Addressing Design Challenges in Mechanical Counterpressure Spacesuit Design and Space-Inspired Informal Education Policy by Allison P.Anderson

Total Page:16

File Type:pdf, Size:1020Kb

Addressing Design Challenges in Mechanical Counterpressure Spacesuit Design and Space-Inspired Informal Education Policy by Allison P.Anderson Addressing Design Challenges in Mechanical Counterpressure Spacesuit Design and Space-Inspired Informal Education Policy by Allison P.Anderson B. S. in Astronautics Engineering University of Southern California, 2007 Submitted to the Department of Aeronautics and Astronautics and the Engineering Systems Division in Partial Fulfillment of the Requirements for the Degrees of Master of Science in Aeronautics and Astronautics and ARCHNIVES MASSACHUSETTS INSTITUTE Master of Science in Technology and Policy OF TECHNOLOGY at the FEB 2 5 2011 MASSACHUSETTS INSTITUTE OF TECHNOLOGY LBRARIES February 2011 @2011 Massachusetts Institute of Technology. All Rights Reserved. Author ................................ ........... ........ Department of Aeronautics &Astronautics and Engineering Systems Division January 14, 2011 Ce rtifie d by ............................. ............................... Dava J. Newman, Ph.D. Professor, MacVicar Faculty Fellow, HST Affiliate Department of Aeronautics &Astronautics and Engineering Systems Division Thesis Supervisor Accepted by Dava J. Newman, Ph.D. Professor of Aeronautics and As onautics and Engineering Systems Director, Technology and Policy Program A cce pte d by .................................................................. --- hfvtan H. Modiano, Ph.D. Associate Professor of Aero autics and Astronautics, Chair, Graduate Program Committee 2 Addressing Design Challenges in Mechanical Counterpressure Spacesuit Design and Space-Inspired Informal Education Policy Allison P.Anderson Submitted on January 19, 2011 to the Department of Aeronautics and Astronautics and the Engineering Systems Division in Partial Fulfillment of the Requirements for the Degrees of Master of Science in Aeronautics and Astronautics and Master of Science in Technology and Policy ABSTRACT Extravehicular activity (EVA), or spacewalks allows astronauts to accomplish some of the most important endeavors in space history. The importance of EVA will continue to increase as people venture further into our solar system. The spacesuit, used to protect the astronaut during EVA, is an anthropomorphic spacecraft that provides the physical environment a person needs to survive in the harsh environment of space. Although the suits are safe and effective, the pressurized suit becomes rigid in the vacuum of space, causing the astronaut to waste energy. Mechanical counterpressure (MCP) suits offer an alternative to gas pressurized suits by using elastic garments to provide pressure against the skin. Despite their many advantages, MCP suits are very difficult to put on, or don, making them infeasible for use today. A network of gas pressurized tubes is proposed as a solution to the donning problem. When pressurized, the tubes expand to become rigid, opening the MCP garment in the process. The system was modeled and a functional prototype was developed using a novel construction process. The model can be used as a design tool for future designs and the prototype serves as a proof-of-concept for this solution to the donning problem. The spectacular feats accomplish through spacewalks and space exploration inspire students to pursue an interest and career in science, technology, engineering, and math (STEM). Since its inception, the National Aeronautics and Space Administration (NASA) has been dedicated to educating the public about its compelling mission, fascinating discoveries, and the complicated technologies it develops. However, as the United States slips in indicators of student performance in STEM subjects, many look toward informal education, or education that occurs outside the classroom, to spur interest in STEM subjects. To maximize educational outcomes, NASA has developed a strategic framework to guide its educational programs. This framework is analyzed in the context of strategic management literature and suggests that the framework could be more easily implemented if NASA were to refine its education structure using the strengths of each of its directorates. The proposed framework was implemented in an informal education project and evaluated to determine if a projects implemented under the framework achieves the intended learning objectives. Students showed an increased understanding of NASA's mission and the complicated nature of space exploration. Suggestions to improve future projects are also given. Thesis Supervisor: Dava Newman Title: Professor, MacVicar Faculty Fellow, HST Affiliate, Department of Aeronautics & Astronautics, and Engineering Systems Division The material contained in this paper is based upon work supported by NASA grant Number NNX09AL79G under the Competitive Program for Science Museums and Planetariums. