THE ECONOMICS of SPACE: an INDUSTRY READY to LAUNCH by Jeff Greason and James C
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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. -
Mitchell Thomas JOS Article
H-SC Journal of Sciences (2017) Vol. VI Thomas Mars: A prospect for settlement Mitchell H. Thomas’17 Department of Biology, Hampden-Sydney College, Hampden-Sydney, VA 23943 The exploration of Mars was once left to the imagination. However, in recent years, the topic of exploring Mars has become more realistic and increasingly popular in news articles and scientific communities. Technology developed in the previous half-century have already allowed humans to send rovers to Mars in order to retrieve some basic data about the planet. Current technological advancements are resulting in reusable rockets that could one day travel between Earth and Mars. Exploration and colonization of Mars are important for the development of research on the planet and the search for life. Current data is limited, but shows that the conditions on Mars could have supported life in the past. To further our knowledge of the red planet, The atmosphere surrounding Earth is nearly organizations like NASA and companies like SpaceX one-hundred times denser than that of Mars and its are developing plans to colonize Mars. Many composition is crucial to life. According to NASA, the obstacles stand in the way before humans can reach Earth’s atmosphere is comprised of 78% Nitrogen, and colonize the red planet. However, Mars is the 21% Oxygen, and 1% Other. On Mars, the sparse best option for interplanetary colonization and the atmosphere is comprised of nearly 96% Carbon most feasible way to research current and future life Dioxide, less than 2% Argon, less than 2% Nitrogen, on a planet other than Earth. -
U.S. Human Space Flight Safety Record As of July 20, 2021
U.S. Human Space Flight Safety Record (As of 20 July 2021) Launch Type Total # of Total # People Total # of Total # of People on Died or Human Space Catastrophic Space Flight Seriously Flights Failures6 Injured3 Orbital (Total) 9271 17 1664 3 Suborbital 2332 3 2135 2 (Total) Total 1160 20 379 5 § 460.45(c) An operator must inform each space flight participant of the safety record of all launch or reentry vehicles that have carried one or more persons on board, including both U.S. government and private sector vehicles. This information must include— (1) The total number of people who have been on a suborbital or orbital space flight and the total number of people who have died or been seriously injured on these flights; and (2) The total number of launches and reentries conducted with people on board and the number of catastrophic failures of those launches and reentries. Federal Aviation Administration AST Commercial Space Transportation Footnotes 1. People on orbital space flights include Mercury (Atlas) (4), Gemini (20), Apollo (36), Skylab (9), Space Shuttle (852), and Crew Dragon (6) a. Occupants are counted even if they flew on only the launch or reentry portion. The Space Shuttle launched 817 humans and picked up 35 humans from MIR and the International Space Station. b. Occupants are counted once reentry is complete. 2. People on suborbital space flights include X-15 (169), M2 (24), Mercury (Redstone) (2), SpaceShipOne (5), SpaceShipTwo (29), and New Shepard System (4) a. Only occupants on the rocket-powered space bound vehicles are counted per safety record criterion #11. -
Space Policy Directive 1 New Shepard Flies Again 5
