Movement and Maneuver in Deep Space: a Framework to Leverage Advanced Propulsion
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An Evolved International Lunar Decade Global Exploration Roadmap
Lunar Exploration Analysis Group (2015) 2016.pdf An Evolved International Lunar Decade Global Exploration Roadmap. David Dunlop. Author1 and Kim Hold- er. Author2, 1 National Space Society, 410 Ashland Ave, Green Bay Wisconsin, [email protected], 2 National Space Society (Patzcuaro, Michoacan, Mexico, Kim [email protected]). Introduction: Since 2007 an International 1 The 2013 GER edition did not reflect the Chinese Space Exploration Coordination Group (ISECG) of 14 government lunar mission series beginning with the of the largest national space agencies has met to look at 2013 Chang’e III successful landing, and reflecting the potential of collaborative planning and coordina- Chang’e IV (now scheduled for 2020 targeting the tion of their national space exploration activities. lunar farside, Change’e V (sample return now sched- While these meetings have generally been closed door uled for 2017) with a Change’6 Mission indicated as a back-up to the sample return mission. (3) events a 2013 edition Global Exploration Roadmap 2 The GER did not reflect any of the Google Lunar X- (GER) was produced (signed off) by 12 of the 14 coun- Prize Missions. Several teams such as Astrobotic and tries reflecting their projected space program activities Moon-X and Team Space IL have received significant in the categories: Low Earth Orbit, Lunar Vicinity, financial support, have developed flight hardware, and Moon, Mars, Asteroids, and Transportation.(1) This while slipping behind the earlier 2015 deadline are GER is a formidable measure of collaborative efforts planning missions to the Moon perhaps succeeding in and spirits and a reflection of significant global coop- 2016 or when more affordable reusable launchers be- eration. -
To All the Craft We've Known Before
400,000 Visitors to Mars…and Counting Liftoff! A Fly’s-Eye View “Spacers”Are Doing it for Themselves September/October/November 2003 $4.95 to all the craft we’ve known before... 23rd International Space Development Conference ISDC 2004 “Settling the Space Frontier” Presented by the National Space Society May 27-31, 2004 Oklahoma City, Oklahoma Location: Clarion Meridian Hotel & Convention Center 737 S. Meridian, Oklahoma City, OK 73108 (405) 942-8511 Room rate: $65 + tax, 1-4 people Planned Programming Tracks Include: Spaceport Issues Symposium • Space Education Symposium • “Space 101” Advanced Propulsion & Technology • Space Health & Biology • Commercial Space/Financing Space Space & National Defense • Frontier America & the Space Frontier • Solar System Resources Space Advocacy & Chapter Projects • Space Law and Policy Planned Tours include: Cosmosphere Space Museum, Hutchinson, KS (all day Thursday, May 27), with Max Ary Oklahoma Spaceport, courtesy of Oklahoma Space Industry Development Authority Oklahoma City National Memorial (Murrah Building bombing memorial) Omniplex Museum Complex (includes planetarium, space & science museums) Look for updates on line at www.nss.org or www.nsschapters.org starting in the fall of 2003. detach here ISDC 2004 Advance Registration Form Return this form with your payment to: National Space Society-ISDC 2004, 600 Pennsylvania Ave. S.E., Suite 201, Washington DC 20003 Adults: #______ x $______.___ Seniors/Students: #______ x $______.___ Voluntary contribution to help fund 2004 awards $______.___ Adult rates (one banquet included): $90 by 12/31/03; $125 by 5/1/04; $150 at the door. Seniors(65+)/Students (one banquet included): $80 by 12/31/03; $100 by 5/1/04; $125 at the door. -
The Flight to Orbit
