It Was Anything but Routine
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Ceramic Matrix Composites with Nano Technology–An Overview
International Review of Applied Engineering Research. ISSN 2248-9967 Volume 4, Number 2 (2014), pp. 99-102 © Research India Publications http://www.ripublication.com/iraer.htm Ceramic Matrix Composites with Nano Technology–An Overview Saubhagya Sharma, Samresh Kumar Shashi and Vikram Tomar Department of Material Science & Nano Technology, University of Petroleum & Energy Studies, Dehradun, Uttrakhand. Abstract Ceramic matrix composites (CMCs) are promising materials for use in high temperature structural applications. This class of materials offers high strength to density ratios. Also, their higher temperature capability over conventional super alloys may allow for components that require little or no cooling. This benefit can lead to simpler component designs and weight savings. These materials can also contribute in increasing the operating efficiency due to higher operating temperatures being achieved. Using carbon/carbon composites with the help of Nanotechnology is more beneficial in structural engineering and can decrease the production cost. They can withstand high stresses and temperatures than the traditional alumina, silicon carbide which fracture easily under mechanical loads Fundamental work in processing, characterization and analysis is important before the structural properties of this new class of Nano composites can be optimized. The fields of the Nano composite materials have received a lot of attention to scientists and engineers in recent years. The fabrication of such composites using Nano technology can make a revolution in the field of material science engineering and can make the composites able to be used in long lasting applications. 1. Introduction As we know that Composite materials are the type of materials that are formed by combining two or more materials of different physical and chemical properties. -
A Perspective on the Design and Development of the Spacex Dragon Spacecraft Heatshield
A Perspective on the Design and Development of the SpaceX Dragon Spacecraft Heatshield by Daniel J. Rasky, PhD Senior Scientist, NASA Ames Research Center Director, Space Portal, NASA Research Park Moffett Field, CA 94035 (650) 604-1098 / [email protected] February 28, 2012 2 How Did SpaceX Do This? Recovered Dragon Spacecraft! After a “picture perfect” first flight, December 8, 2010 ! 3 Beginning Here? SpaceX Thermal Protection Systems Laboratory, Hawthorne, CA! “Empty Floor Space” December, 2007! 4 Some Necessary Background: Re-entry Physics • Entry Physics Elements – Ballistic Coefficient – Blunt vs sharp nose tip – Entry angle/heating profile – Precision landing reqr. – Ablation effects – Entry G’loads » Blunt vs Lifting shapes – Lifting Shapes » Volumetric Constraints » Structure » Roll Control » Landing Precision – Vehicle flight and turn-around requirements Re-entry requires specialized design and expertise for the Thermal Protection Systems (TPS), and is critical for a successful space vehicle 5 Reusable vs. Ablative Materials 6 Historical Perspective on TPS: The Beginnings • Discipline of TPS began during World War II (1940’s) – German scientists discovered V2 rocket was detonating early due to re-entry heating – Plywood heatshields improvised on the vehicle to EDL solve the heating problem • X-15 Era (1950’s, 60’s) – Vehicle Inconel and Titanium metallic structure protected from hypersonic heating AVCOAT » Spray-on silicone based ablator for acreage » Asbestos/silicone moldable TPS for leading edges – Spray-on silicone ablator -
Chapter Fourteen Men Into Space: the Space Race and Entertainment Television Margaret A. Weitekamp