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author and do not necessarily reflect the views of the National Aeronautics and Space Administration. The interview protocols used in this study were approved by the Committee On the Use of Humans as Experimental Subjects under application number 1003003766. TABLE OF CONTENTS List o f Fig u re s ............................................................................................... 8 List o f Ta b le s .............................................................................................. 9 A cknow ledgem ents .................................................................................... 11 1. Intro du ctio n .......................................................................................... 13 1.1. Problem Statement .............................................................. 13 1.2. Research Objectives ............................. 16 1.2 .1. O ve rview ............................................................................. 17 1.2 .2. Specific A im s ........................................................................ 18 1.2.2.1. Specific Aim 1: Modeling..................................... ......... 18 1.2.2.2. Specific Aim 2: Prototyping ................................................... 18 1.2.2.3. Specific Aim 3: Framework Development ............................. 18 1.2.2.4. Specific Aim 4: Evaluation ..................................................... 18 1.3. Research Approach .............................................................. 18 2 . Literature Review ................................................................................. 2 1 2.1. Current State of Spacesuit Design ....................................... 21 2.1.1. Extravehicular Activity .......................................................... 21 2.1.1.1. History of Spacesuit Design ........................ 22 2.1.1.2. Currently Flown Spacesuits ................................................. 26 2.1.1.3. Future of EVA ........................................................................ 30 2.1.2. Need for Pressurized Garments in Space Environment..... 30 2.2. Mechanical Counterpressure ............................................... 33 2.2.1. Space Activity Suit ................................................................ 34 2.2.2. Advances in MCP Glove Technology....................................35 2.2.3. Full Body MCP and Donning Studies of the BioSuit T M Project .39 2.2.3.1. BioSuit T M Concept............................................................... 39 2.2.3.2. Donning/Doffing work ........................................................... 40 2.2.4. Challenges in MCP Design ................................................... 44 2.3. STEM Education in the United States .................................. 44 2.3.1. Informal Education as a Supplement to Formal Education.......46 2.3.2. Role of Federal Agencies in STEM Education ............ 47 2.3.2.1. Federal Agencies - NSF, NOAA, NASA ............................... 47 2.3.2.2. Strategic Management in Agency Programs ........................ 49 2.4. NASA's Education Mission ................................................... 53 2.4 .1. Histo ry ................................................................................ .. 54 2.4.2. Structure and Funding ......................................................... 54 2.4.3. NASA Education Framework ................................................ 56 3. Metho ds ............................................................................................. 61 3.1. MCP Donning/Doffing System Development........................61 3.1.1. Donning Concept ................................................................... 61 3.1.2. Systems Approach ................................................................ 62 3.1.3. Requirements and Assumptions .......................................... 63 3.1.4. Dainese Partnership ............................................................ 65 3.1.5. Glove Development .............................................................. 66 3.1.6. Tube Concept Identification ................................................... 66 3.1.6.1. Elongation Method ............................................................... 66 3.1.6.2. Piston Method ....................................................................... 68 3.1.6.3. Snake Method ...................................................................... 69 3.1.6.4. Fabric Tube Method .............................................................. 70 3.1.6.5. Torus Method ...................................................................... 73 3.1.7. Modeling Methodology .......................................................... 74 3.1.8. Testing and Analysis ............................................................