There are numerous ways to get there— Around the Corner Th As then–US Space Command chief from rocket The Gen. Howell M. Estes III said to launch to space defense writers just before his re- tirement in August, “This is going maneuver to come along a lot quicker than we vehicles—and the think it is. ... We tend to think this stuff is way out there in the future, Air Force is but it’s right around the corner.” keeping its Flight The Air Force and NASA have divided the task of providing the options open. US government with a means of reliable, low-cost transportation to Earth orbit. The Air Force, with the largest immediate need, is heading to up the effort to revamp the Expend- to able Launch Vehicles now used to loft military and other government satellites. Called the Evolved ELV, this program is focused on derivatives of existing rockets. Competitors have been invited to redesign or value- engineer their proven boosters with new materials and technologies to provide reliable launch services at a he Air Force would like to go Orbit far lower price than today’s bench- back and forth to Earth orbit as bit mark of around $10,000 a pound to T O easily as it goes back and forth to Low Earth Orbit. The reasoning is 30,000 feet—routinely, reliably, and that an “evolved”—rather than an relatively cheaply. Such a capability all-new—vehicle will yield cost sav- goes hand in hand with being a true ings while reducing technical risk. -
In a Comprehensive New Test, the Emdrive Fails to Generate Any Thrust 7 April 2021, by Paul M
In a comprehensive new test, the EmDrive fails to generate any thrust 7 April 2021, by Paul M. Sutter conservation of momentum has been tested countless times over centuries—in fact, that principle forms the bedrock of almost every single theory of physics. So in essence, almost every time physics is tested, so is the conservation of momentum. The results of the Eagleworks experiment were not very strong. While the team claimed to measure a thrust, it wasn't statistically significant, and appeared to be a result of "cherry-picking"—the authors watching random fluctuations and waiting for the right time to report their results. But in the spirit of scientific replication, a team at the Dresden University of Technology led by Prof. Martin Tajmar rebuilt the Eagleworks experimental The EmDrive is a hypothetical rocket that setup. proponents claim can generate thrust with no exhaust. This would violate all known physics. In And they found squat. 2016, a team at NASA's Eagleworks lab claimed to measure thrust from an EmDrive device, the news Reporting their results in the Proceedings of Space of which caused quite a stir. The latest attempt to Propulsion Conference 2020, Prof. Tajmar said, replicate the shocking results has resulted in a "We found out that the cause of the 'thrust' was a simple answer: The Eagleworks measurement was thermal effect. For our tests, we used NASAs from heating of the engine mount, not any new EmDrive configuration from White et al. (which was physics. used at the Eagleworks laboratories, because it is best documented and the results were published in The EmDrive is a relatively simple device: It's an the Journal of Propulsion and Power.) empty cavity that isn't perfectly symmetrical. -
Toward Designing Social Human-Robot Interactions for Deep Space Exploration
Toward Designing Social Human-Robot Interactions for Deep Space Exploration Huili Chen Cynthia Breazeal MIT Media Lab MIT Media Lab [email protected] [email protected] ABSTRACT sleep deprivation, decrease in group cohesion, and decrease in mo- In planning for future human space exploration, it is important to tivation [8]. On the team level, factors related to interpersonal consider how to design for uplifting interpersonal communications communications and group dynamics among astronauts also deci- and social dynamics among crew members. What if embodied social sively impact mission success. For example, astronauts will have to robots could help to improve the overall team interaction experi- live in an ICE condition for the entirety of the mission, necessitating ence in space? On Earth, social robots have been shown effective group living skills to combat potential interpersonal problems [11]. in providing companionship, relieving stress and anxiety, fostering Their diverse cultural backgrounds may additionally impact coping connection among people, enhancing team performance, and medi- in an ICE environment and interplanetary crew’s behavior [49]. ating conflicts in human groups. In this paper, we introduce asetof Unlike shorter-duration space missions, LDSE missions require as- novel research questions exploring social human-robot interactions tronauts to have an unprecedented level of autonomy, leading to in long-duration space exploration missions. greater importance of interpersonal communication among crew members for mission success. The real-time support and interven- KEYWORDS tions from human specialists on Earth (e.g., psychologist, doctor, conflict mediator) are reduced to minimal due to costly communi- Human-robot Interaction, Long-duration Human Space Mission, cation and natural delays in communication between space and Space Robot Companion, Social Connection Earth. -
