NASA Human Spaceflight Scenarios Do All Our Models Still Say ‘No’?
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Supportability for Beyond Low Earth Orbit Missions
Supportability for Beyond Low Earth Orbit Missions William Cirillo1 and Kandyce Goodliff2 NASA Langley Research Center, Hampton, VA, 23681 Gordon Aaseng3 NASA Ames Research Center, Moffett Field, CA, 94035 Chel Stromgren4 Binera, Inc., Silver Springs, MD, 20910 and Andrew Maxwell5 Georgia Institute of Technology, Hampton, VA 23666 Exploration beyond Low Earth Orbit (LEO) presents many unique challenges that will require changes from current Supportability approaches. Currently, the International Space Station (ISS) is supported and maintained through a series of preplanned resupply flights, on which spare parts, including some large, heavy Orbital Replacement Units (ORUs), are delivered to the ISS. The Space Shuttle system provided for a robust capability to return failed components to Earth for detailed examination and potential repair. Additionally, as components fail and spares are not already on-orbit, there is flexibility in the transportation system to deliver those required replacement parts to ISS on a near term basis. A similar concept of operation will not be feasible for beyond LEO exploration. The mass and volume constraints of the transportation system and long envisioned mission durations could make it difficult to manifest necessary spares. The supply of on-demand spare parts for missions beyond LEO will be very limited or even non-existent. In addition, the remote nature of the mission, the design of the spacecraft, and the limitations on crew capabilities will all make it more difficult to maintain the spacecraft. Alternate concepts of operation must be explored in which required spare parts, materials, and tools are made available to make repairs; the locations of the failures are accessible; and the information needed to conduct repairs is available to the crew. -
Mobile Launcher Moves to Vehicle Assembly Building EGS MONTHLY HIGHLIGHTS
National Aeronautics and Space Administration EXPLORATION GROUND SYSTEMS HIGHLIGHTS SEPTEMBER 2018 Mobile Launcher Moves to Vehicle Assembly Building EGS MONTHLY HIGHLIGHTS 3 Mobile launcher on the move 4 In the driver’s seat 5 Prepping for Underway Recovery Test 7 6 Employees, guests view ML move MOBILE LAUNCHER ON THE MOVE NASA’s mobile launcher is inside High Bay 3 at the Vehicle Assembly Building (VAB) on Sept. 11, 2018, at NASA’s Kennedy Space Center in Florida. Photo credit: NASA/Frank Michaux NASA’s mobile launcher, atop crawler-transporter 2, traveled from Launch Pad 39B to the Vehicle Assembly Building at the agency’s Kennedy Space Center in Florida, on Sept. 7, 2018. Arriving late in the afternoon, the mobile launcher stopped at the entrance to the VAB. Early the next day, Sept. 8, engineers and technicians rotated and extended the crew access arm near the top of the mobile launcher tower. Then the mobile launcher was moved inside High Bay 3, where it will spend about seven months undergoing verification and validation testing with the 10 levels of new work platforms, ensuring that it can provide support to the agency’s Space Launch System (SLS). The 380-foot-tall structure is equipped with the crew access Cliff Lanham, NASA project manager for the mobile launcher, takes a break arm and several umbilicals that will provide power, environmental to attend the employee event for the mobile launcher move to the Vehicle control, pneumatics, communication and electrical connections Assembly Building on Sept. 7, 2018, at NASA’s Kennedy Space Center in Florida. -
NASA Space Life and Physical Sciences and Research Applications
NASA Space Life and Physical Sciences and Research Applications SLSPRA has 11 topics listed below and on the following pages for your consideration and possible involvement. (1) Program: Physical Sciences Program (2) Research Title: Dusty Plasmas (3) Research Overview: Dusty plasma research uses dusty plasmas – mixtures of electrons, ions, and charged micron-size particles as a model system to understand astronomical phenomena involving dust-laden plasmas, and as a simplified system modelling the behavior of many-body systems in problems of statistical and condensed matter physics. Dusty plasma research also addresses practical questions of dust management in planetary exploration missions. Proposals are sought for research on dusty plasmas, particularly on the transport of particles in dusty plasmas. 