NSIAD-91-194 Aerospace Plane Technology Contents
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Diapositiva 1
Associazione Politecnica Italiana in collaborazione con DIPARTIMENTO DI INGEGNERIA ELETTRICA, GESTIONALE E MECCANICA dell’Università degli Studi di Udine Lockheed F-104 Starfighter Tecnologia ed Eccellenza di un Mito dell’Aeronautica Militare 13 Settembre 2014 Alcune considerazioni introduttive ___________________________________________________________ Earth is the cradle of mankind, but man cannot live in the cradle forever La terra è la culla dell’umanità, ma l’uomo non puo’ vivere nella culla per sempre Kostantin E. Tsiolkovski, 1857-1935 scienziato russo, pionere dell’ingegneria spaziale Aeronautica: un secolo di storia 3 ___________________________________________________________ 17 dicembre 1903: Flyer Peso al decollo: 350 kg Passeggeri: 1 Autonomia: 150 m 27 aprile 2005: Airbus A380 Peso al decollo: 660’000 kg Passeggeri : 525-853 Autonomia : 15’100 km Lo spazio: un decennio di storia 4 ___________________________________________________________ 4 ottobre 1957: Sputnik Massa: 83 kg Diametro: 0.58 m 20 luglio 1969: l’uomo è sulla luna Peso al decollo: 3.038.000 kg Altezza/diametro: 111/10 m Il futuro dello spazio: nuovi sistemi di lancio ___________________________________________________________ Alcune considerazioni introduttive ___________________________________________________________ Perché l’aereo vola ? ___________________________________________________________ La portanza, la forza che consente ad un velivolo di staccarsi da terra e di raggiungere quote elevate, dipende dalla velocità del velivolo rispetto all'aria e dalla configurazione dell'ala. Superficie e inclinazione dell’ala, che vengono modificate attraverso il movimento degli elementi mobili (flap e slat, o ipersostentatori) posti alle estremità anteriori (bordo d'attacco) e posteriori (bordo di uscita). A velocità costante, l’incremento della curvatura dell’ala porta ad un aumento della portanza. La densità dell’aria diminuisce con l’aumentare della quota di volo (all'incirca si dimezza ogni 5 km). -
Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020
Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020 Christopher Baker NASA Space Technology Mission Directorate Flight Opportunities and Small Spacecraft Technology Program Executive National Aeronautics and Space Administration 1 CHANGING THE PACE OF SPACE Through Small Spacecraft Technology and Flight Opportunities, Space Tech is pursuing the rapid identification, development, and testing of capabilities that exploit agile spacecraft platforms and responsive launch capabilities to increase the pace of space exploration, discovery, and the expansion of space commerce. National Aeronautics and Space Administration 2 THROUGH SUBORBITAL FLIGHT The Flight Opportunities program facilitates rapid demonstration of promising technologies for space exploration, discovery, and the expansion of space commerce through suborbital testing with industry flight providers LEARN MORE: WWW.NASA.GOV/TECHNOLOGY Photo Credit: Blue Origin National Aeronautics and Space Administration 3 FLIGHT OPPORTUNITIES BY THE NUMBERS Between 2011 and today… In 2019 alone… Supported 195 successful fights Supported 15 successful fights Enabled 676 tests of payloads Enabled 47 tests of payloads 254 technologies in the portfolio 86 technologies in the portfolio 13 active commercial providers 9 active commercial providers National Aeronautics and Space Administration Numbers current as of March 1, 2020 4 TECHNOLOGY TESTED IN SUBORBITAL Lunar Payloads ISS SPACE IS GOING TO EARTH ORBIT, THE MOON, MARS, AND BEYOND Mars 2020 Commercial Critical Space Lunar Payload Exploration Services Solutions National Aeronautics and Space Administration 5 SUBORBITAL INFUSION HIGHLIGHT Commercial Lunar Payload Services Four companies selected as Commercial Lunar Payload Services (CPLS) providers leveraged Flight Opportunities-supported suborbital flights to test technologies that are incorporated into their landers and/or are testing lunar landing technologies under Flight Opportunities for others. -
Aviazione Termomeccanica
un fatturato di 129 miliardi di lire (- 4% parti di competenza per un analogo motore circa sul 1983) e chiude il bilancio 1984 con previsto da precedenti accordi con General un risultato positivo di 17,1 miliardi di lire Electric. dopo aver spesato ammortamenti per 6,6 Nel campo della propulsione navale è conti miliardi di lire e spese per ricerca e sviluppo nuata la produzione delle turbine da 30.000 per circa 1 miliardo di lire. CV per la Marina Italiana e Marine Stranie Le collegate O.ME.CA., con un fattura re. to di 70 miliardi di lire circa, e Ferrosud, con Infine, relativamente al piccolo motore un fatturato di circa 72 miliardi di lire, a turbina FA 150 - Argo è proseguita hanno chiuso il bilancio 1984 con risultati l’attività di sviluppo e prove al banco in vista positivi, rispettivamente per 3,8 e per 4 dell’utilizzazione quale “Auxiliary Power miliardi di lire. Unit” sul nuovo velivolo italo-brasiliano da appoggio tattico ravvicinato AMX. Per quanto attiene a nuove iniziative commerciali si segnala un accordo siglato Aviazione con Aeritalia per la commercializzazione congiunta di prodotti comuni. Nel corso del 1984, il Settore proseguen do un intenso programma di investimenti Nel 1984, Fiat Aviazione S.p.A. ha rivolti ad iniziative strategiche, di ricerca e realizzato un fatturato di 372 miliardi di lire progettazione, ha conseguito favorevoli ri (+8,8% sul 1983), ed un risultato netto sultati realizzando un incremento di fattura positivo di bilancio di 12,4 miliardi di lire, to e una consistenza del portafoglio ordini dopo aver stanziato ammortamenti per pari a due anni di attività. -
