text]
  • Sounding Rocket Working Group
    Sounding Rocket Working Group 21 January 2014 The attached documents contain technical data within the definition of the International Traffic in Arms Regulation, and are subject to the export control laws of the U.S. Government. Transfer of this data by any means to a foreign person, whether in the U.S. or abroad, without an export license or other approval from the U.S. Department of State, is prohibited. Similarly, publication or other release into the public domain constitutes an export and is not authorized, except as approved by the cognizant U.S. government department or agency. NSRP Briefing Outline • Programmatics - Eberspeaker/Schafer SRPO NSROC • Schedule Adherence - Eberspeaker • Success Criteria Guidelines - Ransone • Anomaly Status - Rosanova • Motors & Vehicle Systems - Brodell/Hesh/Hunter Surplus Peprgrine Brants Orioles FTS Caster • Annual Report & PI Questionnaire - Eberspeaker • Educational Activities - Eberspeaker/Koehler • Range Status - Ransone Wallops Pker WSMR Kwajalein Norway Australia • Technology Development - Rosanova / NSROC 2 SRPO Programmatic Eberspeaker The attached documents contain technical data within the definition of the International Traffic in Arms Regulation, and are subject to the export control laws of the U.S. Government. Transfer of this data by any means to a foreign person, whether in the U.S. or abroad, without an export license or other approval from the U.S. Department of State, is prohibited. Similarly, publication or other release into the public domain constitutes an export and is not authorized, except as approved by the cognizant U.S. government department or agency. June SRWG Findings 1. Strong Concern Regarding Program Vitality (Letter sent to NASA HQ) • The SRPO appreciates the support… 2.
    [Show full text]