CHAPTER FOURTEEN MEN INTO SPACE: THE SPACE RACE AND ENTERTAINMENT TELEVISION MARGARET A. WEITEKAMP The origins of the Cold War space race were not only political and technological, but also cultural.1 On American television, the drama, Men into Space (CBS, 1959-60), illustrated one way that entertainment television shaped the United States’ entry into the Cold War space race in the 1950s. By examining the program’s relationship to previous space operas and spaceflight advocacy, a close reading of the 38 episodes reveals how gender roles, the dangers of spaceflight, and the realities of the Moon as a place were depicted. By doing so, this article seeks to build upon and develop the recent scholarly investigations into cultural aspects of the Cold War. The space age began with the launch of the first artificial satellite, Sputnik, by the Soviet Union on October 4, 1957. But the space race that followed was not a foregone conclusion. When examining the United States, scholars have examined all of the factors that led to the space technology competition that emerged.2 Notably, Howard McCurdy has argued in Space and the American Imagination (1997) that proponents of human spaceflight 1 Notably, Asif A. Siddiqi, The Rocket’s Red Glare: Spaceflight and the Soviet Imagination, 1857-1957, Cambridge Centennial of Flight (Cambridge: Cambridge University Press, 2010) offers the first history of the social and cultural contexts of Soviet science and the military rocket program. Alexander C. T. Geppert, ed., Imagining Outer Space: European Astroculture in the Twentieth Century (New York: Palgrave Macmillan, 2012) resulted from a conference examining the intersections of the social, cultural, and political histories of spaceflight in the Western European context. -
Xii Multifunctional Composites 11 Thermal Protection Systems
xii Multifunctional Composites 11 Thermal protection systems, Maurizio Natali, Luigi Torre, and Jos´e Maria Kenny 337 11.1 The hyperthermal environment . 337 11.2 Non-ablative TPS materials . 339 11.2.1 NA-TPS on the Space Shuttle . 339 11.2.2 SSO reusable surface insulation . 341 11.2.3 Conclusion remarks on non-ablative TPS materials . 342 11.3 High temperature composites as polymeric ablatives . 342 11.4 Testing facilities . 348 11.4.1 The oxy-acetylene torch testbed - OATT . 349 11.4.2 The simulated solid rocket motor - SSRM . 349 11.4.3 Plasma jet torches . 351 11.4.4 Recession rate sensing techniques for TPSs . 352 11.5 PAs as thermal insulating materials . 356 11.5.1 Rigid HSMs . 356 11.5.2 Flexible HSMs for TPSs . 356 11.5.3 Elastomeric HSMs for SRMs . 357 11.6 Phenolic impregnated carbon ablators . 359 11.7 Differences between FRPAs and LCAs . 360 11.8 Nanostructured ablative materials . 360 11.8.1 Nanosilica as filler for traditional and nanostructured ablatives 363 Table of Contents xiii 11.8.2 Carbon nanofilaments based NRAMs . 366 11.9 Conclusions . 368 Bibliography . 369 Chapter 11 Thermal protection systems Maurizio Natali, Luigi Torre, and Jos´eMaria Kenny University of Perugia, Perugia, Italy Abstract Ablative materials play a vital role for the entire aerospace industry. Although some non-polymeric materials have been successfully used as ablatives, polymer ablatives (PA) represent the most versatile class of thermal protection system (TPS) materials. Compared with oxide, inorganic polymer, and metal based TPS materials, PAs have some intrinsic advantages, such as high heat shock resistance and low density. -
Highly Reliable 3-Dimensional Woven Thermal Protection System for Mars Sample Return
Highly Reliable 3-Dimensional Woven Thermal Protection System for Mars Sample Return Don Ellerby Presenting for Keith Peterson [email protected] (512) 650-0885 Co-Authors (alphabetical by last name), E. Christiansen, D. Ellerby, P. Gage, M. Gasch, D. Prabhu, J. Vander Kam , E. Venkatapathy, T. W hite This work is funded by NASA Ames IRAD PI: E. Venkatapathy ; Technical Lead: K. Peterson; 1 3D Woven for MSR - Overview • The MSR Challenge: – Reliability requirements for a Mars Sample Return (MSR) Earth Entry Vehicle (EEV) are expected to be more stringent than any mission flown to date. • This flows down to all EEV subsystems, including heat-shield TPS • Likely to be the key driver for design decisions in many subsystem trades. • The MSR formulation is holding an option to on-ramp a 3D-woven system. The goal of this effort is to: –Provide a recommended 3D woven TPS architecture for MSR using Risk Informed Decision Making (RIDM). • Risk Informed DeCision Making (RIDM): – MSR formulation will institute RIDM processes to select configurations it pursues in future design cycles. • RIDM is a deliberative process that uses a diverse set of performance measures, together with other considerations, to inform decision making. – RIDM acknowledges the inevitable gaps in technical information, and the need for incorporating the cumulative wisdom of experienced personnel to integrate technical and nontechnical factors in order to produce sound decisions. 2 Why 3D Woven on MSR? • All TPS systems under consideration have their own set of challenges: – Carbon-Carbon (Hot Structure): • Certification of thermal-structural performance during re-entry and at temperature under the high strain landing impact environment will be challenging. -
