Rocket in Situ Observation of Equatorial Plasma Irregularities in the Region Between E and F Layers Over Brazil

Total Page:16

File Type:pdf, Size:1020Kb

Rocket in Situ Observation of Equatorial Plasma Irregularities in the Region Between E and F Layers Over Brazil Ann. Geophys., 35, 413–422, 2017 www.ann-geophys.net/35/413/2017/ doi:10.5194/angeo-35-413-2017 © Author(s) 2017. CC Attribution 3.0 License. Rocket in situ observation of equatorial plasma irregularities in the region between E and F layers over Brazil Siomel Savio Odriozola1,2, Francisco Carlos de Meneses Jr.1,3, Polinaya Muralikrishna1, Alexandre Alvares Pimenta1, and Esfhan Alam Kherani1 1National Institute for Space Research – INPE, Av. dos Astronautas, 1758, Jd. Granja-CEP: 12227-010 SJC, SP, Brazil 2Department of Space Geophysics, Institute of Geophysics and Astronomy – IGA, Calle 212, 2906, La Coronela, La Lisa, Havana, Cuba 3State Key Laboratory of Space Weather, National Space Science Center NSSC, Chinese Academy of Sciences (CAS), No. 1 Nanertiao, Zhongguancun, Haidian district, 100190, Beijing, China Correspondence to: Siomel Savio Odriozola ([email protected]) Received: 30 July 2016 – Revised: 23 February 2017 – Accepted: 23 February 2017 – Published: 16 March 2017 Abstract. A two-stage VS-30 Orion rocket was launched LaBelle, 1998; Muralikrishna et al., 2004). Studies using in from the equatorial rocket launching station in Alcântara, situ measurements of equatorial nighttime E region irregular- Brazil, on 8 December 2012 soon after sunset (19:00 LT), ities, however, are quite a few, as noted by Sinha et al.(2011). carrying a Langmuir probe operating alternately in swept and The lack of references is most noticeable when it comes to constant bias modes. At the time of launch, ground equip- the intermediate region between the E and F layers ( ∼ 130– ment operated at equatorial stations showed rapid rise in the 300 km). base of the F layer, indicating the pre-reversal enhancement Although data from other studies show irregular structures of the F region vertical drift and creating ionospheric con- in the electron concentration in the F valley region (Abdu ditions favorable for the generation of plasma bubbles. Ver- et al., 1991; Vickrey et al., 1984; Sinha et al., 1999; Raizada tical profiles of electron density estimated from Langmuir and Sinha, 2000; Hysell et al., 2005; Muralikrishna and probe data showed wave patterns and small- and medium- Abdu, 2006), up to now, only Vickrey et al.(1984) and scale plasma irregularities in the valley region (100–300 km) Raizada and Sinha(2000) have analyzed the irregularities during the rocket upleg and downleg. These irregularities re- detected in this region. Both studies used measurements ob- semble those detected by the very high frequency (VHF) tained using a Langmuir probe onboard rockets that flew in radar installed at Jicamarca and so-called equatorial quasi- low-latitude trajectories. periodic echoes. We present evidence suggesting that these Plasma irregularities located at typical E and F valley observations could be the first detection of this type of irreg- heights have been studied before using VHF radar observa- ularity made by instruments onboard a rocket. tions. Woodman and Chau(2001) were the first to character- Keywords. Ionosphere (equatorial ionosphere; plasma tem- ize irregular structures in E and lower F regions using obser- perature and density; plasma waves and instabilities) vations from the Jicamarca Radio Observatory (JRO). They used the term “Equatorial QuasiPeriodic” or EQP to label these irregular echoes. More recently, Chau and Hysell(2004) reported large- 1 Introduction scale plasma waves at high altitude in the E region over Jicamarca and around twilight. Using an aperture synthesis Many ionospheric studies using rocket-borne probes have fo- imaging technique, the authors were able to show a striking cused their attention on nighttime equatorial plasma irregu- and complex set of striations evidencing different levels of larities. A significant part of these studies has been devoted signal-to-noise ratio (SNR), representing a range of different to the analysis of irregularities located at typical F region electron density regions. heights (e.g., Rino et al., 1981; LaBelle et al., 1986; Jahn and Published by Copernicus Publications on behalf of the European Geosciences Union. 414 S. Savio Odriozola et al.: Rocket observation of equatorial plasma irregularities Figure 1. Rocket trajectory (a) and flight details (b). The blue parabola in (b) is the projection of the trajectory onto a vertical plane. In the equatorial region over Brazil, a statistical study with station in Alcântara (CLA) located at 2.4◦ S, 44.4◦ W (dip observations made during 581 nights (from 2001 to 2008) latitude 5.5◦ S), Brazil, on 8 December 2012 (LT D UT − 3). was conducted by Kherani et al.