Nasa As an Instrument of U.S. Foreign Policy
CHAPTER 11 Nasa as an Instrument of U.S. Foreign Policy John Krige as space exploration,and NASA’s role in it in particular,had an effect on society, Hand, if so, on what aspects of it? And how do we measure any such impact? These are challenging questions indeed. The stakeholders in the huge American space program are multiple and include scientists; engineers; research, development, and launch facilities; industry; administrators; and many government agencies, not to speak of Congress and the U.S. taxpayer.The impacts of spaceflight vary widely, from adding to the stockpile of knowledge and stimulating innovation and industry, to training, education, and creating jobs and—if we move beyond the civilian sphere— to enhancing national security and intelligence gathering. And then there are the intangible, difficult to quantify cultural effects that range from inspiring a young girl to become an astronaut to building national pride and prestige in what are, after all, spectacular scientific and technological, managerial, and industrial achievements. This paper briefly considers one small, but I think important and often overlooked, corner of this vast panorama: the place of spaceflight in American foreign policy. I do not simply want to insist that naSa’s international programs have had an important impact as instruments of foreign policy.I also want to suggest that today they have a particularly significant political and cultural role to play in projecting a positive image of American power and American democracy abroad. In a world increasingly torn apart by conflicts over values—conflicts which history teaches us can seldom be resolved by force—i believe we overlook the potential of NASA as an instrument for American foreign policy at our peril. -
Sixty Years of Australia in Space
Journal & Proceedings of the Royal Society of New South Wales, vol. 153, part 1, 2020, pp. 46–57. ISSN 0035-9173/20/010046-12 Sixty years of Australia in space Kerrie Dougherty Space Humanities Department, International Space University, Strasbourg, France Email: [email protected] Abstract Australia’s involvement in space activities commenced in 1957, at the beginning of the Space Age, with space tracking and sounding rocket launches at Woomera. By 1960, Australia was considered one of the leading space-active nations and in 1967 became one of the earliest countries to launch its own satellite. Yet by 1980, Australia’s space prominence had dwindled, with the country lacking both a national space agency and a coherent national space policy. Despite attempts in the latter part of the 1980s to develop an Australian space industry, the lack of a coherent and consistent national space policy and an effective co-ordinating body, left Australia constantly “punching below its weight” in global space activities until the Twenty First Century. This paper will briefly examine the often-contradictory history of Australian space activities from 1957 to the announcement of the Australian Space Agency in 2017, providing background and context for the later papers in this issue. Introduction Launchpad: the Woomera or 60,000 years the Indigenous people of Rocket Range FAustralia have looked to the sky, using “If the Woomera Range did not already exist, the stars to determine their location, find the proposal that Australia should engage in their way across the land and mark the a program of civil space research would be passage of the seasons and the best times unrealistic”. -
Safety Consideration on Liquid Hydrogen
Safety Considerations on Liquid Hydrogen Karl Verfondern Helmholtz-Gemeinschaft der 5/JULICH Mitglied FORSCHUNGSZENTRUM TABLE OF CONTENTS 1. INTRODUCTION....................................................................................................................................1 2. PROPERTIES OF LIQUID HYDROGEN..........................................................................................3 2.1. Physical and Chemical Characteristics..............................................................................................3 2.1.1. Physical Properties ......................................................................................................................3 2.1.2. Chemical Properties ....................................................................................................................7 2.2. Influence of Cryogenic Hydrogen on Materials..............................................................................9 2.3. Physiological Problems in Connection with Liquid Hydrogen ....................................................10 3. PRODUCTION OF LIQUID HYDROGEN AND SLUSH HYDROGEN................................... 13 3.1. Liquid Hydrogen Production Methods ............................................................................................ 13 3.1.1. Energy Requirement .................................................................................................................. 13 3.1.2. Linde Hampson Process ............................................................................................................15 -