Recommended publications
  • A Glin-IPSE from the INSIDE of a SPACE SUIT: WHAT IS IT REALLY LIKE to TRAIN for an EVA`'
    IAG09.B6.3.6 A GLIn-IPSE FROM THE INSIDE OF A SPACE SUIT: WHAT IS IT REALLY LIKE TO TRAIN FOR AN EVA`' Matthew A. Gast United Space Alliance, LLC 600 Gemini, Houston TX, 77058-2783; USA matthew.gast-1 @nasa.gov Sandra K Moore, Ph.D. United Space Alliance, LLC 600 Gemini, Houston TX, 77058-2783 ;USA sandra. k.moore@nasa. gov Abstract The beauty of the view from the office of a spacewalking astronaut gives the impression of simplicity, but few beyond the astronauts, and those who train them, know what it really takes to get there. Extravehicular Activity (EVA) training is an intense process that utilizes NASA's Neutral Buoyancy Laboratory (NBL) to develop a very specific skill set needed to safely construct and maintain the orbiting Intemational Space Station. To qualify for flight assignments, astronauts must demonstrate the ability to work safely and efficiently in the physically demandin g environment of the spacesuit, possess an acute ability to resolve tuiforeseen problems, and implement proper tool protocols to ensure no tools will be lost in space. Through the insights and the lessons learned by actual EVA astronauts and EVA instructors, this paper twill take you on a journey through an astronaut's earliest experiences working in the spacesuit. termed the Extravehicular Mobility Unit (ENI[J), in the underwater training environment of the NBL. This work details an actual Suit Qualification NBL training event, outlines the numerous challenges the astronauts face throughout their initial training, and the various ways they adapt their own abilities to overcome them.
    [Show full text]
  • Suited for Spacewalking. Teacher's Guide with Activities for Physical and Life Science
    DOCUMENT RESUME ED 381 392 SE 056 203 AUTHOR Vogt, Gregory L. TITLE Suited for Spacewalking. Teacher's Guide with Activities for Physical and Life Science. Revised. INSTITUTION National Aeronautics and Space Administration, Washington, D.C. Educational Programs Div. REPORT NO EG-101 PUB DATE Aug 94 NOTE 70p. PUB TYPE Guides Classroom Use Teaching Guides (For Teacher) (052) EDRS PRICE MF01/PC03 Plus Postage. DESCRIPTORS Biological Sciences; Earth Science; Elementary Secondary Education; Physical Sciences; *Science Activities; Science Curriculum; Science Education; *Space Exploration; Space Sciences; Student Projects IDENTIFIERS *Hands on Science; Space Shuttle;.*Space Suits; Space Travel ABSTRACT This activity guide for teachers interested in using the intense interest many children have inspace exploration as a launching point for exciting hands-on learning opportunities begins with brief discussions of thespace environment, the history of spacewalking, the Space Shuttle spacesuit, and working inspace. These are followed by a series of activities that enable studentsto explore the space environment as well as the science and technology behind the functions of spacesuits. The activitiesare not rated for specific grade levels because they can be adapted for students of many ages. A chart on curriculum application is designed to help teachers incorporate activities into various subjectareas. Activities and related student projects makeuse of inexpensive and easy-to-find materials and tools. Activitiesare arranged into four basic units including: (1) investigating thespace environment; (2) dressing for spacewalking; (3) moving and working inspace; and (4) exploring the surface of Mars. Contains 17 references and 25 resources. (LZ) *********************************************************************** * Reproductions supplied by EDRS are the best thatcan be made from the original document.