(2012) using a low-power The launch time (19:00 LT) was carefully selected in order to coherent scatter radar located at the São Luís equatorial sta- intercept irregular structures that might arise soon after sun- tion. Similar to the results of Woodman and Chau(2001), the set. Flight parameters and the rocket trajectory are shown in structures were observed during occurrences of an ascending Fig.1. irregular bottom-type or bottom-side F layer and at the same As can be seen, the trajectory was toward the magnetic time or prior to an ascending and well-developed plume. Fur- equator in the northeast. The horizontal range was ∼ 384 km, thermore, and unlike Jicamarca, the research showed that the and the apogee of the rocket reached typical F region alti- frequency of occurrence of this type of irregularity was ex- tudes (∼ 428 km). The flight was tracked by three radars over tremely low and the few observations of such events were 647 s. The rocket carried three instruments: a two-axis mag- concentrated in summer months (Southern Hemisphere) and netometer, a GPS receiver prototype and a conical Langmuir years of high solar activity. probe (CLP). Data from a GPS receiver confirm the vehicle’s In this work, the vertical distribution of electron density trajectory provided by the radars. From magnetometer data, was obtained using a Langmuir probe as a payload of a two- it was possible to estimate the rotation (∼ 5 rps) and preces- stage rocket, which flew toward the magnetic equator from sion (∼ 0:09 rps) of the rocket along the flight. the rocket launching station in Alcântara, Brazil. Both the up- leg and downleg profiles, showed small- and medium-scale 2.2 Digisonde observations plasma irregularities in the intermediate region between the E and F layers. Given the characteristics of these profiles, in ◦ ◦ our results we propose that these irregularities are the EQP Ground stations located at São Luís (2.6 S, 44.2 W, dip lat- ◦ ◦ ◦ ◦ irregularities only detected, so far, by VHF coherent scatter itude 6 S) and Fortaleza (3.9 S, 38.4 W, dip latitude 15 S) radars. In the next section, the rocket flight and payload de- regularly probe the ionosphere using digisondes at the same tails, ionosonde observations and Langmuir probe data will time of rocket launch. São Luís station is located only 35 km be presented. Later, our observations will be compared with south of CLA; therefore, it was used to monitor the ideal con- a range time intensity (RTI) map previously obtained at Jica- ditions (pre-launch rocket) that precede the bubble’s onset, marca Radio Observatory. We will conclude by summing up while Fortaleza station is positioned ∼ 684 km southeast of our results and considerations. the launch center. Evidence of the presence of plasma irreg- ularities was observed in the ionograms of both stations. A sequence of eight ionograms taken at São Luís around 2 Observations the time of launching are shown in Fig.2. Until 19:00 LT, ionograms over this station do not exhibit any spread echoes. 0 2.1 Rocket flight Minimum virtual height of the F layer (hminF), however, in- creases suddenly until a first manifestation of spreading in As part of the Iguaiba operation, a two-stage VS-30 Orion the echo received by the digisondes becomes visible around rocket was launched from the equatorial rocket launching 19:00 LT, indicating a fast upward movement of the F layer Ann. Geophys., 35, 413–422, 2017 www.ann-geophys.net/35/413/2017/ S. Savio Odriozola et al.: Rocket observation of equatorial plasma irregularities 415 Figure 2. Sequence of ionograms taken on 8 December 2012 (18:20–19:30 LT) at São Luís. Spread F begins around 19:00 LT. Figure 3. Sequence of ionograms taken on 8 December 2012 (18:20–19:30 LT) at Fortaleza. Spread F begins around 19:30 LT. prior to the sunset. The spread F condition is evident in the over Fortaleza is not as pronounced as that observed in São ionograms for the rest of the night. Luís. Figure3 shows the ionograms obtained at Fortaleza simul- From ionograms of both stations, it can be said that equa- taneously with those appearing in Fig.2. In this case the man- torial and low-latitude irregularities developed at the time of ifestation of a spread echo first appeared in a signal coming launch and after the rocket’s flight. from the north-northeast (echoes in light blue color). Sig- nals vertical above Fortaleza station show a range spread F at 19:30 LT or 30 min after the appearance of the same con- 0 dition at São Luís and the rocket’s launch. The rise of hminF www.ann-geophys.net/35/413/2017/ Ann. Geophys., 35, 413–422, 2017 416 S. Savio Odriozola et al.: Rocket observation of equatorial plasma irregularities Figure 4. Electron density profiles obtained with a Langmuir probe data onboard a VS-30 Orion rocket on 8 December 2012, 19:00 LT. 2.3 Langmuir probe measurements The Langmuir probe used in this experiment was mounted on the nose tip of the rocket and was able to operate alternately in swept and constant bias modes.