4) NASA Contact a. Name: Bradley Carpenter, Ph.D. b. Organization: NASA Headquarters Space Life and Physical Sciences Research and Applications (SLPSRA) c. Work Phone: (202) 358-0826 d. Email: [email protected] 5) Commercial Entity: a. Company Name: na b. Contact Name: na c. Work Phone: na d. Cell Phone: na e Email: na 6) Partner contribution No NASA Partner contributions 7) Intellectual property management: No NASA Partner intellectual property concerns 8) Additional Information: All publications that result from an awarded EPSCOR study shall acknowledge NASA Space Life and Physical Sciences Research and Applications (SLPSRA). NNH20ZHA001C NASA EPSCoR Rapid Response Research (R3) NASA Space Life and Physical Sciences and Research Applications (continued) 1) Program: Fluids Physics and Combustion Science 2) Research Title: Drop Tower Studies 3) Research Overview: Fundamental discoveries made by NASA researchers over the last 50 years in fluids physics and combustion have helped enable advances in fluids management on spacecraft water recovery and thermal management systems, spacecraft fire safety, and fundamental combustion and fluids physics including low-temperature hydrocarbon oxidation, soot formation and flame stability. -
Race to Space Educator Edition
National Aeronautics and Space Administration Grade Level RACE TO SPACE 10-11 Key Topic Instructional Objectives U.S. space efforts from Students will 1957 - 1969 • analyze primary and secondary source documents to be used as Degree of Difficulty supporting evidence; Moderate • incorporate outside information (information learned in the study of the course) as additional support; and Teacher Prep Time • write a well-developed argument that answers the document-based 2 hours essay question regarding the analogy between the Race to Space and the Cold War. Problem Duration 60 minutes: Degree of Difficulty -15 minute document analysis For the average AP US History student the problem may be at a moderate - 45 minute essay writing difficulty level. -------------------------------- Background AP Course Topics This problem is part of a series of Social Studies problems celebrating the - The United States and contributions of NASA’s Apollo Program. the Early Cold War - The 1950’s On May 25, 1961, President John F. Kennedy spoke before a special joint - The Turbulent 1960’s session of Congress and challenged the country to safely send and return an American to the Moon before the end of the decade. President NCSS Social Studies Kennedy’s vision for the three-year old National Aeronautics and Space Standards Administration (NASA) motivated the United States to develop enormous - Time, Continuity technological capabilities and inspired the nation to reach new heights. and Change Eight years after Kennedy’s speech, NASA’s Apollo program successfully - People, Places and met the president’s challenge. On July 20, 1969, the world witnessed one of Environments the most astounding technological achievements in the 20th century. -
Science in Nasa's Vision for Space Exploration
SCIENCE IN NASA’S VISION FOR SPACE EXPLORATION SCIENCE IN NASA’S VISION FOR SPACE EXPLORATION Committee on the Scientific Context for Space Exploration Space Studies Board Division on Engineering and Physical Sciences THE NATIONAL ACADEMIES PRESS Washington, D.C. www.nap.edu 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. Support for this project was provided by Contract NASW 01001 between the National Academy of Sciences and the National Aeronautics and Space Administration. Any opinions, findings, conclusions, or recommendations expressed in this material are those of the authors and do not necessarily reflect the views of the sponsors. International Standard Book Number 0-309-09593-X (Book) International Standard Book Number 0-309-54880-2 (PDF) Copies of this report are available free of charge from Space Studies Board National Research Council The Keck Center of the National Academies 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. Copyright 2005 by the National Academy of Sciences. -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
Orbital Fueling Architectures Leveraging Commercial Launch Vehicles for More Affordable Human Exploration
