Additive Manufacturing for Space : Status and Promises

Total Page:16

File Type:pdf, Size:1020Kb

Additive Manufacturing for Space : Status and Promises This document is downloaded from DR‑NTU (https://dr.ntu.edu.sg) Nanyang Technological University, Singapore. Additive manufacturing for space : status and promises Sacco, Enea; Moon, Seung Ki 2019 Sacco, E., & Moon, S. K. (2019). Additive manufacturing for space : status and promises. The International Journal of Advanced Manufacturing Technology, 105(10), 4123‑4146. doi:10.1007/s00170‑019‑03786‑z https://hdl.handle.net/10356/141133 https://doi.org/10.1007/s00170‑019‑03786‑z © 2019 Springer‑Verlag London Ltd., part of Springer Nature. This is a post‑peer‑review, pre‑copyedit version of an article published in The International Journal of Advanced Manufacturing Technology. The final authenticated version is available online at: http://dx.doi.org/10.1007/s00170‑019‑03786‑z Downloaded on 05 Oct 2021 19:03:29 SGT Noname manuscript No. (will be inserted by the editor) Additive Manufacturing for Space: Status and Promises Enea Sacco · Seung Ki Moon Received: date / Accepted: date Abstract Additive Manufacturing (AM) or 3D print- 1 Introduction ing is a manufacturing technique where successive lay- ers of material are layered to produce parts. The design There are various techniques used to manufacture ob- freedom afforded by AM is ideal for the space indus- jects such as casting, coating, moulding, forming, ma- try, where part production is low volume and highly chining, and joining. Most of these processes involve customized. The objective of this paper is to review re- subtractive manufacturing, the process of removing ma- search in the area of Additive Manufacturing For Space terial in order to manufacture a final object. Additive (AMFS) in all areas, from propulsion to electronics to Manufacturing (AM), or 3D Printing (3DP), does the printing of habitats, and to identify the gaps and direc- opposite: successive layers of material are added one on tions in the research. In this paper we investigate the top of the other until the object is complete [1]. AMFS research by splitting it into two domains: space In the 1980's an early form of Stereolithography and ground-based. Space-based AMFS has been per- (SLA) [2] for producing plastic prototypes was devel- formed on the International Space Station using poly- oped to help visualization of parts during development. mers and we also discuss the future of in-space AM, a From these beginnings came many other techniques and subject closely related to more general in-space manu- machines that can be used to manufacture both func- facturing. The ground-based research is split into three tional parts and prototypes, for example Fused De- categories based on the printing material: metal, poly- position Modeling (FDM) [3], Selective Laser Melting mer, and other. The last category includes regolith, (SLM) [4], Selective Laser Sintering (SLS) [5], Digital cement, and ceramic. This paper explores AMFS by Light Processing (DLP) [6], and Rapid Freeze Prototyp- bringing together as much research information as pos- ing (RFP) [7]. Although all these forms of 3DP work sible using a combination of papers, presentations, and using the same basic concept, the key differences are in news articles. We expect that the paper will allow the the printing process and the materials used. reader to gain an understanding of the current status 3DP's main strength is removing a lot of the limita- of AMFS research and will contribute to the field as a tions present with previous manufacturing techniques reference and research guidelines. and allowing unparalleled design freedom. This greatly reduces the time and cost of development, making AM Keywords 3D Printing · Additive Manufacturing · an integral part of future manufacturing systems. 3DP AM Certification · Satellite · Space · Spacecraft is especially relevant in the production of complex and Enea Sacco · Moon Seung Ki (corresponding author) customized structures that used to be hard if not im- Singapore Centre for 3D Printing, School of Mechanical and possible to make [8,9]. Aerospace Engineering, Nanyang Technological University, 50 Nanyang Avenue, Singapore A sector that is poised to greatly benefit from AM is E-mail: [email protected] the space industry. Almost everything in space is cus- tom made so it is ideal for this manufacturing tech- nology. Space entities have begun using AM in a va- riety of applications broadly for two reasons. Firstly, mass savings from 40% to 90% [10] are possible and mass is directly related to cost (since more massive There is also the fact that governmental agencies spacecraft require more fuel and thrust). Secondly, AM like NASA and ESA are at times not able to release can manufacture complex parts much faster than tradi- sensitive information to the public so cannot go into tional manufacturing, reducing fabrication times from much detail. Private companies such as Space-X, Boe- one year to only 4 months [11]. Agencies like National ing, Thales Alenia Space (TAS), and Airbus usually Aeronautics and Space Administration (NASA) and Eu- release even less details, most research news coming in ropean Space Agency (ESA) have been conducting re- the form of press releases and finished products whose search into how to use AM in a variety of space related details are protected by intellectual copyrights. Finally, applications, from using it to print CubeSat propulsion there are relatively few research institutions such as systems [12], to printing ceramics [13], to using Laser universities that specialize in AMFS, most of the re- Engineered Net Shaping (LENS) [14] with Lunar and search is in general AM. Should the reader wish to, Martian regolith [15], to potentially printing an entire more specific review papers can be found for example spacecraft in orbit [16]. Regolith is the term used to on processes [18,14], materials [19,20], simulation and describe the lunar soil [17] but can be used to also for modelling [21,1], and cost models [22,23]. the Martian soil. There is currently only one way to print in space and Mass use of AM in the space industry has not oc- this has been used to test AM in microgravity to great curred yet though. This is mainly because of the diffi- success but due to the difficulties in performing space- culty in modelling the manufacturing process and pre- based research, most research is still ground based. It dicting the properties of printed parts. This leads to a should be noted that there are instances when authors lack of standardization and therefore limited use in the discuss both space and aerospace AM research. These space industry. have been included in this paper since they are typically Efforts have been made in recent years to character- from agencies like NASA. ize and model the properties of parts made with AM. This paper is organized as follows: first an introduc- This has proven to be difficult since there is an inherent tion will be given on the importance of mass savings for variability in the nature of 3DP that makes modelling the space industry in section 2. Then section 3 is a dis- complicated. The variability comes from many sources cussion of the usage of new technologies in the space but despite this progress has been made in characteriz- sector. Next the paper is split into two broad sections, ing AM materials and efforts are being made to model section 4 covers AMFS research performed in space and and predict the material properties [1]. the future of in-orbit manufacturing. Section 5 then dis- The goal of the current study is to provide an overview cusses the research done on the ground divided by ma- of the state of AM research that is aimed directly at use terial used during printing: metal, polymer, and other. in the space sector, referred to Additive Manufacturing Lastly the research gaps are highlighted in section 6 For Space (AMFS) research. This allows the discussion and the conclusion can be found in section 8. to be specifically about the accomplishments and gaps in AM research whose end goal is use in some aspect of space related applications, from launchers to habitat 2 The importance of mass reductions for building on extraterrestrial planets. Trends and knowl- spacecraft edge gaps will be identified and discussed in an effort to highlight the areas where more research is needed so A variety of materials are used in spacecraft, including that products with higher accuracy, better quality and [24]: desired properties can be produced for use in space. { Ceramic matrix composites It must be noted that although an attempt has been { Various types of carbon composites made to make this paper as comprehensive as possi- { Kapton ble, it does not cover all AMFS due to the sparsity { Teflon of details when in comes to research in this specific { Aluminium alloys area. For example some references are presentations { Glass given by NASA personnel at occasions where no pro- { Stainless steel ceedings were printed, therefore these sources lack de- { Inconel alloys tails that research papers would have. NASA has pub- { Various types of plastics lished these presentations and other sources on their server (https://ntrs.nasa.gov/) and the classifica- Some of these are used only in small amounts, such as tion numbers have been provided. gold and silver, and therefore don't add much weight. Materials such as plastics by their nature don't weigh very much so they also don't add much weight. Alu- the spacecraft is as small as possible, the mass ratio minium, steel, and inconel on the other hand add a lot increases and therefore the ∆v budget increases for a of weight because large parts are built out these mate- given amount of fuel. rials, such as the structure and nozzles. Spacecraft so far have been built using traditional methods but this section briefly describes the basics of orbits and thrusters in an effort to emphasize one, if not the main, way that 3DP can substantially help to reduce costs: mass savings for spacecraft.