BUSINESS | POLITICS | PERSPECTIVE DECEMBER 18, 2017 INSIDE ■ Space Policy Directive 1 ■ New Shepard fl ies again ■ 5 bold predictions for 2018 VISIT SPACENEWS.COM FOR THE LATEST IN SPACE NEWS INNOVATION THROUGH INSIGNT CONTENTS 12.18.17 DEPARTMENTS 3 QUICK TAKES 6 NEWS Blue Origin’s New Shepard flies again Trump establishes lunar landing goal 22 COMMENTARY John Casani An argument for space fission reactors 24 ON NATIONAL SECURITY Clouds of uncertainty over miltary space programs 26 COMMENTARY Rep. Brian Babin and Rep. Ami Ber We agree, Mr. President,. America should FEATURE return to the moon 27 COMMENTARY Rebecca Cowen- 9 Hirsch We honor the 10 Paving a clear “Path” to winners of the first interoperable SATCOM annual SpaceNews awards. 32 FOUST FORWARD Third time’s the charm? SpaceNews will not publish an issue Jan. 1. Our next issue will be Jan. 15. Visit SpaceNews.com, follow us on Twitter and sign up for our newsletters at SpaceNews.com/newsletters. ON THE COVER: SPACENEWS ILLUSTRATION THIS PAGE: SPACENEWS ILLUSTRATION FOLLOW US @SpaceNews_Inc Fb.com/SpaceNewslnc youtube.com/user/SpaceNewsInc linkedin.com/company/spacenews SPACENEWS.COM | 1 VOLUME 28 | ISSUE 25 | $4.95 $7.50 NONU.S. CHAIRMAN EDITORIAL CORRESPONDENTS ADVERTISING SUBSCRIBER SERVICES Felix H. Magowan EDITORINCHIEF SILICON VALLEY BUSINESS DEVELOPMENT DIRECTOR TOLL FREE IN U.S. [email protected] Brian Berger Debra Werner Paige McCullough Tel: +1-866-429-2199 Tel: +1-303-443-4360 [email protected] [email protected] [email protected] Fax: +1-845-267-3478 +1-571-356-9624 Tel: +1-571-278-4090 CEO LONDON OUTSIDE U.S. -
Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports
Commercial Space Transportation 2006 Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports January 2006 HQ003606.INDD 2006 U.S. Commercial Space Transportation Developments and Concepts About FAA/AST About the Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA/AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 49 United States Code, Subtitle IX, Chapter 701 (formerly the Commercial Space Launch Act). FAA/AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA/AST is directed to encour- age, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA/AST’s web site at http://ast.faa.gov. Federal Aviation Administration Office of Commercial Space Transportation i About FAA/AST 2006 U.S. Commercial Space Transportation Developments and Concepts NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Federal Aviation Administration Office of Commercial Space Transportation 2006 U.S. Commercial Space Transportation Developments and Concepts Contents Table of Contents Introduction . .1 Significant 2005 Events . .4 Space Competitions . .6 Expendable Launch Vehicles . .9 Current Expendable Launch Vehicle Systems . .9 Atlas 5 - Lockheed Martin Corporation . -
액체로켓 메탄엔진 개발동향 및 시사점 Development Trends of Liquid
Journal of the Korean Society of Propulsion Engineers Vol. 25, No. 2, pp. 119-143, 2021 119 Technical Paper DOI: https://doi.org/10.6108/KSPE.2021.25.2.119 액체로켓 메탄엔진 개발동향 및 시사점 임병직 a, * ㆍ 김철웅 a⋅ 이금오 a ㆍ 이기주 a ㆍ 박재성 a ㆍ 안규복 b ㆍ 남궁혁준 c ㆍ 윤영빈 d Development Trends of Liquid Methane Rocket Engine and Implications Byoungjik Lim a, * ㆍ Cheulwoong Kim a⋅ Keum-Oh Lee a ㆍ Keejoo Lee a ㆍ Jaesung Park a ㆍ Kyubok Ahn b ㆍ Hyuck-Joon Namkoung c ㆍ Youngbin Yoon d a Future Launcher R&D Program Office, Korea Aerospace Research Institute, Korea b School of Mechanical Engineering, Chungbuk National University, Korea c Guided Munitions Team, Hyundai Rotem, Korea d Department of Aerospace Engineering, Seoul National University, Korea * Corresponding author. E-mail: [email protected] ABSTRACT Selecting liquid methane as fuel is a prevailing trend for recent rocket engine developments around the world, triggered by its affordability, reusability, storability for deep space exploration, and prospect for in-situ resource utilization. Given years of time required for acquiring a new rocket engine, a national-level R&D program to develop a methane engine is highly desirable at the earliest opportunity in order to catch up with this worldwide trend towards reusing launch vehicles for competitiveness and mission flexibility. In light of the monumental cost associated with development, fabrication, and testing of a booster stage engine, it is strategically a prudent choice to start with a low-thrust engine and build up space application cases. -