Recommended publications
  • Brazil's Accession to the Mtcr
    Wyn Q. Bowen Report: BRAZIL’S ACCESSION TO THE MTCR by Wyn Q. Bowen Wyn Q. Bowen is a Senior Research Associate of the Center for Nonproliferation Studies at the Monterey Institute of International Studies. He is also a Ph.D. candidate in International Relations at the University of Birmingham and is completing a dissertation on U.S. missile nonproliferation policy during the Bush administration. n October 1995, Brazil’s membership in the Mis- the design and construction of a center from which to sile Technology Control Regime (MTCR) was ap- launch the VLS at Alcantara (CLA), in the northern proved unanimously at the regime’s 10th plenary state of Maranhao.1 The VLS was to be developed us- I 2 meeting in Bonn, Germany. Acceptance in the MTCR ing technology derived from the Sonda rocket series. was the outcome of a series of policy changes initi- The central role of the military in the MECB during ated by Brazil in early 1994 to address international the 1980s, however, cast doubt over the true nature of missile proliferation concerns. This report consid- the space program. The Brazilian Commission for Space ers the past Brazilian rocket and missile activities that Activities (COBAE), responsible for overseeing and generated these concerns and the policy changes running the MECB, was chaired by the armed forces which Brazil undertook to gain acceptance in the chief of staff.3 The prominent role of the Air Force’s MTCR. The implications of Brazil’s membership in Aerospace Technical Center (CTA) in developing the the regime are also considered, along with some of VLS also suggested the military might have other rea- the missile proliferation concerns which continue to sons for developing space launch vehicles.
    [Show full text]
  • Aerospace-America-April-2019.Pdf
    17–21 JUNE 2019 DALLAS, TX SHAPING THE FUTURE OF FLIGHT The 2019 AIAA AVIATION Forum will explore how rapidly changing technology, new entrants, and emerging trends are shaping a future of flight that promises to be strikingly different from the modern global transportation built by our pioneers. Help shape the future of flight at the AIAA AVIATION Forum! PLENARY & FORUM 360 SESSIONS Hear from industry leaders and innovators including Christopher Emerson, President and Head, North America Region, Airbus Helicopters, and Greg Hyslop, Chief Technology Officer, The Boeing Company. Keynote speakers and panelists will discuss vertical lift, autonomy, hypersonics, and more. TECHNICAL PROGRAM More than 1,100 papers will be presented, giving you access to the latest research and development on technical areas including applied aerodynamics, fluid dynamics, and air traffic operations. NETWORKING OPPORTUNITIES The forum offers daily networking opportunities to connect with over 2,500 attendees from across the globe representing hundreds of government, academic, and private institutions. Opportunities to connect include: › ADS Banquet (NEW) › AVIATION 101 (NEW) › Backyard BBQ (NEW) › Exposition Hall › Ignite the “Meet”ing (NEW) › Meet the Employers Recruiting Event › Opening Reception › Student Welcome Reception › The HUB Register now aviation.aiaa.org/register FEATURES | APRIL 2019 MORE AT aerospaceamerica.aiaa.org The U.S. Army’s Kestrel Eye prototype cubesat after being released from the International Space Station. NASA 18 30 40 22 3D-printing solid Seeing the far Managing Getting out front on rocket fuel side of the moon drone traffi c Researchers China’s Chang’e-4 Package delivery alone space technology say additive “opens up a new could put thousands manufacturing is scientifi c frontier.” of drones into the sky, U.S.