Recommended publications
  • The Space Elevator NIAC Phase II Final Report March 1, 2003
    The Space Elevator NIAC Phase II Final Report March 1, 2003 Bradley C. Edwards, Ph.D. Eureka Scientific [email protected] The Space Elevator NIAC Phase II Final Report Executive Summary This document in combination with the book The Space Elevator (Edwards and Westling, 2003) summarizes the work done under a NASA Institute for Advanced Concepts Phase II grant to develop the space elevator. The effort was led by Bradley C. Edwards, Ph.D. and involved more than 20 institutions and 50 participants at some level. The objective of this program was to produce an initial design for a space elevator using current or near-term technology and evaluate the effort yet required prior to construction of the first space elevator. Prior to our effort little quantitative analysis had been completed on the space elevator concept. Our effort examined all aspects of the design, construction, deployment and operation of a space elevator. The studies were quantitative and detailed, highlighting problems and establishing solutions throughout. It was found that the space elevator could be constructed using existing technology with the exception of the high-strength material required. Our study has also found that the high-strength material required is currently under development and expected to be available in 2 years. Accepted estimates were that the space elevator could not be built for at least 300 years. Colleagues have stated that based on our effort an elevator could be operational in 30 to 50 years. Our estimate is that the space elevator could be operational in 15 years for $10B. In any case, our effort has enabled researchers and engineers to debate the possibility of a space elevator operating in 15 to 50 years rather than 300.
    [Show full text]
  • A Sample AMS Latex File
    Riot, V. J. et al. (2021): JoSS, Vol. 10, No. 1, pp. 995–1006 (Peer-reviewed article available at www.jossonline.com) www.adeepakpublishing.com www. JoSSonline.com Lessons Learned Using Iridium to Com- municate with a CubeSat in Low Earth Orbit Vincent J. Riot, Lance M. Simms, and Darrell Carter Lawrence Livermore National Laboratory Livermore, CA, USA Abstract This paper presents the design and approval process for operating an Iridium transceiver on orbit and provide on-orbit performance data obtained from a CubeSat platform in Low Earth Orbit (LEO) (500 km orbit). On-orbit data demonstrates that use of a commercial, low-cost Iridium transceiver can serve as a valuable communication approach for low volume telemetry with less than a 30-minute lag for approximately 90% of the time. We also demonstrate that a radial differential velocity of 7 km/sec corresponding to about a 37.5kHz doppler shift and a distance of less than 2,000 km can be used for mission planning. Introduction Setting up a dedicated radio communication link tion is about 5-15 minutes per day per ground station, with a CubeSat in Low Earth Orbit (LEO) presents depending on the altitude and inclination of the satel- several challenges, especially for institutions with lim- lite, as well as the latitude of the ground station. This ited funding or resources. The traditional approach of means the operator is oblivious to the current state of using one or more dedicated radio ground stations to the satellite most of the time, even if multiple ground communicate directly with the satellite is often prohib- stations distributed across the Earth are used.
    [Show full text]
  • 2020 International Space Station U.S. National Laboratory Additive Manufacturing in Space Workshop ______Virtual Event Discussion Summary September 10, 2020
    2020 International Space Station U.S. National Laboratory Additive Manufacturing in Space Workshop __________________________________________________________ Virtual Event Discussion Summary September 10, 2020 The 2020 International Space Station (ISS) U.S. National Laboratory Additive Manufacturing in Space Workshop held on July 28, 2020 was hosted by the Center for the Advancement of Science in Space (CASIS), manager of the ISS National Lab. 2020 Additive Manufacturing in Space Workshop Summary Contents I. EXECUTIVE SUMMARY ........................................................................................................................... 3 II. INTRODUCTION ...................................................................................................................................... 4 Workshop Objectives and Plan .................................................................................................................. 4 III. WORKSHOP DETAILS .............................................................................................................................. 5 Agenda ....................................................................................................................................................... 5 Breakout Sessions ...................................................................................................................................... 5 IV. MAIN SESSION PRESENTATIONS ...........................................................................................................
    [Show full text]
  • Phonesat: Modeling a Spacecraft for Remote Imaging
    MIT Space Exploration Initiative Outreach PhoneSat: Modeling a spacecraft for remote imaging Avery Normandin Published on: Apr 02, 2020 License: Creative Commons Attribution 4.0 International License (CC-BY 4.0) MIT Space Exploration Initiative Outreach PhoneSat: Modeling a spacecraft for remote imaging Activity: creating a small satellite to protect your cell phone in outer-space environments! Background: Small satellites are constantly orbiting Earth, providing useful data about the planet over time. These satellites are designed and built by engineers to withstand the harsh space environment. A “cubesat” is a specific type of small satellite that has very particular specifications, making it easier for people around the world to design and launch. Today, you’ll be turning your phone into a mock-satellite! Mission: It’s your first visit to space as NASA’s newest astronaut - congratulations! Your first mission is to deploy a 1U (10 x 10 x 10 cm) small satellite that takes pictures of the plants and trees in your neighborhood. Your plan is to thrust the satellite into orbit by throwing it outside the International Space Station (ISS). However, during launch, you hear a loud crash - the satellite you have spent the last year designing and building has fallen and broken! Mission control informs you that you are still responsible for getting a satellite into orbit upon your arrival to the ISS. Your new mission is to rebuild the satellite and test a prototype first at home -- one that takes. The only ‘computer’ available to run your satellite? Your smartphone! Using the constraints defined by a cubesat, you will be creating a prototype structure that nests your phone as a “satellite payload”.