ESPA Ring Datasheet
PAYLOAD ADAPTERS | ESPA ESPA THE EVOLVED SECONDARY PAYLOAD ADAPTER ESPA mounts to the standard NSSL (formerly EELV) interface bolt pattern (Atlas V, Falcon 9, Delta IV, OmegA, Vulcan, Courtesy of Lockheed Martin New Glenn) and is a drop-in component in the launch stack. Small payloads mount to ESPA ports featuring either a Ø15-inch bolt circle with 24 fasteners or a 4-point mount with pads at each corner of a 15-inch square; both of these interfaces have become small satellite standards. ESPA is qualified to carry 567 lbs (257 kg), and a Heavy interface Courtesy of NASA (with Ø5/16” fastener hardware) has been introduced with a capacity of 991 lbs (450 kg). All small satellite mass capabilities require the center of gravity (CG) to be within 20 inches (50.8 cm) of the ESPA port surface. Alternative configurations can be accommodated. ESPA GRANDE ESPA Grande is a more capable version of ESPA with Ø24-inch ports; the ring height is typically 42 inches. The Ø24-inch port has been qualified by test to Courtesy of ORBCOMM & Sierra Nevada Corp. carry small satellites up to 1543 lb (700 kg). ESPA ESPA IS ADAPTABLE TO UNIQUE MISSION REQUIREMENTS • The Air Force’s STP-1 mission delivered multiple small satellites on an Atlas V. • NASA’s Lunar Crater Observation and Sensing Satellite (LCROSS): ESPA was the spacecraft hub for the LCROSS shepherding satellite in 2009. • ORBCOMM Generation 2 (OG2) launched stacks of two and three ESPA Grandes on two different Falcon 9 missions and in total deployed 17 satellites. -
Computational Fluid Dynamic Analysis of Scaled Hypersonic Re-Entry Vehicles
Computational Fluid Dynamic Analysis of Scaled Hypersonic Re-Entry Vehicles A project presented to The Faculty of the Department of Aerospace Engineering San Jose State University In partial fulfillment of the requirements for the degree Master of Science in Aerospace Engineering by Simon H.B. Sorensen March 2019 approved by Dr. Periklis Papadopoulous Faculty Advisor 1 i ABSTRACT With the advancement of technology in space, reusable re-entry space planes have become a focus point with their ability to save materials and utilize existing flight data. Their ability to not only supply materials to space stations or deploy satellites, but also in atmosphere flight makes them versatile in their deployment and recovery. The existing design of vehicles such as the Space Shuttle Orbiter and X-37 Orbital Test Vehicle can be used to observe the effects of scaling existing vehicle geometry and how it would operate in identical conditions to the full-size vehicle. These scaled vehicles, if viable, would provide additional options depending on mission parameters without losing the advantages of reusable re-entry space planes. 2 Table of Contents Abstract . i Nomenclature . .1 1. Introduction. .1 2. Literature Review. 2 2.1 Space Shuttle Orbiter. 2 2.2 X-37 Orbital Test Vehicle. 3 3. Assumptions & Equations. 3 3.1 Assumptions. 3 3.2 Equations to Solve. 4 4. Methodology. 5 5. Base Sized Vehicles. 5 5.1 Space Shuttle Orbiter. 5 5.2 X-37. 9 6. Scaled Vehicles. 11 7. Simulations. 12 7.1 Initial Conditions. 12 7.2 Initial Test Utilizing X-37. .13 7.3 X-37 OTV. -
NASA's Strategic Direction and the Need for a National Consensus