    [Show full text]
  • Suited for Spacewalking
    Education Product National Aeronautics and Space Administration Teachers Grades 5–12 Suited for S pac ewa l k i n g ATeacher’s Guide with Activities for Technology Education, Mathematics, and Science Suited for Spacewalking—A Teacher’s Guide with Activities for Technology Education, Mathematics, and Science is available in electronic format through NASA Spacelink—one of the Agency’s electronic resources specifically developed for use by the educational community. The system may be accessed at the following address: http://spacelink.nasa.gov Suited for Spacewalking A Teacher’s Guide with Activities for Technology Education, Mathematics, and Science National Aeronautics and Space Administration Office of Human Resources and Education Education Division Washington, DC Education Working Group NASA Johnson Space Center Houston, Texas This publication is in the Public Domain and is not protected by copyright. Permission is not required for duplication. EG-1998-03-112-HQ Deborah A. Shearer Acknowledgments Science Teacher Zue S. Baales Intermediate School This publication was developed for the National Friendswood, Texas Aeronautics and Space Administration by: Sandy Peck Writer/Illustrator: Clear Creek Independent School District Gregory L. Vogt, Ed.D. League City, Texas Crew Educational Affairs Liaison Teaching From Space Program Marilyn L. Fowler, Ph.D. NASA Johnson Space Center Science Project Specialist Houston, TX Charles A. Dana Center University of Texas at Austin Editor: Jane A. George Jeanne Gasiorowski Educational Materials Specialist Manager, NASA Educator Resource Center Teaching From Space Program Classroom of the Future NASA Headquarters Wheeling Jesuit University Washington, DC Wheeling, West Virginia Reviewers: Dr. Peggy House Linda Godwin Director, The Glenn T.
    [Show full text]
  • ILC Space Suits & Related Products
    ILC Space Suits & Related Products 0000-712731 Rev. A REVISIONS LETTER DESCRIPTION DATE - Initial Release 10/26/07 A Update with review comments and inclusion of the Antarctic Habitat and 11/28/07 Shuttle Adjustable Protective Mitten Assembly (APMA). This report was written through the volunteer efforts of ILC employees, retirees and friends. Additionally, this report would not have been possible without the efforts of Ken Thomas at Hamilton Sundstrand who truly realizes the significance of preserving the history of US space suit development. The information has been compiled to the best of the participant’s abilities given the volunteer nature of this effort. Any errors are unintentional and will be corrected once identified and verified. If there are any questions regarding any detail of this report, please call (302) 335-3911 Ext. 248. The production of this report does not imply ILC Dover agrees with or is responsible for the contents therein. This report has been compiled from information in the public domain and poses no export licensing issues. William Ayrey Primary Author & Publisher 2 ILC Space Suits & Related Products 0000-712731 Rev. A Table Of Content Chapter 1 The Path Leading To Space -------------------------------------------------------------------------------- 6 The XMC-2-ILC X-15 Competition Prototype (1957) --------------------------------------------------------- 6 The SPD-117 Mercury Competition Prototype (1959) --------------------------------------------------------- 8 Chapter 2 The Journey To The Moon (1960-72) --------------------------------------------------------------- 9 ILC Developments & Prototype Suits Leading To The Apollo Contract (1960-62)----------------------- 10 SPD-143 Training Suits -------------------------------------------------------------------------------------------- 14 Glove Development For Apollo And The World (1962-Present) -------------------------------------------- 17 AX1H - The First New Design Of The Apollo Program ------------------------------------------------------ 19 AX2H Suits (Sept.
    [Show full text]
  • Extravehicular Mobility Unit
    National Aeronautics and Space Administration Extravehicular Mobility Unit The Extravehicular Mobility Unit (EMU) is comprised mainly of the spacesuit assembly and the Portable Life Support System, which provides breathable air for the astronaut and battery power for the suit’s electrical functions. The EMU accommodates a variety of interchangeable systems that interconnect easily and securely in a single-handed operation for either normal or emergency use. Services Provided • System-level engineering insight into the hardware operational performance and detailed leadership into anomaly resolution. • Real-time mission support for on-orbit activities. • Ground training simulations for training and crew extraction from the Neutral Buoyancy Laboratory and vacuum chamber facilities. • Engineering risk-based guidance for management and sustaining of the EMU hardware and forecast for long-term hardware life-cycle usage. • Developmental proof of concept for changes and additions to the EMU hardware system. Johnson Space Center JOHNSON SPACE CENTER EMU Description Spacesuits are unique in that they are anthropomorphic, customized spacecraft. They must provide environmental protection, mobility, and life support to the crewmember during spacewalks. The suit is modular in design, with many interchangeable parts. The upper torso, lower torso, arms, and gloves are manufactured in three different sizes for the major hard-good components (such as the hard upper torso) and can be assembled for each mission in combinations needed to fit male and female astronauts. This design is cost effective because the suits are reusable and not custom fitted as were Extravehicular Activity (EVA) spacesuits used in previous NASA manned space flight programs. When preparing to work in space, the astronaut goes into the airlock of the International Space Station (ISS) and puts on the following parts of the EMU: • A maximum absorbency garment, which is a modified incontinence diaper.