    [Show full text]
  • The Space Sector in 2014 and Beyond
    The Space Economy at a Glance 2014 © OECD 2014 Chapter 1 The space sector in 2014 and beyond Chapter 1 reviews major trends in the space sector. It first provides a review of the “space economy” in 2014. It then focuses on an original analysis of global value chains in the space sector, including a spotlight on fifty years of European space co-operation. The chapter also looks at new dynamics in the sector, which may impact incumbents and new entrants, with a focus on innovation in industrial processes and the development of small satellites. 15 1. THE SPACE SECTOR IN 2014 AND BEYOND Defining the “space economy” in 2014 Straddling the defence and aerospace industries, the space sector has for decades been a relatively discrete sector, developed to serve strategic objectives in many OECD and non-OECD economies, with security applications, science and space exploration. The space sector, like many other high-tech sensitive domains, is now attracting much more attention around the world, as governments and private investors seek new sources of economic growth and innovation. The “space economy” has become an intriguing domain to examine, bringing interesting innovation capacities as well as new commercial opportunities. Over the past decade, the number of public and private actors involved in space activities worldwide has increased, spurring even further the development of the nascent space economy. Despite strong headwinds in many related sectors (e.g. defence), the space sector overall has not been significantly affected by the world economic crisis. It remains a strategic sector for many countries, relatively sheltered because of national imperatives (e.g.
    [Show full text]
  • Communications for the Techedsat/Phonesat Missions NASA Ames Research Center
    Communications for the TechEdSat/PhoneSat Missions NASA Ames Research Center Presentation to Small Satellite Pre-Conference Workshop August 5, 2017 Marcus Murbach, PI Rick Alena, Co-I Ali Guarneros-Luna, Co-I Jon Wheless, Engineer SOAREX/TechEdSat/PhoneSat Teams Flight Experiments of Recent Years (2008-2017): 9 Flights SOAREX-6 (2008) SOAREX-7 TES-1 TES-2 (2009) Oct 4, 2012 TES-3 PhoneSat Aug 3, 2013 Iridium-test (6 wk de- Aug 21, 2013 TES-4 orbit) Mar 3, 2015 TES-5 (4 wk de-orbit) Mar 6, 2017 (deorbited Jul 29) TES/PS Team, 2014 SOAREX-8 (2015) SOAREX-9 (2016) TES/PS Team, Summer 2017 What is an Exo-Brake…? Simple, drag-modulated de-orbit system based on tension elements TechEdSat5 was deployed from ISS on March 6, 2017 by NanoRacks The TechEdSat 5 Exo-Brake Experiment • The Exo-Brake is an exo-atmospheric braking and de-orbit device which has successfully flown twice before in a fixed configuration on TechEdSat-3 and 4 • The TechEdSat rapid prototype flight series is conducted as a hands-on training environment for young professionals and university partners • The project helps verify Entry Systems Modeling by gathering real-world data aboard sounding rockets and CubeSats • In the future, passive Exo-Brake systems may be used for small-sat disposal and the development of technologies to permit on-demand sample return from Low Earth Orbit (LEO) scientific/manufacturing platforms TechEdSat 5 (TES5) Avionics, Software and Communications • The 3.5 U CubeSat contains a low-level AVR microprocessor for power control and a high-level Atom processor for fast data processing • The primary Command and Telemetry (C&T) link is provided by the Iridium constellation through on-board Short Burst Data (SBD) modems.