Aerothermodynamic Design of the Mars Science Laboratory Heatshield
Aerothermodynamic Design of the Mars Science Laboratory Heatshield Karl T. Edquist∗ and Artem A. Dyakonovy NASA Langley Research Center, Hampton, Virginia, 23681 Michael J. Wrightz and Chun Y. Tangx NASA Ames Research Center, Moffett Field, California, 94035 Aerothermodynamic design environments are presented for the Mars Science Labora- tory entry capsule heatshield. The design conditions are based on Navier-Stokes flowfield simulations on shallow (maximum total heat load) and steep (maximum heat flux, shear stress, and pressure) entry trajectories from a 2009 launch. Boundary layer transition is expected prior to peak heat flux, a first for Mars entry, and the heatshield environments were defined for a fully-turbulent heat pulse. The effects of distributed surface roughness on turbulent heat flux and shear stress peaks are included using empirical correlations. Additional biases and uncertainties are based on computational model comparisons with experimental data and sensitivity studies. The peak design conditions are 197 W=cm2 for heat flux, 471 P a for shear stress, 0.371 Earth atm for pressure, and 5477 J=cm2 for total heat load. Time-varying conditions at fixed heatshield locations were generated for thermal protection system analysis and flight instrumentation development. Finally, the aerother- modynamic effects of delaying launch until 2011 are previewed. Nomenclature 1 2 2 A reference area, 4 πD (m ) CD drag coefficient, D=q1A D aeroshell diameter (m) 2 Dim multi-component diffusion coefficient (m =s) ci species mass fraction H total enthalpy -
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www.arianespace.com www.starsem.com www.avio Arianespace’s eighth launch of 2021 with the fifth Soyuz of the year will place its satellite passengers into low Earth orbit. The launcher will be carrying a total payload of approximately 5 518 kg. The launch will be performed from Baikonur, in Kazakhstan. MISSION DESCRIPTION 2 ONEWEB SATELLITES 3 Liftoff is planned on at exactly: SOYUZ LAUNCHER 4 06:23 p.m. Washington, D.C. time, 10:23 p.m. Universal time (UTC), LAUNCH CAMPAIGN 4 00:23 a.m. Paris time, FLIGHT SEQUENCES 5 01:23 a.m. Moscow time, 03:23 a.m. Baikonur Cosmodrome. STAKEHOLDERS OF A LAUNCH 6 The nominal duration of the mission (from liftoff to separation of the satellites) is: 3 hours and 45 minutes. Satellites: OneWeb satellite #255 to #288 Customer: OneWeb • Altitude at separation: 450 km Cyrielle BOUJU • Inclination: 84.7degrees [email protected] +33 (0)6 32 65 97 48 RUAG Space AB (Linköping, Sweden) is the prime contractor in charge of development and production of the dispenser system used on Flight ST34. It will carry the satellites during their flight to low Earth orbit and then release them into space. The dedicated dispenser is designed to Flight ST34, the 29th commercial mission from the Baikonur Cosmodrome in Kazakhstan performed by accommodate up to 36 spacecraft per launch, allowing Arianespace and its Starsem affiliate, will put 34 of OneWeb’s satellites bringing the total fleet to 288 satellites Arianespace to timely deliver the lion’s share of the initial into a near-polar orbit at an altitude of 450 kilometers. -
Why NASA Consistently Fails at Congress