ORBITAL FUELING ARCHITECTURES LEVERAGING COMMERCIAL LAUNCH VEHICLES FOR MORE AFFORDABLE HUMAN EXPLORATION by DANIEL J TIFFIN Submitted in partial fulfillment of the requirements for the degree of: Master of Science Department of Mechanical and Aerospace Engineering CASE WESTERN RESERVE UNIVERSITY January, 2020 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis of DANIEL JOSEPH TIFFIN Candidate for the degree of Master of Science*. Committee Chair Paul Barnhart, PhD Committee Member Sunniva Collins, PhD Committee Member Yasuhiro Kamotani, PhD Date of Defense 21 November, 2019 *We also certify that written approval has been obtained for any proprietary material contained therein. 2 Table of Contents List of Tables................................................................................................................... 5 List of Figures ................................................................................................................. 6 List of Abbreviations ....................................................................................................... 8 1. Introduction and Background.................................................................................. 14 1.1 Human Exploration Campaigns ....................................................................... 21 1.1.1. Previous Mars Architectures ..................................................................... 21 1.1.2. Latest Mars Architecture ......................................................................... -
On-Orbit Servicing and Refueling Concepts!
On-orbit Servicing and Refueling Concepts! June 17, 2015 Benjamin B. Reed Deputy Project Manager Satellite Servicing Capabilities Office http://ssco.gsfc.nasa.gov Pre-decisional. Do not forward or post without the consent of [email protected] Introduction! • Over the past five years, NASA has: – Invested in satellite-servicing technologies and tested them on the ground and in orbit – Examined several different “design reference missions” • Non-Shuttle-based Hubble Space Telescope • Propellant depot • 30-m telescope assembly • GOES-12 refueling (GEO) • Landsat 7 refueling (LEO) Growing momentum towards robotic satellite servicing capability. Pre-decisional. Do not forward or post without the consent of [email protected] 2 In Space Robotic Servicing ! • The Satellite Servicing Capabilities Office is responsible for the overall management, coordination, and implementation of satellite servicing technologies and capabilities for NASA. To meet these objectives it: – Conducts studies – Conducts demonstration experiments in orbit and on the ground – Manages technology development and satellite servicing missions – Advises and designs cooperative servicing elements and subsystems Pre-decisional. Do not forward or post without the consent of [email protected] 3 In Space Robotic Servicing Team and Partners! Johnson Space Canadian Space Center Agency Goddard Space Flight Center Department of Defense Space Test Program Glenn Research Center WVU RPI JHU UMD Naval Research Kennedy Laboratory Space Center Pre-decisional. Do not forward or post without the consent of [email protected] 4 Servicing Supports Multiple Objectives! On-orbit Assembly Asteroid Infrastructure Redirection Inspection and Maintenance Fleet Management Government and Commercial Human Exploration Observatory Servicing Servicing Planetary Capabilities! Defense Propellant Depot 5 5 Pre-decisional. -
L-8: Enabling Human Spaceflight Exploration Systems & Technology
Johnson Space Center Engineering Directorate L-8: Enabling Human Spaceflight Exploration Systems & Technology Development Public Release Notice This document has been reviewed for technical accuracy, business/management sensitivity, and export control compliance. It is Montgomery Goforth suitable for public release without restrictions per NF1676 #37965. November 2016 www.nasa.gov 1 NASA’s Journey to Mars Engineering Priorities 1. Enhance ISS: Enhanced missions and systems reliability per ISS customer needs 2. Accelerate Orion: Safe, successful, affordable, and ahead of schedule 3. Enable commercial crew success 4. Human Spaceflight (HSF) exploration systems development • Technology required to enable exploration beyond LEO • System and subsystem development for beyond LEO HSF exploration JSC Engineering’s Internal Goal for Exploration • Priorities are nice, but they are not enough. • We needed a meaningful goal. • We needed a deadline. • Our Goal: Get within 8 years of launching humans to Mars (L-8) by 2025 • Develop and mature the technologies and systems needed • Develop and mature the personnel needed L-8 Characterizing L-8 JSC Engineering: HSF Exploration Systems Development • L-8 Is Not: • A program to go to Mars • Another Technology Road-Mapping effort • L-8 Is: • A way to translate Agency Technology Roadmaps and Architectures/Scenarios into a meaningful path for JSC Engineering to follow. • A way of focusing Engineering’s efforts and L-8 identifying our dependencies • A way to ensure Engineering personnel are ready to step up -