    [Show full text]
  • Space Resources : Social Concerns / Editors, Mary Fae Mckay, David S
    Frontispiece Advanced Lunar Base In this panorama of an advanced lunar base, the main habitation modules in the background to the right are shown being covered by lunar soil for radiation protection. The modules on the far right are reactors in which lunar soil is being processed to provide oxygen. Each reactor is heated by a solar mirror. The vehicle near them is collecting liquid oxygen from the reactor complex and will transport it to the launch pad in the background, where a tanker is just lifting off. The mining pits are shown just behind the foreground figure on the left. The geologists in the foreground are looking for richer ores to mine. Artist: Dennis Davidson NASA SP-509, vol. 4 Space Resources Social Concerns Editors Mary Fae McKay, David S. McKay, and Michael B. Duke Lyndon B. Johnson Space Center Houston, Texas 1992 National Aeronautics and Space Administration Scientific and Technical Information Program Washington, DC 1992 For sale by the U.S. Government Printing Office Superintendent of Documents, Mail Stop: SSOP, Washington, DC 20402-9328 ISBN 0-16-038062-6 Technical papers derived from a NASA-ASEE summer study held at the California Space Institute in 1984. Library of Congress Cataloging-in-Publication Data Space resources : social concerns / editors, Mary Fae McKay, David S. McKay, and Michael B. Duke. xii, 302 p. : ill. ; 28 cm.—(NASA SP ; 509 : vol. 4) 1. Outer space—Exploration—United States. 2. Natural resources. 3. Space industrialization—United States. I. McKay, Mary Fae. II. McKay, David S. III. Duke, Michael B. IV. United States.
    [Show full text]
  • Phonesat the Smartphone Nanosatellite
    PhoneSat The Smartphone Nanosatellite NASA’s PhoneSat project tests whether To do this, the PhoneSat design makes spacecraft can be built using smartphones extensive use of commercial-off-the-shelf to launch the lowest-cost satellites ever components, including a smartphone. flown in space. Each PhoneSat nanosatellite Smartphones offer a wealth of capabilities is one cubesat unit - a satellite in a 10 cm needed for satellite systems such as fast cube (approx. 4 inches) or about the size of processors, versatile operating systems, a tissue box - and weighs approximately 1 multiple miniature sensors, high-resolution kg (2.2 pounds). Engineers believe PhoneSat technology will enable NASA to launch cameras, GPS receivers, and several radios. multiple new satellites capable of conducting PhoneSat engineers also are changing the science and exploration missions at a small way missions are designed by prototyping fraction of the cost of conventional satellites. and incorporating existing commercial The small teams of NASA engineers technologies and hardware to see what supporting PhoneSat at NASA’s Ames capabilities they can provide, rather than Research Center, Moffett Field, Calif., aim trying to custom-design technology to rapidly evolve satellite architecture and solutions to meet set requirements. incorporate the Silicon Valley approach PhoneSat 1.0 demonstrated that low-cost, of “release early, release often,” adding modern electronics can fly in space. It was new functionality to the satellite with each built around the Nexus One smartphone succeeding iteration. made by HTC Corp., running Google’s Left image: The PhoneSat 1.0 cubesat bus with a smartphone inside. Image credit: Ben Howard.
    [Show full text]
  • Defending Planet Earth: Near-Earth Object Surveys and Hazard Mitigation Strategies Final Report
    PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION Defending Planet Earth: Near-Earth Object Surveys and Hazard Mitigation Strategies Final Report Committee to Review Near-Earth Object Surveys and Hazard Mitigation Strategies Space Studies Board Aeronautics and Space Engineering Board Division on Engineering and Physical Sciences THE NATIONAL ACADEMIES PRESS Washington, D.C. www.nap.edu PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION THE NATIONAL ACADEMIES PRESS 500 Fifth Street, N.W. 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 the Contract NNH06CE15B 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 author(s) 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: Space Studies Board National Research Council 500 Fifth Street, N.W. Washington, DC 20001 Additional copies of this report are available from the National Academies Press, 500 Fifth Street, N.W., Lockbox 285, Washington, DC 20055; (800) 624-6242 or (202) 334-3313 (in the Washington metropolitan area); Internet, http://www.nap.edu.
