Cubesat 101: Basic Concepts and Processes for First-Time Cubesat Developers NASA Cubesat Launch Initiative Cubesat 101
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Space Station Intergovernmental Agreement
AGREEMENT AMONG THE GOVERNMENT OF CANADA, GOVERNMENTS OF MEMBER STATES OF THE EUROPEAN SPACE AGENCY, THJ3 GOVERNMENT OF JAPAN, THE GOVERNMENT OF THE RUSSIAN FEDERATION, AND THE GOVERNMENT OF THE UNITED STATES OF AMERICA CONCERNING COOPERATION ON THE CIVIL INTERNATIONAL SPACE STATION , - Table of Contents Arkle 1 Object and Scope Art~le 2 International Rights and Obhgatlons Article 3 Detimtlons Artxle 4 Cooperatmg Agencies Article 5 Reglstratlon, lunsd~cl~on and Control Article 6 Ownershrp of Elements and Equipment Article 7 Management Artxle 8 De&&d Des1811and Development Artde 9 Utthzation Article 10 Operation Article I I crew Article I2 Transportation Article 13 Communlcatrons Article I4 Evolution Article I5 Fundmg Article 16 Cross-Waiver of Liability Article I7 Llabillty Convention Article 18 Customs and Immigmtlon Article 19 Exchange of Data and Goods Article 20 Treatment of Data and Goods in Transit Article 2 1 Intellectual Property tiicle 22 Crimmal Junsdic~on Artxle 23 Consultations Article 24 Space StatIon Cooperation Review Alticle 25 Entry into Force Arlicle 26 Opmti~e Effect as between Certain PartIes Artxle 27 Amendments Article 28 Withdrawal Annex Space Station Elements to be Provided by the Partners I - II I The Government of Canada (heremafter also “Canada”), The Governments of the Kingdom of Belgium, the Kmgdom of Denmark, the French Republic, the Federal Republic of Germany, the Italian Repubhc, the Kmgdom of the Netherlands, the Kingdom of Norway, the Kingdom of Spam, the Kingdom of Sweden, the Swiss Confederation, and -
Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite
46th AIAA Aerospace Sciences Meeting and Exhibit AIAA 2008-1131 7 – 10 January 20006, Reno, Nevada Launch and Deployment Analysis for a Small, MEO, Technology Demonstration Satellite Stephen A. Whitmore* and Tyson K. Smith† Utah State University, Logan, UT, 84322-4130 A trade study investigating the economics, mass budget, and concept of operations for delivery of a small technology-demonstration satellite to a medium-altitude earth orbit is presented. The mission requires payload deployment at a 19,000 km orbit altitude and an inclination of 55o. Because the payload is a technology demonstrator and not part of an operational mission, launch and deployment costs are a paramount consideration. The payload includes classified technologies; consequently a USA licensed launch system is mandated. A preliminary trade analysis is performed where all available options for FAA-licensed US launch systems are considered. The preliminary trade study selects the Orbital Sciences Minotaur V launch vehicle, derived from the decommissioned Peacekeeper missile system, as the most favorable option for payload delivery. To meet mission objectives the Minotaur V configuration is modified, replacing the baseline 5th stage ATK-37FM motor with the significantly smaller ATK Star 27. The proposed design change enables payload delivery to the required orbit without using a 6th stage kick motor. End-to-end mass budgets are calculated, and a concept of operations is presented. Monte-Carlo simulations are used to characterize the expected accuracy of the final orbit. -
The Solar Cruiser Mission: Demonstrating Large Solar Sails for Deep Space Missions
The Solar Cruiser Mission: Demonstrating Large Solar Sails for Deep Space Missions Les Johnson*, Frank M. Curran**, Richard W. Dissly***, and Andrew F. Heaton* * NASA Marshall Space Flight Center ** MZBlue Aerospace NASA Image *** Ball Aerospace Solar Sails Derive Propulsion By Reflecting Photons Solar sails use photon “pressure” or force on thin, lightweight, reflective sheets to produce thrust. NASA Image 2 Solar Sail Missions Flown (as of October 2019) NanoSail-D (2010) IKAROS (2010) LightSail-1 (2015) CanX-7 (2016) InflateSail (2017) NASA JAXA The Planetary Society Canada EU/Univ. of Surrey Earth Orbit Interplanetary Earth Orbit Earth Orbit Earth Orbit Deployment Only Full Flight Deployment Only Deployment Only Deployment Only 3U CubeSat 315 kg Smallsat 3U CubeSat 3U CubeSat 3U CubeSat 10 m2 196 m2 32 m2 <10 m2 10 m2 3 Current and Planned Solar Sail Missions CU Aerospace (2018) LightSail-2 (2019) Near Earth Asteroid Solar Cruiser (2024) Univ. Illinois / NASA The Planetary Society Scout (2020) NASA NASA Earth Orbit Earth Orbit Interplanetary L-1 Full Flight Full Flight Full Flight Full Flight In Orbit; Not yet In Orbit; Successful deployed 6U