APRSAF22 Space Research and Development in the Philippines.Key
Space Research and Development in ! the Philippines EGULUS! R! SPACETECH SPACETECH! Dr. Rogel Mari Sese EGULUS! SPACETECH! RSPACETECH! ! Program Leader, National SPACE Development Program Focal Person, Philippine Space Science Education Program SPACETECH! SPACETECH! Challenges of Philippine Space R&D NO DIRECT ACCESS TO SPACE The Philippines has no direct access to space (e.g. satellites, launchers etc.) ! ! RELIANT ON SATELLITE DATA PROVIDERS Despite having two orbital slot allocations, we do not have any satellite in orbit; ! ! MINIMAL NUMBER OF TRAINED EXPERTS The country has a very small pool of trained astrophysicists, space scientists and engineers; ! ! SMALL SPACE R&D AND INDUSTRY No existing full capability to develop rockets and payloads to high altitudes and outer space. ! ! NO SPACE POLICY AND AGENCY The Philippines is not a signatory to most international space treaties and currently has no space agency to implement a cohesive space development strategy. Space-Related Programs and Activities Optical and Radio Astronomy since 1897 ! Rocket Development Program in the 1970s! AGILA-2 Telecommunications Satellite in 1990s! Committee on Space Technology and Applications (COSTA)! Philippine Space Science Education Program! 10-Year Baseline Research of Space Science and Technology Applications (SSTA)! Philippine Microsat Program and PEDRO Project! National Space Development and Utilization Policy and National Space Agency! National SPACE Development Program! Cost Benefit Analysis of a National Space Program Who conducts space research? Major universities through various programs -mostly through degree programs not directly related to space; ! Government agencies and institutions - as end-users and more focused on applications ! Private companies and NGOs - supports academe and government in R&D ! SSTA 10-Year Baseline Research Outcomes Functions of a space agency is distributed to various government agencies and units. -
Kennedy's Quest: Leadership in Space
Kennedy’s Quest: Leadership in Space Overview Topic: “Space Race” Grade Level: 9-12 Subject Area: US History Time Required: One class period. Goals/Rationale: The decision by the Kennedy Administration to make a manned lunar landing the major goal of the US space program derived from political as well as scientific motivations. In this lesson plan, students do a close reading of four primary sources related to the US space program in 1961, analyzing how and why public statements made by the White House regarding space may have differed from private statements made within the Kennedy Administration. Essential Questions: How was the “Space Race” connected to the Cold War? How and why might the White House communicate differently in public and in private? How might the Administration garner support for their policy? Objectives Students will be able to: analyze primary sources, considering the purpose of the source, the audience, and the occasion. analyze the differences in the tone or content of the primary sources. explain the Kennedy Administration’s arguments for putting a human on the Moon by the end of the 1960s. Connections to Curriculum (Standards) National History Standards US History, Era 9: Postwar United States (1945 to early 1970s) Standard 2A: The student understands the international origins and domestic consequences of the Cold War. Historical Thinking Skills Standard 2: Historical Comprehension Reconstruct the literal meaning of a historical passage. Appreciate historical perspectives . Historical Thinking Skills Standard 4: Historical Research Capabilities Support interpretations with historical evidence. Massachusetts History and Social Science Curriculum Frameworks USII [T.5] 1. Using primary sources such as campaign literature and debates, news articles/analyses, editorials, and television coverage, analyze the important policies and events that took place during the presidencies of John F. -
Status of the Space Shuttle Solid Rocket Booster
The Space Congress® Proceedings 1980 (17th) A New Era In Technology Apr 1st, 8:00 AM Status of The Space Shuttle Solid Rocket Booster William P. Horton Solid Rocket Booster Engineering Office, George C. Marshall Space Flight Center, Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Horton, William P., "Status of The Space Shuttle Solid Rocket Booster" (1980). The Space Congress® Proceedings. 3. https://commons.erau.edu/space-congress-proceedings/proceedings-1980-17th/session-1/3 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]. STATUS OF THE SPACE SHUTTLE SOLID ROCKET BOOSTER William P. Horton, Chief Engineer Solid Rocket Booster Engineering Office George C. Marshall Space Flight Center, AL 35812 ABSTRACT discuss retrieval and refurbishment plans for Booster reuse, and will address Booster status Two Solid Rocket Boosters provide the primary for multimission use. first stage thrust for the Space Shuttle. These Boosters, the largest and most powerful solid rocket vehicles to meet established man- BOOSTER CONFIGURATION rated design criteria, are unique in that they are also designed to be recovered, refurbished, It is appropriate to review the Booster config and reused. uration before describing the mission profile. The Booster is 150 feet long and is 148 inches The first SRB f s have been stacked on the in diameter (Figure 1), The inert weight Mobile Launch Platform at the Kennedy Space is 186,000 pounds and the propellant weight is Center and are ready to be mated with the approximately 1.1 million pounds for each External Tank and Orbiter in preparation for Booster. -