    [Show full text]
  • 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]
  • 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]
  • Hybrid Rocket Propulsion
    CZECH TECHNICAL UNIVERSITY IN PRAGUE FACULTY OF TRANSPORTATION Department of Air Transport Bc. Tomáš Cáp HYBRID ROCKET PROPULSION Diploma Thesis 2017 1 2 3 4 Acknowledgements I would like to express my sincere thanks to my thesis advisor, doc. Ing. Jakub Hospodka, PhD., for valuable feedback and support during the process of creation of this thesis. Additionally, I am thankful for moral support extended by my family without which the process of writing this thesis would be significantly more difficult. Čestné prohlášení Prohlašuji, že jsem předloženou práci vypracoval samostatně a že jsem uvedl veškeré použité informační zdroje v souladu s Metodickým pokynem o etické přípravě vysokoškolských závěrečných prací. Nemám žádný závažný důvod proti užití tohoto školního díla ve smyslu § 60 Zákona č. 121/2000 Sb., o právu autorském, o právech souvisejících s právem autorským a o změně některých zákonů (autorský zákon). V Praze dne 29. 5. 2017 ……………………………… Tomáš Cáp 5 Abstrakt Autor: Bc. Tomáš Cáp Název práce: Hybrid Rocket Propulsion Škola: České vysoké učení technické v Praze, Fakulta dopravní Rok obhajoby: 2017 Počet stran: 56 Vedoucí práce: doc. Ing. Jakub Hospodka, PhD. Klíčová slova: hybridní raketový motor, raketový pohon, raketové palivo, komerční lety do vesmíru Cílem této diplomové práce je představení hybridního raketového pohonu coby perspektivní technologie, která do budoucna zřejmě výrazně ovlivní směřování kosmonautiky. Součástí práce je stručný popis konvenčních raketových motorů na tuhá a kapalná paliva a základní popis problematiky hybridních raketových motorů. V druhé části práce jsou zmíněny přibližné náklady na provoz těchto systémů a je provedeno srovnání těchto finančních nákladů v poměru k poskytovanému výkonu. V závěru jsou doporučeny oblasti možných využití vhodné pro hybridní raketové motory vzhledem k současnému stupni jejich technologické vyspělosti.
    [Show full text]
  • An Optimized Hybrid Rocket Motor for the SARA Platform Reentry System
    doi: 10.5028/jatm.2012.04032312 An Optimized Hybrid Rocket Motor for the SARA Platform Reentry System Pedro Luiz Kaled Da Cás, Cristiano Queiroz Vilanova, Manuel Nascimento Dias Barcelos Jr.*, Carlos Alberto Gurgel Veras Universidade de Brasília - Brasília/DF Brazil Abstract: This paper has described a system design process, based on a multidisciplinary optimization technique, of a conceptual optimized hybrid propellant rocket motor. The proposed engine could be a technological option for the reentry maneuvering system of the Brazilian recoverable satellite (SARA), which was designed by the Brazilian Institute of Aeronautics and Space. The resulting optimized propulsion system must be viewed as a proof of concept allowing comparison to more conventional technologies, i.e., liquid and solid motors. Design effort was conducted for hybrid SURSHOODQWVHQJLQHVEDVHGRQDOLTXHI\LQJIXHO VROLGSDUDI¿Q DQGWZRGLIIHUHQWR[LGL]HUV+2O2 KLJKWHVWSHUR[LGH and self-pressurizing N227KHPXOWLGLVFLSOLQDU\FRQ¿JXUDWLRQRSWLPL]DWLRQWHFKQLTXHZDVVXSSRUWHGRQJHRPHWULFDO operating parameters of the motor, rather than on performance, in order to facilitate subsequent design and fabrication. Results from the code presented a hybrid motor, which was considered a competitive alternative for the deboost engine when compared to the traditional chemical systems, solid and liquid bipropellant, and monopropellant. The estimated mass of the reentry system, for the cases addressed in this study, varied from 22 to 29 kg, which is lower than either liquid bipropellant or solid engines formerly proposed. Keywords:+\EULGURFNHWSURSXOVLRQ0XOWLSK\VLFVDQDO\VLV'HVLJQRSWLPL]DWLRQ INTRODUCTION The SARA satellite was conceived as a microgravity 300 km from the launch site. The system should be accelerated recoverable and reusable research platform by both Brazilian by a Brazilian VS-40 sounding rocket (Fig.