CubeSat 90 Kg Spacecraft 3U CubeSat 86 m2 >1200 m2 3U CubeSat 32 m2 20 m2 4 Near Earth Asteroid Scout The Near Earth Asteroid Scout Will • Image/characterize a NEA during a slow flyby • Demonstrate a low cost asteroid reconnaissance capability Key Spacecraft & Mission Parameters • 6U cubesat (20cm X 10cm X 30 cm) • ~86 m2 solar sail propulsion system • Manifested for launch on the Space Launch System (Artemis 1 / 2020) • 1 AU maximum distance from Earth Leverages: combined experiences of MSFC and JPL Close Proximity Imaging Local scale morphology, with support from GSFC, JSC, & LaRC terrain properties, landing site survey Target Reconnaissance with medium field imaging Shape, spin, and local environment NEA Scout Full Scale EDU Sail Deployment 6 Solar Cruiser Mission Concept Mission Profile Solar Cruiser may launch as a secondary payload on the NASA IMAP mission in October, 2024. -
Materials Challenges for the Starshot Lightsail
PERSPECTIVE https://doi.org/10.1038/s41563-018-0075-8 Materials challenges for the Starshot lightsail Harry A. Atwater 1*, Artur R. Davoyan1, Ognjen Ilic1, Deep Jariwala1, Michelle C. Sherrott 1, Cora M. Went2, William S. Whitney2 and Joeson Wong 1 The Starshot Breakthrough Initiative established in 2016 sets an audacious goal of sending a spacecraft beyond our Solar System to a neighbouring star within the next half-century. Its vision for an ultralight spacecraft that can be accelerated by laser radiation pressure from an Earth-based source to ~20% of the speed of light demands the use of materials with extreme properties. Here we examine stringent criteria for the lightsail design and discuss fundamental materials challenges. We pre- dict that major research advances in photonic design and materials science will enable us to define the pathways needed to realize laser-driven lightsails. he Starshot Breakthrough Initiative has challenged a broad nanocraft, we reveal a balance between the high reflectivity of the and interdisciplinary community of scientists and engineers sail, required for efficient photon momentum transfer; large band- Tto design an ultralight spacecraft or ‘nanocraft’ that can reach width, accounting for the Doppler shift; and the low mass necessary Proxima Centauri b — an exoplanet within the habitable zone of for the spacecraft to accelerate to near-relativistic speeds. We show Proxima Centauri and 4.2 light years away from Earth — in approxi- that nanophotonic structures may be well-suited to meeting such mately -
Small Space Launch: Origins & Challenges Lt Col Thomas H
Small Space Launch: Origins & Challenges Lt Col Thomas H. Freeman, USAF, [email protected], (505)853-4750 Maj Jose Delarosa, USAF, [email protected], (505)846-4097 Launch Test Squadron, SMC/SDTW Small Space Launch: Origins The United States Space Situational Awareness capability continues to be a key element in obtaining and maintaining the high ground in space. Space Situational Awareness satellites are critical enablers for integrated air, ground and sea operations, and play an essential role in fighting and winning conflicts. The United States leads the world space community in spacecraft payload systems from the component level into spacecraft, and in the development of constellations of spacecraft. The United States’ position is founded upon continued government investment in research and development in space technology [1], which is clearly reflected in the Space Situational Awareness capabilities and the longevity of these missions. In the area of launch systems that support Space Situational Awareness, despite the recent development of small launch vehicles, the United States launch capability is dominated by an old, unresponsive and relatively expensive set of launchers [1] in the Expandable, Expendable Launch Vehicles (EELV) platforms; Delta IV and Atlas V. The EELV systems require an average of six to eight months from positioning on the launch table until liftoff [3]. Access to space requires maintaining a robust space transportation capability, founded on a rigorous industrial and technology base. The downturn of commercial space launch service use has undermined, for the time being, the ability of industry to recoup its significant investment in current launch systems. -
Nasa Langley Research Center 2012