    [Show full text]
  • Defining the Goals for Future Human Space Endeavors Is a Challenge Now Facing All Spacefaring Nations
    - 1 - Chapter 22 LIFE SUPPORT AND PERFORMANCE ISSUES FOR EXTRAVEHICULAR ACTIVITY (EVA) Dava Newman, Ph.D. and Michael Barratt, M.D. 22.1 Introduction Defining the goals for future human space endeavors is a challenge now facing all spacefaring nations. Given the high costs and associated risks of sending humans into Earth orbit or beyond – to lunar or Martian environments, the nature and extent of human participation in space exploration and habitation are key considerations. Adequate protection for humans in orbital space or planetary surface environments must be provided. The Space Shuttle, Mir Space Station, Salyut-Soyuz, and Apollo programs have proven that humans can perform successful extravehicular activity (EVA) in microgravity and on the Lunar surface. Since the beginning of human exploration above and below the surface of the Earth, the main challenge has been to provide the basic necessities for human life support that are normally provided by nature. A person subjected to the near vacuum of space would survive only a few minutes unprotected by a spacesuit. Body fluids would vaporize without a means to supply pressure, and expanded gas would quickly form in the lungs and other tissues, preventing circulation and respiratory movements. EVA is a key and enabling operational resource for long- duration missions which will establish human presence beyond the Earth into the solar system. In this chapter, EVA is used to describe space activities in which a crew member leaves the spacecraft or base and is provided life support by the spacesuit. To meet the challenge of EVA, many factors including atmosphere composition and pressure, thermal control, radiation protection, human performance, and other areas must be addressed.
    [Show full text]
  • How to Walk, Talk, and Breathe on Mars
    Extravehicular Activity Suit Systems Design: How to Walk, Talk, and Breathe on Mars Cornell University 1999 Contributors and advisors: Life Support Systems Communications Systems Power Systems George Barton Alison Diehl George Barton Akio Cox Joel Haenlein Randall Goldsmith Lauren DeFlores Jonathan Mitchell Alex Iglecia Ari Garber Abigail Ross Kerri Kusza Randall Goldsmith Rachel Sanchez Brett Lee Brett Lee Sri Priya Sundararajan Stephen Shannon Saemi Mathews Kiri Wagstaff Mike Valdepenas Faculty Advisor: Steven W. Squyres, Professor of Astronomy Administrative Advisors: Diane Sherman Kathy May Other Contributors: Kevin Reigeluth Robert Shydo, Jr. Abstract Design parameters for a Mars Extravehicular Mobility Unit (EMU) are different from current space shuttle and past Apollo EMU designs. This report derives functional requirements for the life support, communication, and power subsystems of a Mars EMU from the HEDS reference mission and Mars surface conditions and proposes a design that satisfies all of the currently understood functional requirements for each subsystem. Design for the life support system incorporates O2 storage, possible O2 production, CO2 absorption, humidity control, thermal regulation, and radiation protection. The communication system design centers on a reconfigurable wireless network, virtual retinal display, and emergency locator beacons. Portable power options are analyzed, and Direct Methanol Liquid Feed Fuel cells are selected for use in a design that satisfies the power requirements. Mass, cost, and technological readiness are considered for each system. This paper concludes with a recommended combination of subsystem designs that combine to form the primary subsystems of a Mars EMU. 1.0 Introduction Mankind has the ability to safely send humans into Earth orbit and to the Moon.