    [Show full text]
  • The Future of Cubesat Communications
    Upcoming CubeSat Launches: The Flood Has Arrived Bryan Klofas KF6ZEO SRI International [email protected] AMSAT-NA Symposium Houston, Texas 1 November 2013 Upcoming CubeSat Launches Name Vehicle Deployers Date # CS # PQ ORS-3/ELaNa-4 Minotaur 1 8 P-POD/8 NLAS 19 Nov 2013 24 (2 CubeStack) ISS ISS/HTV-4 2 J-SSOD 20 Nov 2013 4 Dnepr Dnepr 9 ISIPOD 21 Nov 2013 18 5 UniSat-5 NROL-39/ELaNa-2 Atlas V 8 P-POD 5 Dec 2013 12 (NPSCuL) ISS ISS/Antares 16 NanoRacks 6U Dec 2013 28+ Soyuz Soyuz 1 ISIPOD Feb 2014 1 Dnepr Dnepr 3 P-POD April 2014 3+ ORS-4 Super Strypi 8 NLAS April 2014 10+ (1 CubeStack) Totals: 100+ 5 Slide 2 Statistics of Upcoming Four Launches • 63 CubeSats and PocketQubs (discussed in paper) – Exact frequencies and services listed if known • 9 satellites using 145 MHz amateur satellite band for downlink – 2 under experimental license (DragonSat-1, CAPE-2) – 7 under amateur satellite service (non-US) • 31 satellites using 437 MHz amateur satellite band for downlink – 23 under experimental license (US) – 8 under amateur-satellite service (non-US) • 4 satellites using 2.2 GHz for downlink • 12 satellites using unpublished frequencies • Remaining 8 satellites using 402, 425, 915, 980 MHz Slide 3 Frequency Licensing • FCC released “Guidance on Obtaining Licenses for Small Satellites” DA-13-445 – Clarifies the licensing process and rules related to small satellites – Does not provide guidance on which service to use • Separately, the FCC is pushing non-amateur CubeSats to file for experimental licenses, even if they are using amateur frequencies
    [Show full text]
  • Prototype Design and Mission Analysis for a Small Satellite Exploiting Environmental Disturbances for Attitude Stabilization
    Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis and Dissertation Collection 2016-03 Prototype design and mission analysis for a small satellite exploiting environmental disturbances for attitude stabilization Polat, Halis C. Monterey, California: Naval Postgraduate School http://hdl.handle.net/10945/48578 NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIFORNIA THESIS PROTOTYPE DESIGN AND MISSION ANALYSIS FOR A SMALL SATELLITE EXPLOITING ENVIRONMENTAL DISTURBANCES FOR ATTITUDE STABILIZATION by Halis C. Polat March 2016 Thesis Advisor: Marcello Romano Co-Advisor: Stephen Tackett Approved for public release; distribution is unlimited THIS PAGE INTENTIONALLY LEFT BLANK REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704–0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188) Washington, DC 20503. 1. AGENCY USE ONLY 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED (Leave blank) March 2016 Master’s thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS PROTOTYPE DESIGN AND MISSION ANALYSIS FOR A SMALL SATELLITE EXPLOITING ENVIRONMENTAL DISTURBANCES FOR ATTITUDE STABILIZATION 6. AUTHOR(S) Halis C. Polat 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING Naval Postgraduate School ORGANIZATION REPORT Monterey, CA 93943-5000 NUMBER 9.
    [Show full text]
  • Overview of the In-Space Manufacturing Technology Portfolio
    NASA & ISS National Lab Microgravity Materials Science Overview of the In-Space Workshop Manufacturing Technology Portfolio Atlanta, GA July 29, 2019 Tracie Prater, Ph.D. Diane Risdon Jennifer. Edmunson, Ph.D. Frank Ledbetter, Ph.D. Kevin Wheeler, Ph.D. Vasyl Hafiychuk, Ph.D. Christopher Roberts, Ph.D. Mike Fiske Leigh Elrod Why manufacture in space: The logistics quandary of long endurance spaceflight Each square represents 1000 kg • Based on historical data, 95% of spares will never be used • Impossible to know which spares will be needed Image credit: Bill Cirillo • Unanticipated system issues always appear, even after years of (LaRC) and Andrew Owens (MIT) testing and operations 2 In-space manufacturing removes constraints Constraint1 Constraint removed by ISM? Structures must be designed for launch ISM enables structures which are loads. optimized for operation in space, not for launch loads. Structures must fit within launch vehicle ISM enables structures whose size is payload fairings. limited only by the fabrication volume of the ISM capability. Materials must be disposed of at the end Materials can be recycled and used for of their lifecycle. further manufacturing. All the spare parts and equipment needed Spare parts can be made on-demand. ISM for on-orbit servicing or repair and capabilities can enable on-orbit servicing replacement activities must be and repair of equipment. prepositioned. Component reliability and redundancy Redundancy is augmented by ISM (R&R) largely driven by mission capability to make components on life/duration. demand. R&R requirements may be reduced in some instances when an ISM capability is present. Paradigm shift 1.
    [Show full text]