National Aeronautics and Space Administration NASA LANGLEY RESEARCH CENTER 2012 www.nasa.gov An Orion crew capsule test article moments before it is dropped into a An Atlantis flag flew outside Langley’s water basin at Langley to simulate an ocean splashdown. headquarters building during NASA’s final space shuttle mission in July. Launching a New Era of Exploration Welcome to Langley NASA Langley had a banner year in 2012 as we helped propel the nation toward a new age of air and space. From delivering on missions to creating new technologies and knowledge for space, aviation and science, Langley continued the rich tradition of innovation begun 95 years ago. Langley is providing leading-edge research and game-changing technology innovations for human space exploration. We are testing prototype articles of the Orion crew vehicle to optimize designs and improve landing systems for increased crew survivability. Langley has had a role in private-industry space exploration through agreements with SpaceX, Sierra Nevada Corp. and Boeing to provide engineering expertise, conduct testing and support research. Aerospace and Science With the rest of the world, we held our breath as the Curiosity rover landed on Mars – with Langley’s help. The Langley team performed millions of simulations of the entry, descent and landing phase of the Mars Science Laboratory mission to enable a perfect landing, Langley Center Director Lesa Roe and Mark Sirangelo, corporate and for the first time made temperature and pressure vice president and head of Sierra Nevada Space Systems, with measurements as the spacecraft descended, providing the Dream Chaser Space System model. -
Pocketqube Standard Issue 1 7Th of June, 2018
The PocketQube Standard Issue 1 7th of June, 2018 The PocketQube Standard June 7, 2018 Contributors: Organization Name Authors Reviewers TU Delft S. Radu S. Radu TU Delft M.S. Uludag M.S. Uludag TU Delft S. Speretta S. Speretta TU Delft J. Bouwmeester J. Bouwmeester TU Delft - A. Menicucci TU Delft - A. Cervone Alba Orbital A. Dunn A. Dunn Alba Orbital T. Walkinshaw T. Walkinshaw Gauss Srl P.L. Kaled Da Cas P.L. Kaled Da Cas Gauss Srl C. Cappelletti C. Cappelletti Gauss Srl - F. Graziani Important Note(s): The latest version of the PocketQube Standard shall be the official version. 2 The PocketQube Standard June 7, 2018 Contents 1. Introduction ............................................................................................................................................................... 4 1.1 Purpose .............................................................................................................................................................. 4 2. PocketQube Specification ......................................................................................................................................... 4 1.2 General requirements ....................................................................................................................................... 5 2.2 Mechanical Requirements ................................................................................................................................. 5 2.2.1 Exterior dimensions .................................................................................................................................. -
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. -
Ground-Based Demonstration of Cubesat Robotic Assembly
Ground-based Demonstration of CubeSat Robotic Assembly CubeSat Development Workshop 2020 Ezinne Uzo-Okoro, Mary Dahl, Emily Kiley, Christian Haughwout, Kerri Cahoy 1 Motivation: In-Space Small Satellite Assembly Why not build in space? GEO MEO LEO The standardization of electromechanical CubeSat components for compatibility with CubeSat robotic assembly is a key gap 2 Goal: On-Demand On-Orbit Assembled CubeSats LEO Mission Key Phases ➢ Ground Phase: Functional electro/mechanical prototype ➢ ISS Phase: Development and launch of ISS flight unit locker, with CubeSat propulsion option ➢ Free-Flyer Phase: Development of agile free-flyer “locker” satellite with robotic arms to assemble and deploy rapid response CubeSats GEO ➢ Constellation Phase: Development of strategic constellation of agile free-flyer “locker” satellites with robotic Internal View of ‘Locker’ Showing Robotic Assembly arms to autonomously assemble and deploy CubeSats IR Sensors VIS Sensors RF Sensors Propulsion Mission Overview Mission Significance • Orbit-agnostic lockers deploy on-demand robot-assembled CubeSats Provides many CubeSat configurations responsive to • ‘Locker’ is mini-fridge-sized spacecraft with propulsion rapidly evolving space needs capability ✓ Flexible: Selectable sensors and propulsion • Holds robotic arms, sensor, and propulsion modules for ✓ Resilient: Dexterous robot arms for CubeSat assembly 1-3U CubeSats without humans-in-the-loop on Earth and on-orbit Build • Improve response: >30 days to ~hours custom-configured CubeSats on Earth or in space saving -