W&M ScholarWorks Undergraduate Honors Theses Theses, Dissertations, & Master Projects 6-2013 The Wrong Right Stuff: Why NASA Consistently Fails at Congress Andrew Follett College of William and Mary Follow this and additional works at: https://scholarworks.wm.edu/honorstheses Part of the Political Science Commons Recommended Citation Follett, Andrew, "The Wrong Right Stuff: Why NASA Consistently Fails at Congress" (2013). Undergraduate Honors Theses. Paper 584. https://scholarworks.wm.edu/honorstheses/584 This Honors Thesis is brought to you for free and open access by the Theses, Dissertations, & Master Projects at W&M ScholarWorks. It has been accepted for inclusion in Undergraduate Honors Theses by an authorized administrator of W&M ScholarWorks. For more information, please contact [email protected]. The Wrong Right Stuff: Why NASA Consistently Fails at Congress A thesis submitted in partial fulfillment of the requirement for the degree of Bachelors of Arts in Government from The College of William and Mary by Andrew Follett Accepted for . John Gilmour, Director . Sophia Hart . Rowan Lockwood Williamsburg, VA May 3, 2013 1 Table of Contents: Acknowledgements 3 Part 1: Introduction and Background 4 Pre Soviet Collapse: Early American Failures in Space 13 Pre Soviet Collapse: The Successful Mercury, Gemini, and Apollo Programs 17 Pre Soviet Collapse: The Quasi-Successful Shuttle Program 22 Part 2: The Thin Years, Repeated Failure in NASA in the Post-Soviet Era 27 The Failure of the Space Exploration Initiative 28 The Failed Vision for Space Exploration 30 The Success of Unmanned Space Flight 32 Part 3: Why NASA Fails 37 Part 4: Putting this to the Test 87 Part 5: Changing the Method. -
Communication Skills: English
HEZKUNTZA SAILA DEPARTAMENTO DE EDUCACIÓN GRADUATE IN SECONDARY EDUCATION OPEN TEST COMMUNICATION SKILLS: ENGLISH NOVEMBER 2017 SURNAMES AND NAME: ___________________________________________ SIGNATURE: Donostia-San Sebastián, 1 - 01010 VITORIA-GASTEIZ Tef. 945 01 83 66 - Fax 945 01 83 36 - E-mail: [email protected] GRADUATE IN SECONDARY EDUCATION - COMMUNICATION SKILLS: ENGLISH - OPEN TEST- HOLIDAYS IN SPACE Make your reservation now!!!! Astronauts are not the only people travelling to space anymore. Everyone can buy a ticket and spend their holidays in space, as long as they have the money! The space tourism industry is officially open for business and tickets cost at least $20 million for a one-week stay in space. Russia made American businessman Denis Tito the world's first space tourist when he sent him to the International Space Station on April 30, 2001. Russia's Mir space station was supposed to be the first destination for space tourists. But in March 2001, the Russian Aerospace Agency brought Mir down into the Pacific Ocean and this temporarily delayed tourist trips into space. Space tourism will be one of the most lucrative industries in the 21st century. There are already several space tourism companies planning to build suborbital vehicles and orbital cities within the next two decades. These companies have invested millions, believing that the space tourism industry is about to take off. However, there seem to be big difficulties. How will ordinary people react to life in space? Today's astronauts spend months training before going into space. They have to be in top form too. Holidays in space will not be for tomorrow, that is certain; but will they finally become true in the more distant future? Adapted from: http://science.howstuffworks.com/space-tourism.htm GRADUATE IN SECONDARY EDUCATION - COMMUNICATION SKILLS: ENGLISH - OPEN TEST- 1. -
Understanding Socio-Technical Issues Affecting the Current Microgravity Research Marketplace
Understanding Socio-Technical Issues Affecting the Current Microgravity Research Marketplace The MIT Faculty has made this article openly available. Please share how this access benefits you. Your story matters. Citation Joseph, Christine and Danielle Wood. "Understanding Socio- Technical Issues Affecting the Current Microgravity Research Marketplace." 2019 IEEE Aerospace Conference, March 2019, Big Sky, Montana, USA, Institute of Electrical and Electronics Engineers, June 2019. © 2019 IEEE As Published http://dx.doi.org/10.1109/aero.2019.8742202 Publisher Institute of Electrical and Electronics Engineers (IEEE) Version Author's final manuscript Citable link https://hdl.handle.net/1721.1/131219 Terms of Use Creative Commons Attribution-Noncommercial-Share Alike Detailed Terms http://creativecommons.org/licenses/by-nc-sa/4.0/ Understanding Socio-Technical Issues Affecting the Current Microgravity Research Marketplace Christine Joseph Danielle Wood Massachusetts Institute of Technology Massachusetts Institute of Technology 77 Massachusetts Ave 77 Massachusetts