NASA's Strategic Direction and the Need for a National Consensus
NASA's Strategic Direction and the Need for a National Consensus NASAs Strategic Direction and the Need for a National Consensus Committee on NASAs Strategic Direction Division on Engineering and Physical Sciences THE NATIONAL ACADEMIES PRESS Washington, D.C. www.nap.edu PREPUBLICATION COPYSUBJECT TO FURTHER EDITORIAL CORRECTION Copyright © National Academy of Sciences. All rights reserved. NASA's Strategic Direction and the Need for a National Consensus THE NATIONAL ACADEMIES PRESS 500 Fifth Street, NW Washington, DC 20001 NOTICE: The project that is the subject of this report was approved by the Governing Board of the National Research Council, whose members are drawn from the councils of the National Academy of Sciences, the National Academy of Engineering, and the Institute of Medicine. The members of the committee responsible for the report were chosen for their special competences and with regard for appropriate balance. This study is based on work supported by Contract NNH10CC48B between the National Academy of Sciences and the National Aeronautics and Space Administration. Any opinions, findings, conclusions, or recommendations expressed in this publication are those of the authors and do not necessarily reflect the views of the agency that provided support for the project. International Standard Book Number-13: 978-0-309-XXXXX-X International Standard Book Number-10: 0-309-XXXXX-X Copies of this report are available free of charge from: Division on Engineering and Physical Sciences National Research Council 500 Fifth Street, NW Washington, DC 20001 Additional copies of this report are available from the National Academies Press, 500 Fifth Street, NW, Keck 360, Washington, DC 20001; (800) 624-6242 or (202) 334-3313; http://www.nap.edu. -
Design a Crew Module Drop Test Data Log Use This Data Log to Record the Results of Each Drop Test
National Aeronautics and DESIGN A Space Administration CREWYour Challenge MODULE Design and build a crew module model that will secure two astronaut figures during a drop test. Do First Watch the instructional video for this module: go.nasa.gov/34hVUvL Astronaut safety is of the highest Design Constraints importance. For Artemis missions, 1) The crew module must safely carry two astronauts. You must design and build a secure NASA’s Orion spacecraft must seat for the astronauts, without gluing or taping them in place. The astronauts should be able to support astronauts stay in their seats during each drop test. for weeks at a time and operate reliably in the harsh space 2) The crew module must fit into the container you chose. This item is simply for size environment. restraints. The crew module must not be dropped while inside the container. 3) The crew module must have one hatch that opens and closes easily. The hatch should remain shut during all drop tests. 4) Your crew module design should consider mass and strength. Mass is important in space travel. The heavier the crew module, the more expensive it is to build and, ultimately, to launch. NASA is looking for a lightweight but strong crew module. Ask and Imagine Think of ways to safely secure two astronauts inside of the crew module. Learn more: • What types of materials will protect the astronauts? Orion Capabilities for Deep Space • How can you reduce the impact on the crew module and astronauts? Enabled Crewed Artemis Moon • What essential elements are needed for crew safety? Missions go.nasa.gov/2GEMBN1 Top 5 Technologies needed for a LET’S GET STARTED! Spacecraft to Survive Deep Space 1. -
Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883
Journal of Aviation/Aerospace Education & Research Volume 13 Number 1 JAAER Fall 2003 Article 1 Fall 2003 Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883 Thomas Forenz Follow this and additional works at: https://commons.erau.edu/jaaer Scholarly Commons Citation Forenz, T. (2003). Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883. Journal of Aviation/Aerospace Education & Research, 13(1). https://doi.org/10.15394/ jaaer.2003.1559 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in Journal of Aviation/Aerospace Education & Research by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Forenz: Assessing the Evolution of the Airborne Generation of Thermal Lif Thermal Lift ASSESSING THE EVOLUTION OF THE AIRBORNE GENERATION OF THERMAL LIFT IN AEROSTATS 1783 TO 1883 Thomas Forenz ABSTRACT Lift has been generated thermally in aerostats for 219 years making this the most enduring form of lift generation in lighter-than-air aviation. In the United States over 3000 thermally lifted aerostats, commonly referred to as hot air balloons, were built and flown by an estimated 12,000 licensed balloon pilots in the last decade. The evolution of controlling fire in hot air balloons during the first century of ballooning is the subject of this article. The purpose of this assessment is to separate the development of thermally lifted aerostats from the general history of aerostatics which includes all gas balloons such as hydrogen and helium lifted balloons as well as thermally lifted balloons.