    [Show full text]
  • Space Suit Evolution from Custom Tailored to Off-The-Rack
    Space Suit Evolution From Custom Tailored To Off-The-Rack Apollo Space Suits Were Custom Tailored The Apollo space suit was basically a one-piece suit. Each suit was made to fit (custom tailored) each astronaut. Each Apollo mission required fifteen (15) suits to support the mission. The main, or prime, three-man crew each had three suits: I for flight; 1 for training; and 1 as a flight back-up in case something happened to their flight suit, thus a total of 9 suits for the prime crew. The back-up three-man crew each had two suits: I for flight and I for training. The astronaut corps at that time included between 25 and 27 astronauts. Shuttle Space Suits Are "Off-The-Rack" The Shuttle astronaut corps includes about 120 men and women. The Shuttle space suit, to accommodate the large number of astronauts with widely varying body sizes, was designed to be made up of many interchangeable parts. These parts (upper and lower torso's, arms, etc.) are fabricated at ILC in different sizes, inspected/tested, then shipped to Johnson Space Center (JSC) where they are inventoried for the astronaut corps. ILC Dover has a staff of about 15 people who work on-site at JSC. This staff is primarily responsible for the control, use, and maintenance of the suit components produced in Frederica after they arrive at JSC. The staff also develops and executes the crew training schedules. This involves everything from taking measurements and conducting fitchecks to de-stow and post-flight inspection/test of the space suit.
    [Show full text]
  • Wardrobe for Space Flight and What They Wear Depends on the Job They Are Doing
    An astronaut working in the space shuffle orbiter cargo bay wears a spacesuit and a jet-powered, hand-controlled maneuvering unit. With this protection and equipment, the astronaut becomes an individual spacecraft able to move about and perform tasks in the microgravity of space. WHY WEAR A SPACESUIT? To explore and work in space, human beings must take their environment with them because there is no atmospheric pressure and no oxygen to sustain life. Inside the spacecraft, the atmosphere can be controlled so that special clothing isn't needed, but when outside, humans need the protection of a spacesuit. Earth's atmosphere is 20 percent oxygen and 80 percent nitrogen from sea level to about 75 miles up, where space begins. At 18,000 feet, the atmosphere is half as dense as it is on the ground, and at altitudes above 40,000 feet, air is so thin and the amount of oxygen so small that pressure oxygen masks no longer do the job. Above the 63,000-foot threshold, humans must wear spacesuits that supply oxygen for breathing and that maintain a pressure around the body to keep body fluids in the liquid state. At this altitude the total air pressure is no longer sufficient to keep body fluids from boiling. Spacesuits for the space shuttle era are pressurized at 4.3 pounds per square inch (psi), but because the gas in the suit is 100 percent oxygen instead of 20 percent, the person in a spacesuit actually has more oxygen to breathe than is available at an altitude of 10,000 feet or even at sea level without the spacesuit.
    [Show full text]
  • The Space Shuttle Extravehicular Mobility Unit (EMU)
    The Space Shuttle Extravehicular Mobility Unit (EMU) As NASA changed from launching astronauts on expendable rockets to the Space Shuttle system with its reusable orbiter and solid rocket boosters, spacesuit engineers began deve l o pment of a reusable EMU. Previously, all spacesuits were one- time garments. Spacesuits were custom-built to each astronaut’s body size. In the Apollo program, for example, e a ch astronaut had three custom suits—one for flight, one for training, and one for flight backup.Shuttle suits, however, are tailored from a stock of standard-size parts to fit astronauts with a wide range of measurements. In cons t r ucting the Shuttle spacesuit, de vel o p - ers were able to conc e n t r ate all their designs towa r d a single function— g oing EVA. Suits from earli e r manned spaceflight prog r ams had to serve mul t i p l e fu n c t i on s . Th e y had to provide backup pres s u r e in case of cabin pre s s u re failure and, on Gemini mi s s i on s , pro t e c t i o n if ejection became necessary du r ing launch .T h ey also had to provide an envi r on- ment for EVA in microg ra v i t y and in low grav i t y while walking on the Moon (Apo l lo missions ) . Sui t s we r e worn during lift off and ree n t r y and had to be com f o r table under the high-g forces experie n c e d du r ing accelerat i o n and decelerat i on .