INTRODUCTION to U.S. Export Controls for the Commercial Space Industry
INTRODUCTION TO U.S. Export Controls for the Commercial Space Industry 2nd Edition – November 2017 Department of Federal Aviation Commerce Administration This publication was prepared by the U.S. Department of Commerce’s Office of Space Commerce and the Federal Aviation Administration’s Office of Commercial Space Transportation. For additional information, questions, or comments, please visit our websites: www.space.commerce.gov ast.faa.gov IMAGE CREDITS Cover: Spaceflight Industries, Inc. Page 2: Blue Origin Page 12: NASA/Orbital ATK Page 32: Mobilus In Mobili Page 50: Planet Page 58: SSL Page 62: Spire Table of Contents PURPOSE ......................................................................1 SECTION 1: BACKGROUND ...................................................2 1.1 Export Control 101 ........................................................4 1.1.1 Definitions: Exports, Deemed Exports, and Re-exports .................4 1.1.2 The Reasons for Controls ................................................4 1.1.3 Regulations and Responsible Departments .............................5 1.1.4 Multilateral Commitments ..............................................7 1.2 What’s Changed Under Export Control Reform .........................8 1.2.1 Satellite Export Control Reform .........................................8 1.2.2 Major Process Changes under Export Control Reform ..................9 SECTION 2: UNDERSTANDING THE CONTROL LISTS AND HOW THEY WORK ......................................................12 2.1 Overview .................................................................14 -
An Assessment of Aerocapture and Applications to Future Missions
Post-Exit Atmospheric Flight Cruise Approach An Assessment of Aerocapture and Applications to Future Missions February 13, 2016 National Aeronautics and Space Administration An Assessment of Aerocapture Jet Propulsion Laboratory California Institute of Technology Pasadena, California and Applications to Future Missions Jet Propulsion Laboratory, California Institute of Technology for Planetary Science Division Science Mission Directorate NASA Work Performed under the Planetary Science Program Support Task ©2016. All rights reserved. D-97058 February 13, 2016 Authors Thomas R. Spilker, Independent Consultant Mark Hofstadter Chester S. Borden, JPL/Caltech Jessie M. Kawata Mark Adler, JPL/Caltech Damon Landau Michelle M. Munk, LaRC Daniel T. Lyons Richard W. Powell, LaRC Kim R. Reh Robert D. Braun, GIT Randii R. Wessen Patricia M. Beauchamp, JPL/Caltech NASA Ames Research Center James A. Cutts, JPL/Caltech Parul Agrawal Paul F. Wercinski, ARC Helen H. Hwang and the A-Team Paul F. Wercinski NASA Langley Research Center F. McNeil Cheatwood A-Team Study Participants Jeffrey A. Herath Jet Propulsion Laboratory, Caltech Michelle M. Munk Mark Adler Richard W. Powell Nitin Arora Johnson Space Center Patricia M. Beauchamp Ronald R. Sostaric Chester S. Borden Independent Consultant James A. Cutts Thomas R. Spilker Gregory L. Davis Georgia Institute of Technology John O. Elliott Prof. Robert D. Braun – External Reviewer Jefferey L. Hall Engineering and Science Directorate JPL D-97058 Foreword Aerocapture has been proposed for several missions over the last couple of decades, and the technologies have matured over time. This study was initiated because the NASA Planetary Science Division (PSD) had not revisited Aerocapture technologies for about a decade and with the upcoming study to send a mission to Uranus/Neptune initiated by the PSD we needed to determine the status of the technologies and assess their readiness for such a mission. -
MULTIPHYSICS DESIGN and SIMULATION of a TUNGSTEN-CERMET NUCLEAR THERMAL ROCKET a Thesis by BRAD APPEL Submitted to the Office O