    [Show full text]
  • SPACE TRANSPORTATION Contents
    Chapter 5 SPACE TRANSPORTATION Contents Page Introduction. ..............103 The Space Transportation Industry . ................103 The providers of Space Transportation Services . .. ...103 Buyers of Space Transportation Services . ................122 Competition in Space Transportation . ......125 Development of Competition . ............125 Assessment of Demand . .................126 Nature of Competition . .. ...128 Effects of Competition . .. ....134 Cooperation in Space Transportation . ..............137 Current Policies. ........................138 Future Policy Options.. .. ....140 List of Tables Table No. Page 5-1. Ariane Flights . ..........115 5-2. Transportation Costs to Geosynchronous Orbit . ......................132 5-3. NASA vs. Arianespace Financing . ..............133 5-4. Companies That Contribute to Manufacturing Japanese Launch Vehicles ..139 List of Figures Figure No. Page 5-1. U.S. Launch vehicles . ..............104 5-2.The Hermes Spaceplane . ..................116 5-3. Foreign National Comparative Launch Vehicle Development. ..........118 5-4. Projection of Future Space Shuttle Demand Rockwell International. ...127 5-5. Outside Users Payload Model Battelle’s Columbus Laboratories . .......,128 5-6. Low Model Market Share by Launch Vehicle . ...............129 5-7. High Model Market Share by Launch Vehicle . .......................130 5-8. Arianespace Financing . ..133 5-9. Rockwell International Estimates That the Shuttle is Most Economical Over ELVs at High-Volume Operations. ............................135
    [Show full text]
  • Acquisition Story 54 Introduction 2 Who We Were 4 194Os 8 195Os 12
    table of contents Introduction 2 Who We Were 4 194Os 8 195Os 12 196Os 18 197Os 26 198Os 30 199Os 34 2OOOs 38 2O1Os 42 Historical Timeline 46 Acquisition Story 54 Who We Are Now 58 Where We Are Going 64 Vision For The Future 68 1 For nearly a century, innovation and reliability have been the hallmarks of two giant U.S. aerospace icons – Aerojet and Rocketdyne. The companies’ propulsion systems have helped to strengthen national defense, launch astronauts into space, and propel unmanned spacecraft to explore the universe. ➢ Aerojet’s diverse rocket propulsion systems have powered military vehicles for decades – from rocket-assisted takeoff for propeller airplanes during World War II – through today’s powerful intercontinental ballistic missiles (ICBMs). The systems helped land men on the moon, and maneuvered spacecraft beyond our solar system. ➢ For years, Rocketdyne engines have played a major role in national defense, beginning with powering the United States’ first ICBM to sending modern military communication satellites into orbit. Rocketdyne’s technology also helped launch manned moon missions, propelled space shuttles, and provided the main power system for the International Space Station (ISS). ➢ In 2013, these two rocket propulsion manufacturers became Aerojet Rocketydne, blending expertise and vision to increase efficiency, lower costs, and better compete in the market. Now, as an industry titan, Aerojet Rocketdyne’s talented, passionate employees collaborate to create even greater innovations that protect America and launch its celestial future. 2011 A Standard Missile-3 (SM-3) interceptor is being developed as part of the U.S. Missile Defense Agency’s sea-based Aegis Ballistic Missile Defense System.
