Opening the Moon for Business Derek Webber, FBIS, Spaceport Associates
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Tianwen-1: China's Mars Mission
Tianwen-1: China's Mars Mission drishtiias.com/printpdf/tianwen-1-china-s-mars-mission Why In News China will launch its first Mars Mission - Tianwen-1- in July, 2020. China's previous ‘Yinghuo-1’ Mars mission, which was supported by a Russian spacecraft, had failed after it did not leave the earth's orbit and disintegrated over the Pacific Ocean in 2012. The National Aeronautics and Space Administration (NASA) is also going to launch its own Mars mission in July, the Perseverance which aims to collect Martian samples. Key Points The Tianwen-1 Mission: It will lift off on a Long March 5 rocket, from the Wenchang launch centre. It will carry 13 payloads (seven orbiters and six rovers) that will explore the planet. It is an all-in-one orbiter, lander and rover system. Orbiter: It is a spacecraft designed to orbit a celestial body (astronomical body) without landing on its surface. Lander: It is a strong, lightweight spacecraft structure, consisting of a base and three sides "petals" in the shape of a tetrahedron (pyramid- shaped). It is a protective "shell" that houses the rover and protects it, along with the airbags, from the forces of impact. Rover: It is a planetary surface exploration device designed to move across the solid surface on a planet or other planetary mass celestial bodies. 1/3 Objectives: The mission will be the first to place a ground-penetrating radar on the Martian surface, which will be able to study local geology, as well as rock, ice, and dirt distribution. It will search the martian surface for water, investigate soil characteristics, and study the atmosphere. -
JAXA's Space Exploration Activities
JAXA’s Space Exploration Activities Jun Gomi, Deputy Director General, JAXA Hayabusa 2 ✓ Asteroid Explorer of the C-type asteroid ✓ Launched in December, 2014 ✓ Reached target asteroid “Ryugu” in 2018 ✓ First successful touchdown to Ryugu on February 22, 2019 ✓ Return to Earth in 2020 (162173) Ryugu 2 Hayabusa 2 (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, Nagoya University, Chiba Institute of Technology, Meiji University, Nagoya University, Chiba Institute of Technology, Meiji University, University of Aizu and AIST. University of Aizu, AIST Asteroid Ryugu photographed from a Asteroid Ryugu from an altitude of 6km. distance of about 20 km. The image Image was captured with the Optical was taken on June 30, 2018. Navigation Camera on July 20, 2018. Hayabusa 2 4 JAXA’s Plan for Space Exploration International • Utilization of ISS/Kibo • Cis-Lunar Platform (Gateway) Cooperation • Lunar exploration and beyond Industry & • JAXA Space Exploration Innovation Academia Hub Partnerships • Science Community discussions JAXA’s Overall Scenario for International Space Exploration Mars, others ★ Initial Exploration ★ Full Fledge Exploration MMX: JFY2024 • Science and search for life • Utilization feasibility exam. Kaguya Moon ©JAXA ©JAXA ©JAXA ©JAXA ©JAXA Full-fledged Exploration & SLIM Traversing exploration(2023- ) Sample Return(2026- ) Utilization (JFY2021) • Science exploration • S/R from far side • Cooperative science/resource • Water prospecting • Technology demo for human mission exploration by robotic and human HTV-X der.(2026- ) • Small probe deploy, data relay etc. Gateway Phase 1 Gateway (2022-) Phase 2 • Support for Lunar science Earth • Science using deep space Promote Commercialization International Space Station 6 SLIM (Smart Lander for Investigating Moon) ✓ Demonstrate pin-point landing on the moon. -
Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway
69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 October 2018. Copyright © 2018 by Lockheed Martin Corporation. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-18.A5.1.4x46653 Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway Timothy Cichana*, Stephen A. Baileyb, Adam Burchc, Nickolas W. Kirbyd aSpace Exploration Architect, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] bPresident, 8100 Shaffer Parkway, Unit 130, Deep Space Systems, Inc., Littleton, Colorado, 80127-4124, [email protected] cDesign Engineer / Graphic Artist, 8341 Sangre de Christo Rd, Deep Space Systems, Inc., Littleton, Colorado, 80127, [email protected] dSystems Engineer, Advanced Programs, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] * Corresponding Author Abstract Lockheed Martin is working with NASA on the development of the Lunar Orbiting Platform – Gateway, or Gateway. Positioned in the vicinity of the Moon, the Gateway allows astronauts to demonstrate operations beyond Low Earth Orbit for months at a time. The Gateway is evolvable, flexible, modular, and is a precursor and mission demonstrator directly on the path to Mars. Mars Base Camp is Lockheed Martin's vision for sending humans to Mars. Operations from an orbital base camp will build on a strong foundation of today's technologies and emphasize scientific exploration as mission cornerstones. Key aspects of Mars Base Camp include utilizing liquid oxygen and hydrogen as the basis for a nascent water-based economy and the development of a reusable lander/ascent vehicle. -
Surveyor 1 Space- Craft on June 2, 1966 As Seen by the Narrow Angle Camera of the Lunar Re- Connaissance Orbiter Taken on July 17, 2009 (Also See Fig
i “Project Surveyor, in particular, removed any doubt that it was possible for Americans to land on the Moon and explore its surface.” — Harrison H. Schmitt, Apollo 17 Scientist-Astronaut ii Frontispiece: Landing site of the Surveyor 1 space- craft on June 2, 1966 as seen by the narrow angle camera of the Lunar Re- connaissance Orbiter taken on July 17, 2009 (also see Fig. 13). The white square in the upper photo outlines the area of the enlarged view below. The spacecraft is ca. 3.3 m tall and is casting a 15 m shadow to the East. (NASA/LROC/ ASU/GSFC photos) iii iv Surveyor I: America’s First Moon Landing by William F. Mellberg v © 2014, 2015 William F. Mellberg vi About the author: William Mellberg was a marketing and public relations representative with Fokker Aircraft. He is also an aerospace historian, having published many articles on both the development of airplanes and space vehicles in various magazines. He is the author of Famous Airliners and Moon Missions. He also serves as co-Editor of Harrison H. Schmitt’s website: http://americasuncommonsense.com Acknowledgments: The support and recollections of Frank Mellberg, Harrison Schmitt, Justin Rennilson, Alexander Gurshstein, Paul Spudis, Ronald Wells, Colin Mackellar and Dwight Steven- Boniecki is gratefully acknowledged. vii Surveyor I: America’s First Moon Landing by William F. Mellberg A Journey of 250,000 Miles . December 14, 2013. China’s Chang’e 3 spacecraft successfully touched down on the Moon at 1311 GMT (2111 Beijing Time). The landing site was in Mare Imbrium, the Sea of Rains, about 25 miles (40 km) south of the small crater, Laplace F, and roughly 100 miles (160 km) east of its original target in Sinus Iridum, the Bay of Rainbows. -
Europa Lander
Europa Lander Europa Lander SDT Report & Mission Concept OPAG February 22, 2017, Atlanta, GA Kevin Hand, Alison Murray, Jim Garvin & Europa Lander Team Science Definition Team Co-Chairs: Alison Murray, DRI/Univ. NV Reno, Jim Garvin, GSFC; Kevin Hand, JPL • Ken Edgett, MSSS • Sarah Horst, JHU • Bethany Ehlmann, Caltech • Peter Willis, JPL • Jonathan Lunine, Cornell • Alex Hayes, Cornell • Alyssa Rhoden, ASU • Brent Christner, Univ FL • Will Brinkerhoff, GSFC • Chris German, WHOI • Alexis Templeton, CU Boulder • Aileen Yingst, PSI • Michael Russell, JPL • David Smith, MIT • Tori Hoehler, NASA Ames • Chris Paranicas, APL • Ken Nealson, USC • Britney Schmidt, GA Tech Planetary scientists, Microbiologists, Geochemists Pre-Decisional Information — For Planning and Discussion Purposes Only 2 Europa Lander Mission Concept Key Parameters: • Lander would be launched as a separate mission. • Target launch: 2024-2025 on SLS rocket. • Battery powered mission: 20+ day surface lifetime. • Spacecraft provides 42.5 kg allocation for science payload (with reserves). • Baseline science includes: • Analyses of 5 samples, • Samples acquired from 10 cm depth or deeper (beneath radiation processed regolith) and from 5 different regions within the lander workspace, • Each sample must have a minimum volume of 7 cubic centimeters. Pre-Decisional Information — For Planning and Discussion Purposes Only Europa Lander Mission Concept Pre-Decisional Information — For Planning and Discussion Purposes Only Europa Lander Goals: A Robust Approach to Searching for Signs -