The Esa Exploration Programme – Exomars and Beyond
Lunar and Planetary Science XXXVI (2005) 2408.pdf THE ESA EXPLORATION PROGRAMME – EXOMARS AND BEYOND. G. Kminek1 and the Exploration Team, 1European Space Agency, D/HME, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands, [email protected]. Management and Organization: The countries Technology Development for Exploration: Two participating in the European Exploration Programme categories for exploration technology developments Aurora have recently confirmed and increased their have been identified: contribution. The ESA Council has later approved the Generic Exploration Technology: They have a Agency’s budgets for 2005, including the budget for long-term strategic value, both for robotic and human Aurora. These developments enable major industrial exploration missions. Planetary protection, habitable activities to continue in line with original plans. These systems, risk assessment for human missions to planets, include work on the ExoMars mission and the Mars grey and black water recycling as well as psychological Sample Return mission, in-orbit assembly, rendezvous support for the Concordia Antarctic Station, Facility and docking, habitation and life support systems plus a for Integrated Planetary Exploration Simulations are broad range of technology development work. examples of selected generic exploration technologies. The Aurora Exploration Programme has been inte- Mission Specific Technologies: Specifically devel- grated into the Human Spaceflight and Microgravity oped for the programme’s missions, and will eventually Directorate , which now forms the Human Spaceflight, be implemented after reaching a minimum technology Microgravity, and Exploration Directorate of ESA. readiness level. EVD, sealing and sealing monitoring Early Robotic Missions: Robotic mission have technology, containment technology, specific instru- been identified as necessary prerequisite before send- ment developments, sample handling and distribution ing human to Mars. -
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. -
SHOW DAILY SHOW Aug
Aug. 8, 2019 • Visit us at 239T DAY 3 SHOW DAILY OFFICIAL SHOW DAILY OF THE 33RD AIAA/USU CONFERENCE ON SMALL SATELLITES NASA seeking proposals for cubesats on second SLS launch ASA is soliciting proposals to fly cubesats on the second flight of its Space Launch N System, even as those cubesats chosen for the first SLS launch patiently await their ride. At an agency town hall meeting during the Conference on Small Satellites Aug. 5, Renee Cox, deputy manager for SLS payload integration at NASA’s Marshall Space Flight Center, said the agency was planning to fly cubesats on Artemis 2, the second flight of the SLS, tentatively sched- uled for 2022. “Recently we achieved a level of maturity that has allowed us to identify performance margin, so that means we get to fly cubesats,” she said of the decision to add cubesats to the mission. NASA announced in 2016 it would fly 13 cubesats on the first SLS mission, originally called Explora- tion Mission (EM) 1 and renamed Artemis 1 earlier this year. Those satellites include NASA-funded science and technology demonstration missions, payloads from international partners and compet- itors in the Cube Quest Challenge competition. As with the Artemis 1 mission, the cubesats flying on Artemis 2 will be mounted on the inside of a stage adapter ring between the SLS upper stage and the Orion spacecraft, and will be de- Renee Cox, deputy manager for SLS payload integration, at SmallSat on Wednesday holds a model of an adapter ployed after Orion separates. Unlike Artemis 1, ring that can accomodate six-unit and 12-unit cubesats between the SLS upper stage and Orion spacecraft.