MULTIPHYSICS DESIGN AND SIMULATION OF A TUNGSTEN-CERMET NUCLEAR THERMAL ROCKET A Thesis by BRAD APPEL Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE August 2012 Major Subject: Nuclear Engineering Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket Copyright 2012 Brad Appel ii MULTIPHYSICS DESIGN AND SIMULATION OF A TUNGSTEN-CERMET NUCLEAR THERMAL ROCKET A Thesis by BRAD APPEL Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Approved by: Chair of Committee, Karen Vierow Committee Members, Shannon Bragg-Sitton Paul Cizmas Head of Department, Yassin Hassan August 2012 Major Subject: Nuclear Engineering iii iii ABSTRACT Multiphysics Design and Simulation of a Tungsten-Cermet Nuclear Thermal Rocket. (August 2012) Brad Appel, B.S., Purdue University Chair of Advisory Committee: Dr. Karen Vierow The goal of this research is to apply modern methods of analysis to the design of a tungsten-cermet Nuclear Thermal Rocket (NTR) core. An NTR is one of the most viable propulsion options for enabling piloted deep-space exploration. Concerns over fuel safety have sparked interest in an NTR core based on tungsten-cermet fuel. This work investigates the capability of modern CFD and neutronics codes to design a cermet NTR, and makes specific recommendations for the configuration of channels in the core. First, the best CFD practices available from the commercial package Star-CCM+ are determined by comparing different modeling options with a hot-hydrogen flow experiment. -
Gravity-Assist Trajectories to Jupiter Using Nuclear Electric Propulsion
AAS 05-398 Gravity-Assist Trajectories to Jupiter Using Nuclear Electric Propulsion ∗ ϒ Daniel W. Parcher ∗∗ and Jon A. Sims ϒϒ This paper examines optimal low-thrust gravity-assist trajectories to Jupiter using nuclear electric propulsion. Three different Venus-Earth Gravity Assist (VEGA) types are presented and compared to other gravity-assist trajectories using combinations of Earth, Venus, and Mars. Families of solutions for a given gravity-assist combination are differentiated by the approximate transfer resonance or number of heliocentric revolutions between flybys and by the flyby types. Trajectories that minimize initial injection energy by using low resonance transfers or additional heliocentric revolutions on the first leg of the trajectory offer the most delivered mass given sufficient flight time. Trajectory families that use only Earth gravity assists offer the most delivered mass at most flight times examined, and are available frequently with little variation in performance. However, at least one of the VEGA trajectory types is among the top performers at all of the flight times considered. INTRODUCTION The use of planetary gravity assists is a proven technique to improve the performance of interplanetary trajectories as exemplified by the Voyager, Galileo, and Cassini missions. Another proven technique for enhancing the performance of space missions is the use of highly efficient electric propulsion systems. Electric propulsion can be used to increase the mass delivered to the destination and/or reduce the trip time over typical chemical propulsion systems.1,2 This technology has been demonstrated on the Deep Space 1 mission 3 − part of NASA’s New Millennium Program to validate technologies which can lower the cost and risk and enhance the performance of future missions. -
Magnetoshell Aerocapture: Advances Toward Concept Feasibility
Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly A thesis submitted in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics & Astronautics University of Washington 2018 Committee: Uri Shumlak, Chair Justin Little Program Authorized to Offer Degree: Aeronautics & Astronautics c Copyright 2018 Charles L. Kelly University of Washington Abstract Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly Chair of the Supervisory Committee: Professor Uri Shumlak Aeronautics & Astronautics Magnetoshell Aerocapture (MAC) is a novel technology that proposes to use drag on a dipole plasma in planetary atmospheres as an orbit insertion technique. It aims to augment the benefits of traditional aerocapture by trapping particles over a much larger area than physical structures can reach. This enables aerocapture at higher altitudes, greatly reducing the heat load and dynamic pressure on spacecraft surfaces. The technology is in its early stages of development, and has yet to demonstrate feasibility in an orbit-representative envi- ronment. The lack of a proof-of-concept stems mainly from the unavailability of large-scale, high-velocity test facilities that can accurately simulate the aerocapture environment. In this thesis, several avenues are identified that can bring MAC closer to a successful demonstration of concept feasibility. A custom orbit code that dynamically couples magnetoshell physics with trajectory prop- agation is developed and benchmarked. The code is used to simulate MAC maneuvers for a 60 ton payload at Mars and a 1 ton payload at Neptune, both proposed NASA mis- sions that are not possible with modern flight-ready technology. In both simulations, MAC successfully completes the maneuver and is shown to produce low dynamic pressures and continuously-variable drag characteristics. -