Year in Review—2013
MSM DEC 2013 cover SATCOM For Net-Centric Warfare December 2013 MilsatMagazine YEARYEAR ININ REVIEW—2013REVIEW—2013 MilsatMagazineDecember 2013 Publishing Operations Senior Contributors Silvano Payne, Publisher + Writer Mike Antonovich, ATEME Hartley G. Lesser, Editorial Director Bert Sadtler, Boxwood Executive Search Pattie Waldt, Executive Editor Richard Dutchik Jill Durfee, Sales Director, Editorial Assistant Tony Bardo, Hughes Simon Payne, Development Director Chris Forrester, Broadgate Publications Donald McGee, Production Manager Karl Fuchs, iDirect Government Services Dan Makinster, Technical Advisor Bob Gough, Carrick Communications Jos Heyman, TIROS Space Information David Leichner, Gilat Satellite Networks This Issue’s Authors Giles Peeters, Track24 Defence Mark A Baird, Colonel, USAF Ian Canning Hartley Lesser Jose Lujano, III, Corporal, USMC Michael Mantz Rafael Martie, Petty Officer, 1st Class, USN Susan Miller Elliot Holokauahi Pulham John Ratigan Scott Scheimreif Pattie Waldt Amy Walker Published 11 times a year by SatNews Publishers 800 Siesta Way Sonoma, CA 95476 USA Phone: (707) 939-9306 Fax: (707) 838-9235 © 2013 SatNews Publishers We reserve the right to edit all submitted materials to meet our content guidelines, as well as for grammar or to move articles to an alternative issue to accommodate publication space requirements, or Cover and Table of masthead Image... removed due to space restrictions. Submission of content does not Staff Sgt. Shelby Johnson, a squad leader with the 4th Brigade constitute acceptance of said material by SatNews Publishers. Edited Combat Team, 10th Mountain Division (Light Infantry), observes the materials may, or may not, be returned to author and/or company area around Forward Operating Base Torkham, Afghanistan, while for review prior to publication. -
FY2009 NRO Congressional Budget Justification Book
NATIONAL RECONNAISSANCE OFFICE 14675 Lee Road Chantilly, VA 20151-1715 6 July 2009 Mr. Steven Aftergood Senior Research Analyst Federation of American Scientists 1725 DeSales St NW, 6th Floor Washington, D.C. 20036 Dear Mr. Aftergood: This is in response to your faxed letter, dated 5 March 2008, received in the Information Management Services Center of the National Reconnaissance Office (NRO) on 7 March 2008. Pursuant to the Freedom of Information Act (FOIA), you requested "a copy of all unclassified portions of the NRO Congressional Budget Justification Book (CBJB) for Fiscal Year 2009.° Your request was processed in accordance with the Freedom of Information Act, 5 U.S.C. § 552, as amended. A thorough search of our files and databases located one record, consisting of 465 pages that is responsive to your request. This record is being released to you in part. Material withheld is denied pursuant to FOIA exemption(b) (3) which applies to information specifically exempt by statute, 50 U.S.C. § 403-1(i) which protects intelligence sources and methods from unauthorized disclosure. AS you are aware, the FOIA authorizes federal agencies to assess fees for record services. Based upon the information provided, you have been placed in the "other" category of requesters, which means that a requester is responsible for charges incurred for the cost of search time exceeding two hours and duplication in excess of the first 100 pages of document reproduction in the processing of this request. In your request, you expressed a willingness to pay fees up to the amount of $50.00. -
NASA TV Schedule for Web (Week of 6-22-2020).Xlsx
NASA TV Daily Program Schedule Monday - 6/22/2020 Eastern Daylight Time 12 a.m. Way Station to Space: The History of Stennis Space Center 12 a.m. 12:30 a.m. Preparing America for Deep Space (Ep.2) 12:30 a.m. 1 a.m. The Final Shuttle Mission 1 a.m. 1:30 a.m. Airborne Tropical Tropopause Experiment (Ep.2) 1:30 a.m. 2 a.m. NASA X - SAGE 3 Monitoring Earths Ozone Layer 2 a.m. 2:30 a.m. Space for Women 2:30 a.m. 3 a.m. NASA EDGE - Robotics 3 a.m. 3:30 a.m. No Small Steps 3:30 a.m. 4 a.m. The Time of Apollo 4 a.m. 4:30 a.m. Space Shuttle Era (Ep.3) 4:30 a.m. 5 a.m. KORUS-AQ: Chapter 3/4 5 a.m. 5:30 a.m. Exploration of the Planets (1971) 5:30 a.m. 6 a.m. NASA X - SAGE 3 Monitoring Earths Ozone Layer 6 a.m. 6:30 a.m. Airborne Tropical Tropopause Experiment (Ep.2) 6:30 a.m. 7 a.m. NASA EDGE - Robotics 7 a.m. 7:30 a.m. ISS Benefits for Humanity (Ep.2) 7:30 a.m. 8 a.m. The Time of Apollo 8 a.m. 8:30 a.m. Space Shuttle Era (Ep.3) 8:30 a.m. 9 a.m. KORUS-AQ: Chapter 3/4 9 a.m. 9:30 a.m. Way Station to Space: The History of Stennis Space Center 9:30 a.m.