Ave Cambridge, MA 02139 Cambridge, MA 02139 [email protected] [email protected] Abstract— For decades, the International Space Station (ISS) 1. INTRODUCTION has operated as a bastion of international cooperation and a unique testbed for microgravity research. Beyond enabling For anyone who is a teenager in October 2019, the insights into human physiology in space, the ISS has served as a International Space Station has been in operation and hosted microgravity platform for numerous science experiments. In humans for the entirety of that person’s life. The platform has recent years, private industry has also been affiliating with hosted a diverse spectrum of microgravity, human space NASA and international partners to offer transportation, exploration, technology demonstration, and education related logistics management, and payload demands. -
Soyuz Launch Brochure
Incredible Adventures is excited to offer a unique opportunity – a chance to visit the famous Baikonur Cosmodrome and observe a manned launch of a Russian Soyuz spacecraft. You’ll be completely immersed in the electric atmosphere surrounding a launch. You’ll explore Baikonur’s launch sites, museums and most historic places. Join IA for an Incredible Space Adventure. Highlights of Your Incredible Baikonur Adventure 800-644-7382 or 941-346-2603 www.incredible-adventures.com Observe roll-out and installation of the Soyuz rocket at launch pad. Attend international press conference of main and back- up crews. See the farewell of the crew at the cosmonaut hotel. Hear crew's ready-to-go official report. See launch of the Soyuz rocket, something you’ll never forget. Incredible Baikonur Adventure Day 1 Meet IA representative at the airport. Flight from Moscow to Baikonur .Transfer to the hotel. Time to relax. Day 2 Breakfast in the hotel Transfer to Baikonur Cosmodrome Roll-out of the Soyuz Rocket. (Follow the Soyuz to its launch site.) Observe installation of the rocket on the launch pad. Visit to the integration building of Soyuz and Progress spaceships. Transfer back to town. Visit to the International Space School. 9 Day 3 Breakfast in the hotel. Visit Museum of History Cosmodrome Baikonur. Enjoy general sightseeing in the town of Baikonur (learn history of the town, visit memorials and monuments). Transfer to Cosmonaut hotel. International press conference with the main and backup crews of Soyuz-TMA vehicle. Walk along the historical alley of Cosmonauts where personalized trees are planted. -
A Legal Regime for Space Tourism: Creating Legal Certainty in Outer Space Zhao Yun
Journal of Air Law and Commerce Volume 74 | Issue 4 Article 6 2009 A Legal Regime for Space Tourism: Creating Legal Certainty in Outer Space Zhao Yun Follow this and additional works at: https://scholar.smu.edu/jalc Recommended Citation Zhao Yun, A Legal Regime for Space Tourism: Creating Legal Certainty in Outer Space, 74 J. Air L. & Com. 959 (2009) https://scholar.smu.edu/jalc/vol74/iss4/6 This Article is brought to you for free and open access by the Law Journals at SMU Scholar. It has been accepted for inclusion in Journal of Air Law and Commerce by an authorized administrator of SMU Scholar. For more information, please visit http://digitalrepository.smu.edu. A LEGAL REGIME FOR SPACE TOURISM: CREATING LEGAL CERTAINTY IN OUTER SPACE DR. ZHAO YUN* 'Just tell me the general idea you have in mind-the idea Sven and my daughterkeep so mysteriously to themselves. What is this thing that's so revolutionary and daring? Fantastic and at the same time logical? I'm quoting, of course, my daughter." He looked steadily at Lee. His eyes brightened as if an inner light had been turned on. Lee glanced at the architect and the girl. He found response in theirfaces. "I need your assistance in building a hotel in outer space," he said artlessly.' I. INTRODUCTION A STORY LIKE the above must be the truly classic scene for space futurists. Outer space exhibits an unlimited source for imaginative science fiction writers. Earlier in the mid-nine- teenth century, a number of science fiction stories were written showing the rich imagination from renowned authors.2 Space tourism was among the most popular topics for those writers.3 But no one has taken this idea so seriously as in the late twenti- eth century.