    [Show full text]
  • Extravehicular Mobility Unit
    National Aeronautics and Space Administration Extravehicular Mobility Unit The Extravehicular Mobility Unit (EMU) is comprised mainly of the spacesuit assembly and the Portable Life Support System, which provides breathable air for the astronaut and battery power for the suit’s electrical functions. The EMU accommodates a variety of interchangeable systems that interconnect easily and securely in a single-handed operation for either normal or emergency use. Services Provided • System-level engineering insight into the hardware operational performance and detailed leadership into anomaly resolution. • Real-time mission support for on-orbit activities. • Ground training simulations for training and crew extraction from the Neutral Buoyancy Laboratory and vacuum chamber facilities. • Engineering risk-based guidance for management and sustaining of the EMU hardware and forecast for long-term hardware life-cycle usage. • Developmental proof of concept for changes and additions to the EMU hardware system. Johnson Space Center JOHNSON SPACE CENTER Testing Spacesuits are unique in that they are anthropomorphic, customized spacecraft. They must provide environmental protection, mobility, and life support to the crewmember during spacewalks. The suit is modular in design, with many interchangeable parts. The upper torso, lower torso, arms, and gloves are manufactured in three different sizes for the major hard-good components (such as the hard upper torso) and can be assembled for each mission in combinations needed to fit male and female astronauts. This design is cost effective because the suits are reusable and not custom fitted as were Extravehicular Activity (EVA) spacesuits used in previous NASA manned space flight programs. When preparing to work in space, the astronaut goes into the airlock of the International Space Station (ISS) and puts on the following parts of the EMU: • A maximum absorbency garment, which is a modified incontinence diaper.
    [Show full text]
  • Astrospud Spacesuit Design Challenge Grade 5 Academic Lesson #6
    Civil Air Patrol’s ACE Program Astrospud Spacesuit Design Challenge Grade 5 Academic Lesson #6 Topics: spacesuits, safety, cost-benefit analysis, compare and contrast (science, math, engineering, language arts) Length of Lesson: 50-70 minutes Lesson Reference: NASA Quest NASA’s Potato Astronaut at Lunar Nautics Objectives: ● Students will use critical thinking skills to design a protective covering for a potato. ● Students will simulate a micrometeoroid or space debris hitting a spacesuit. ● Students will consider the possible effects of micrometeoroids and space debris on spacesuits. ● Students will identify characteristics and purposes of spacesuits. Next Generation Science Standards: ● Obtain and combine information about ways individual communities use science ideas to protect the earth’s resources and environment. (5-ESS3-1) ● Define a simple design problem reflecting a need or a want that includes specified criteria for success and constraints on materials, time, or cost. (3-5-ETS1-1) ● Generate and compare multiple possible solutions to a problem based on how well each is likely to meet the criteria and constraints of the problem. (3-5-ETS1-2) ● Plan and carry out fair tests in which variables are controlled and failure points are considered to identify aspects of a model or prototype that can be improved. (3-5-ETS1-3) CCSS Math: ● 5.NBT.5 - Perform operations with multi-digit whole numbers and with decimals to hundredths. Background Information: (from NASA) Astronauts on spacewalks are likely to encounter fast-moving particles called meteoroids. A meteoroid is usually a fragment of an asteroid consisting of rock and/or metal. It can be very large with a mass of several hundred metric tons, or it can be very small- a micrometeoroid, which is a particle smaller than a grain of sand.
    [Show full text]