Explore Digital.Pdf
EXPLORE “sic itur ad astra” ~ thus you shall go to the stars EXPERTISE FOR THE MISSION We’ve built more interplanetary spacecraft than all other U.S. companies combined. We’re ready for humanity’s next step, for Earth, the Sun, our planets … and beyond. We do this for the New capability explorers. And for us for a new space era Achieving in space takes tenacity. Lockheed Martin brings more We’ve never missed a tight (and finite) capability to the table than ever planetary mission launch window. before, creating better data, new Yet, despite how far we go, the most images and groundbreaking ways to important technologies we develop work. And we’re doing it with smarter improve life now, closer to home. factories and common products, Here on Earth. making our systems increasingly affordable and faster to produce. HALF A CENTURY AT MARS Getting to space is hard. Each step past that is increasingly harder. We’ve been a part of every NASA mission to Mars, and we know what it takes to arrive on another planet and explore. Our proven work includes aeroshells, autonomous deep space operations or building orbiters and landers, like InSight. AEROSHELLS VIKING 1 VIKING 2 PATHFINDER MARS POLAR SPIRIT OPPORTUNITY PHOENIX CURIOSITY INSIGHT MARS 2020 1976 1976 1996 LANDER 2004 2018 2008 2012 2018 2020 1999 ORBITERS MARS OBSERVER MARS GLOBAL MARS CLIMATE MARS ODYSSEY MARS RECONNAISSANCE MAVEN 1993 SURVEYOR ORBITER 2001 ORBITER 2014 1997 1999 2006 LANDERS VIKING 1 VIKING 2 MARS POLAR PHOENIX INSIGHT 1976 1976 LANDER 2008 2018 1999 Taking humans back to the Moon – We bring solutions for our customers that include looking outside our organization to deliver the best science through our spacecraft and operations expertise. -
Localization of the Chang'e-5 Lander Using Radio-Tracking and Image
remote sensing Technical Note Localization of the Chang’e-5 Lander Using Radio-Tracking and Image-Based Methods Jia Wang 1, Yu Zhang 1, Kaichang Di 2,3 , Ming Chen 1, Jianfeng Duan 1, Jing Kong 1, Jianfeng Xie 1, Zhaoqin Liu 2, Wenhui Wan 2,*, Zhifei Rong 1, Bin Liu 2 , Man Peng 2 and Yexin Wang 2 1 Beijing Aerospace Control Center (BACC), Beijing 100094, China; [email protected] (J.W.); [email protected] (Y.Z.); [email protected] (M.C.); [email protected] (J.D.); [email protected] (J.K.); [email protected] (J.X.); [email protected] (Z.R.) 2 State Key Laboratory of Remote Sensing Science, Aerospace Information Research Institute, Chinese Academy of Sciences, Beijing 100101, China; [email protected] (K.D.); [email protected] (Z.L.); [email protected] (B.L.); [email protected] (M.P.); [email protected] (Y.W.) 3 CAS Center for Excellence in Comparative Planetology, Hefei 230026, China * Correspondence: [email protected]; Tel.: +86-10-64807987 Abstract: Chang’e-5, China’s first unmanned lunar sample-return mission, was successfully landed in Northern Oceanus Procellarum on 1 December 2020. Determining the lander location precisely and timely is critical for both engineering operations and subsequent scientific research. Localization of the lander was performed using radio-tracking and image-based methods. The lander location was determined to be (51.92◦W, 43.06◦N) by both methods. Other localization results were compared for cross-validation. The localization results greatly contributed to the planning of the ascender lifting off from the lander and subsequent maneuvers, and they will contribute to scientific analysis of the returned samples and in situ acquired data. -
Nobackupreview of Human Spaceflight Overview Public 3.Pptx