NASA's Strategic Direction and the Need for a National Consensus NASAs Strategic Direction and the Need for a National Consensus Committee on NASAs Strategic Direction Division on Engineering and Physical Sciences THE NATIONAL ACADEMIES PRESS Washington, D.C. www.nap.edu PREPUBLICATION COPYSUBJECT TO FURTHER EDITORIAL CORRECTION Copyright © National Academy of Sciences. All rights reserved. NASA's Strategic Direction and the Need for a National Consensus THE NATIONAL ACADEMIES PRESS 500 Fifth Street, NW 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 Contract NNH10CC48B 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 authors 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: Division on Engineering and Physical Sciences National Research Council 500 Fifth Street, NW Washington, DC 20001 Additional copies of this report are available from the National Academies Press, 500 Fifth Street, NW, Keck 360, Washington, DC 20001; (800) 624-6242 or (202) 334-3313; http://www.nap.edu. -
Trade Studies Towards an Australian Indigenous Space Launch System
TRADE STUDIES TOWARDS AN AUSTRALIAN INDIGENOUS SPACE LAUNCH SYSTEM A thesis submitted for the degree of Master of Engineering by Gordon P. Briggs B.Sc. (Hons), M.Sc. (Astron) School of Engineering and Information Technology, University College, University of New South Wales, Australian Defence Force Academy January 2010 Abstract During the project Apollo moon landings of the mid 1970s the United States of America was the pre-eminent space faring nation followed closely by only the USSR. Since that time many other nations have realised the potential of spaceflight not only for immediate financial gain in areas such as communications and earth observation but also in the strategic areas of scientific discovery, industrial development and national prestige. Australia on the other hand has resolutely refused to participate by instituting its own space program. Successive Australian governments have preferred to obtain any required space hardware or services by purchasing off-the-shelf from foreign suppliers. This policy or attitude is a matter of frustration to those sections of the Australian technical community who believe that the nation should be participating in space technology. In particular the provision of an indigenous launch vehicle that would guarantee the nation independent access to the space frontier. It would therefore appear that any launch vehicle development in Australia will be left to non- government organisations to at least define the requirements for such a vehicle and to initiate development of long-lead items for such a project. It is therefore the aim of this thesis to attempt to define some of the requirements for a nascent Australian indigenous launch vehicle system. -
Small Satellite Launchers
SMALL SATELLITE LAUNCHERS NewSpace Index 2020/04/20 Current status and time from development start to the first successful or planned orbital launch NEWSPACE.IM Northrop Grumman Pegasus 1990 Scorpius Space Launch Demi-Sprite ? Makeyev OKB Shtil 1998 Interorbital Systems NEPTUNE N1 ? SpaceX Falcon 1e 2008 Interstellar Technologies Zero 2021 MT Aerospace MTA, WARR, Daneo ? Rocket Lab Electron 2017 Nammo North Star 2020 CTA VLM 2020 Acrux Montenegro ? Frontier Astronautics ? ? Earth to Sky ? 2021 Zero 2 Infinity Bloostar ? CASIC / ExPace Kuaizhou-1A (Fei Tian 1) 2017 SpaceLS Prometheus-1 ? MISHAAL Aerospace M-OV ? CONAE Tronador II 2020 TLON Space Aventura I ? Rocketcrafters Intrepid-1 2020 ARCA Space Haas 2CA ? Aerojet Rocketdyne SPARK / Super Strypi 2015 Generation Orbit GoLauncher 2 ? PLD Space Miura 5 (Arion 2) 2021 Swiss Space Systems SOAR 2018 Heliaq ALV-2 ? Gilmour Space Eris-S 2021 Roketsan UFS 2023 Independence-X DNLV 2021 Beyond Earth ? ? Bagaveev Corporation Bagaveev ? Open Space Orbital Neutrino I ? LIA Aerospace Procyon 2026 JAXA SS-520-4 2017 Swedish Space Corporation Rainbow 2021 SpinLaunch ? 2022 Pipeline2Space ? ? Perigee Blue Whale 2020 Link Space New Line 1 2021 Lin Industrial Taymyr-1A ? Leaf Space Primo ? Firefly 2020 Exos Aerospace Jaguar ? Cubecab Cab-3A 2022 Celestia Aerospace Space Arrow CM ? bluShift Aerospace Red Dwarf 2022 Black Arrow Black Arrow 2 ? Tranquility Aerospace Devon Two ? Masterra Space MINSAT-2000 2021 LEO Launcher & Logistics ? ? ISRO SSLV (PSLV Light) 2020 Wagner Industries Konshu ? VSAT ? ? VALT