Global Exploration Roadmap
The Global Exploration Roadmap January 2018 What is New in The Global Exploration Roadmap? This new edition of the Global Exploration robotic space exploration. Refinements in important role in sustainable human space Roadmap reaffirms the interest of 14 space this edition include: exploration. Initially, it supports human and agencies to expand human presence into the robotic lunar exploration in a manner which Solar System, with the surface of Mars as • A summary of the benefits stemming from creates opportunities for multiple sectors to a common driving goal. It reflects a coordi- space exploration. Numerous benefits will advance key goals. nated international effort to prepare for space come from this exciting endeavour. It is • The recognition of the growing private exploration missions beginning with the Inter- important that mission objectives reflect this sector interest in space exploration. national Space Station (ISS) and continuing priority when planning exploration missions. Interest from the private sector is already to the lunar vicinity, the lunar surface, then • The important role of science and knowl- transforming the future of low Earth orbit, on to Mars. The expanded group of agencies edge gain. Open interaction with the creating new opportunities as space agen- demonstrates the growing interest in space international science community helped cies look to expand human presence into exploration and the importance of coopera- identify specific scientific opportunities the Solar System. Growing capability and tion to realise individual and common goals created by the presence of humans and interest from the private sector indicate and objectives. their infrastructure as they explore the Solar a future for collaboration not only among System. -
IAF Space Propulsion Symposium 2019
IAF Space Propulsion Symposium 2019 Held at the 70th International Astronautical Congress (IAC 2019) Washington, DC, USA 21 -25 October 2019 Volume 1 of 2 ISBN: 978-1-7138-1491-7 Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 Some format issues inherent in the e-media version may also appear in this print version. Copyright© (2019) by International Astronautical Federation All rights reserved. Printed with permission by Curran Associates, Inc. (2020) For permission requests, please contact International Astronautical Federation at the address below. International Astronautical Federation 100 Avenue de Suffren 75015 Paris France Phone: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 www.iafastro.org Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 USA Phone: 845-758-0400 Fax: 845-758-2633 Email: [email protected] Web: www.proceedings.com TABLE OF CONTENTS VOLUME 1 PROPULSION SYSTEM (1) BLUE WHALE 1: A NEW DESIGN APPROACH FOR TURBOPUMPS AND FEED SYSTEM ELEMENTS ON SOUTH KOREAN MICRO LAUNCHERS ............................................................................ 1 Dongyoon Shin KEYNOTE: PROMETHEUS: PRECURSOR OF LOW-COST ROCKET ENGINE ......................................... 2 Jérôme Breteau ASSESSMENT OF MON-25/MMH PROPELLANT SYSTEM FOR DEEP-SPACE ENGINES ...................... 3 Huu Trinh 60 YEARS DLR LAMPOLDSHAUSEN – THE EUROPEAN RESEARCH AND TEST SITE FOR CHEMICAL SPACE PROPULSION SYSTEMS ....................................................................................... 9 Anja Frank, Marius Wilhelm, Stefan Schlechtriem FIRING TESTS OF LE-9 DEVELOPMENT ENGINE FOR H3 LAUNCH VEHICLE ................................... 24 Takenori Maeda, Takashi Tamura, Tadaoki Onga, Teiu Kobayashi, Koichi Okita DEVELOPMENT STATUS OF BOOSTER STAGE LIQUID ROCKET ENGINE OF KSLV-II PROGRAM .......................................................................................................................................................