Review of Human Spaceflight Plans Constellation Overview June 17, 2009 Doug Cooke Jeff Hanley Constellation Architecture Earth Departure Stage Altair Lunar Lander Orion Ares I Crew Exploration Crew Launch Vehicle Vehicle Ares V Cargo Launch Vehicle Constellation is an Integrated Architecture Key Exploration Objectives 1. Replace Space Shuttle capability, with Shuttle retirement in 2010 2. To ensure sustainability, development and operations costs must be minimized 3. Develop systems to serve as building blocks for human exploration of the solar system using the Moon as a test bed 4. Design future human spaceflight systems to be significantly safer than heritage systems 5. Provide crew transport to ISS by 2015, to the lunar surface for extended durations by 2020, and to Mars by TBD 6. Separate crew from cargo delivery to orbit 7. Maintain and grow existing national aerospace supplier base 8. Provide global lunar access to maximize science return 9. Lunar “any time return” is a safety requirement 10. Utilize ISS to support exploration goals 11. Promote international and commercial participation in exploration Solutions Must Be Addressed Through an Integrated Architecture Influence of Key Drivers on Architecture Selection Exploration Crew Transport NASA Developed NASA Develop Human ISS Crew No No Transport? Spaceflight Spacecraft or (Orion) Yes New Needs, Yes International Goals and Objectives VSE, ‘05/’08 NASA Auth. Has Missions No Maximum Beyond LEO commonality and No or Beyond cost Sharing LEO? Yes Continue Orbital Space Yes! Shuttle -
Earth-Moon System
©JSR 2013/2018 Astronomy: Earth-Moon system Earth-Moon System Earth at night To see even the bright Moon properly you need clear skies and I can't resist taking the opportunity of beginning with NASA’s spectacular Earth-at-night picture - or how the Earth would appear without cloud cover. It's a picture that is not only of astronomical interest, but one that says a lot about the world's demography and economy. This section of the course, taking two to three lectures, covers the Earth-Moon system. Moon slide There are many features of the Earth-Moon system that are relevant to the study of the Universe at large. • It is held together by universal gravitation, whose basic law is simple but whose effects are not. • The Moon has craters, like many other objects in our solar system and presumably throughout the Universe. How were they formed and what do they tell us? • Measuring size and distance is a fundamental issue in astronomy. We have to start from homebase. The surer we are of distances in the solar system, the surer we are of measuring the much larger distances between stars and between galaxies. The Moon is the first permanent body beyond the Earth. The Earth-Moon system is the obvious first solar system distance to find. • The Earth-Moon system provides the fascinating spectacle of both lunar and solar eclipses. These have influenced societies, ancient and modern, and provided valuable insights into the nature of the Sun in particular. • There is a tendency to think of heavenly objects as points, because they are so far away. -
China Dream, Space Dream: China's Progress in Space Technologies and Implications for the United States
China Dream, Space Dream 中国梦,航天梦China’s Progress in Space Technologies and Implications for the United States A report prepared for the U.S.-China Economic and Security Review Commission Kevin Pollpeter Eric Anderson Jordan Wilson Fan Yang Acknowledgements: The authors would like to thank Dr. Patrick Besha and Dr. Scott Pace for reviewing a previous draft of this report. They would also like to thank Lynne Bush and Bret Silvis for their master editing skills. Of course, any errors or omissions are the fault of authors. Disclaimer: This research report was prepared at the request of the Commission to support its deliberations. Posting of the report to the Commission's website is intended to promote greater public understanding of the issues addressed by the Commission in its ongoing assessment of U.S.