    [Show full text]
  • ROCKETS and MISSILES Recent Titles in Greenwood Technographies
    ROCKETS AND MISSILES Recent Titles in Greenwood Technographies Sound Recording: The Life Story of a Technology David L. Morton Jr. Firearms: The Life Story of a Technology Roger Pauly Cars and Culture: The Life Story of a Technology Rudi Volti Electronics: The Life Story of a Technology David L. Morton Jr. ROCKETS AND MISSILES 1 THE LIFE STORY OF A TECHNOLOGY A. Bowdoin Van Riper GREENWOOD TECHNOGRAPHIES GREENWOOD PRESS Westport, Connecticut • London Library of Congress Cataloging-in-Publication Data Van Riper, A. Bowdoin. Rockets and missiles : the life story of a technology / A. Bowdoin Van Riper. p. cm.—(Greenwood technographies, ISSN 1549–7321) Includes bibliographical references and index. ISBN 0–313–32795–5 (alk. paper) 1. Rocketry (Aeronautics)—History. 2. Ballistic missiles—History. I. Title. II. Series. TL781.V36 2004 621.43'56—dc22 2004053045 British Library Cataloguing in Publication Data is available. Copyright © 2004 by A. Bowdoin Van Riper All rights reserved. No portion of this book may be reproduced, by any process or technique, without the express written consent of the publisher. Library of Congress Catalog Card Number: 2004053045 ISBN: 0–313–32795–5 ISSN: 1549–7321 First published in 2004 Greenwood Press, 88 Post Road West,Westport, CT 06881 An imprint of Greenwood Publishing Group, Inc. www.greenwood.com Printed in the United States of America The paper used in this book complies with the Permanent Paper Standard issued by the National Information Standards Organization (Z39.48–1984). 10987654321 For Janice P. Van Riper who let a starstruck kid stay up long past his bedtime to watch Neil Armstrong take “one small step” Contents Series Foreword ix Acknowledgments xi Timeline xiii 1.
    [Show full text]
  • May 5, 2016 IG-16-020
    May 5, 2016 IG-16-020 NASA’S INTERNATIONAL PARTNERSHIPS: CAPABILITIES, BENEFITS, AND CHALLENGES N A S A OFFICE OF INSPECTOR GENERAL MESSAGE FROM THE INSPECTOR GENERAL The Space Act of 1958 that created NASA identified the need to cooperate with “nations and groups of nations” in aeronautical and space activities as one of the Agency’s primary mission objectives. To this end, NASA currently manages more than 750 international agreements with 125 different countries, the flagship being the International Space Station, which after 15 years in low Earth orbit is expected to continue operating until at least 2024. These collaborative efforts have enhanced space-related knowledge through sharing of capabilities, expertise, and scientific research while cultivating positive working relations between nations. Moreover, as NASA missions become more complex and costly, it will be difficult for the Agency to achieve its ambitious goals without leveraging international partnerships, particularly for human exploration in deep space. This report examines NASA’s efforts to partner with foreign space agencies. We identified the space-related interests of more than a dozen space agencies around the world, examined their technical and financial capabilities, identified potential barriers to cooperation, and suggested possible ways to minimize those barriers. The observations we present are based on our analysis of information we received from NASA and firsthand from its foreign partners as well as information from studies prepared by NASA, our office, the Government Accountability Office, and other research, educational, and advisory organizations. In sum, we found that NASA faces significant challenges to its use of international partnerships. First, the process of developing agreements with foreign space agencies requires approval from the Department of State, which often takes many months, if not years, to complete.
    [Show full text]
  • Review of Space Activities in South America.Pdf
    Journal of Aeronautical History Revised 11 September 2018 Paper 2018/08 Review of Space Activities in South America Bruno Victorino Sarli, Space Generation Advisory Council, Brazil Marco Antonio Cabero Zabalaga, Space Generation Advisory Council, Bolivia Alejandro Lopez Telgie, Universidad de Concepción, Facultad de Ingeniería, Departamento de Ingeniería Mecánica, Chile Josué Cardoso dos Santos, São Paulo State University (FEG-UNESP), Brazil Brehme Dnapoli Reis de Mesquita, Federal Institute of Education, Science and Technology of Maranhão, Açailândia Campus, Brazil Avid Roman-Gonzalez, Space Generation Advisory Council, Peru Oscar Ojeda, Space Generation Advisory Council, Colombia Natalia Indira Vargas Cuentas, Space Generation Advisory Council, Bolivia Andrés Aguilar, Universidad Tecnológica Nacional Facultad Regional Delta, Argentina ABSTRACT This paper addresses the past and current efforts of the South American region in space. Space activities in the region date back to 1961; since then, South American countries have achieved a relatively modest capability through their national programs, and some international collaboration, with space activities in the region led primarily by the Brazilian and Argentinian space programs. In an era where missions explore the solar system and beyond, this paper focus on the participation of a region that is still in the early stages of its space technology development, yet has a considerable amount to offer in terms of material, specialized personnel, launch sites, and energy. In summary, this work presents a historical review of the main achievements in the South American region, and through analysis of past and present efforts, aims to project a trend for the future of space in South America. The paper also sets out current efforts of regional integration such as the South American Space Agency proposal.
    [Show full text]