-China economic relations and their implications for U.S. security, as mandated by Public Law 106-398 and Public Law 108-7. However, it does not necessarily imply an endorsement by the Commission or any individual Commissioner of the views or conclusions expressed in this commissioned research report. CONTENTS Acronyms ......................................................................................................................................... i Executive Summary ....................................................................................................................... iii Introduction ................................................................................................................................... 1 -
Spaceports and Landing Pads
Spaceports and Landing Pads A Moon Dialogs Salon Report – Nov 2020 moondialogs.org Spaceports and Landing Pads moondialogs.org Background The issue of lunar dust has been discussed at length across the lunar community. Earlier in 2020, a Moon Dialog was held specifically to investigate all the details of the challenge of dust and damage, and mitigation of these issues. You can see the report and video from this session here: https://www.moondialogs.org/events/research- salon-2-lunar-dust-resource-contention. One of the themes which was repeated frequently during that session and also afterwards was the opportunity of investing in dust-mitigating infrastructure. Many organisations around the world have addressed this in different ways, from sintering to bring-your-own landing pad solution. There is no singular solution thus far which would solve all considerations simultaneously. Thus, we set out to convene a discussion about the plural options for landing infrastructure which mitigate dust and damage, and the resultant social, economic, political and legal implications of different solution sets. Open Lunar Foundation, a co-convenor of Moon Dialogs, had completed relevant work within their research fellowship program (recruit.openlunar.org), with space architect Jeffrey Montes, whose work became the core provocation for this salon. Speakers This salon was grateful to host the following three subject matter experts as provocateurs and discussants: Jeffrey Montes is a Space architect and technologist whose work on habitat designs has been awarded by NASA and exhibited in museums around the world. Jeffrey was the principal designer of Marsha, a novel design and 3D printed prototype for a Mars habitat awarded 1st place in the finale of the NASA 3D Printed Habitat Challenge. -
Guide to Observing the Moon
Your guide to The Moonby Robert Burnham A supplement to 618128 Astronomy magazine 4 days after New Moon south is up to match the view in a the crescent moon telescope, and east lies to the left. f you look into the western sky a few evenings after New Moon, you’ll spot a bright crescent I glowing in the twilight. The Moon is nearly everyone’s first sight with a telescope, and there’s no better time to start watching it than early in the lunar cycle, which begins every month when the Moon passes between the Sun and Earth. Langrenus Each evening thereafter, as the Moon makes its orbit around Earth, the part of it that’s lit by the Sun grows larger. If you look closely at the crescent Mare Fecunditatis zona I Moon, you can see the unlit part of it glows with a r a ghostly, soft radiance. This is “the old Moon in the L/U. p New Moon’s arms,” and the light comes from sun- /L tlas Messier Messier A a light reflecting off the land, clouds, and oceans of unar Earth. Just as we experience moonlight, the Moon l experiences earthlight. (Earthlight is much brighter, however.) At this point in the lunar cycle, the illuminated Consolidated portion of the Moon is fairly small. Nonetheless, “COMET TAILS” EXTENDING from Messier and Messier A resulted from a two lunar “seas” are visible: Mare Crisium and nearly horizontal impact by a meteorite traveling westward. The big crater Mare Fecunditatis. Both are flat expanses of dark Langrenus (82 miles across) is rich in telescopic features to explore at medium lava whose appearance led early telescopic observ- and high magnification: wall terraces, central peaks, and rays.