STP Background • STP Enablers • Rideshare Opportunities • Summary
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Space) Barriers for 50 Years: the Past, Present, and Future of the Dod Space Test Program
SSC17-X-02 Breaking (Space) Barriers for 50 Years: The Past, Present, and Future of the DoD Space Test Program Barbara Manganis Braun, Sam Myers Sims, James McLeroy The Aerospace Corporation 2155 Louisiana Blvd NE, Suite 5000, Albuquerque, NM 87110-5425; 505-846-8413 [email protected] Colonel Ben Brining USAF SMC/ADS 3548 Aberdeen Ave SE, Kirtland AFB NM 87117-5776; 505-846-8812 [email protected] ABSTRACT 2017 marks the 50th anniversary of the Department of Defense Space Test Program’s (STP) first launch. STP’s predecessor, the Space Experiments Support Program (SESP), launched its first mission in June of 1967; it used a Thor Burner II to launch an Army and a Navy satellite carrying geodesy and aurora experiments. The SESP was renamed to the Space Test Program in July 1971, and has flown over 568 experiments on over 251 missions to date. Today the STP is managed under the Air Force’s Space and Missile Systems Center (SMC) Advanced Systems and Development Directorate (SMC/AD), and continues to provide access to space for DoD-sponsored research and development missions. It relies heavily on small satellites, small launch vehicles, and innovative approaches to space access to perform its mission. INTRODUCTION Today STP continues to provide access to space for DoD-sponsored research and development missions, Since space first became a viable theater of operations relying heavily on small satellites, small launch for the Department of Defense (DoD), space technologies have developed at a rapid rate. Yet while vehicles, and innovative approaches to space access. -
Thesis Submitted to Florida Institute of Technology in Partial Fulfllment of the Requirements for the Degree Of
Dynamics of Spacecraft Orbital Refueling by Casey Clark Bachelor of Aerospace Engineering Mechanical & Aerospace Engineering College of Engineering 2016 A thesis submitted to Florida Institute of Technology in partial fulfllment of the requirements for the degree of Master of Science in Aerospace Engineering Melbourne, Florida July, 2018 ⃝c Copyright 2018 Casey Clark All Rights Reserved The author grants permission to make single copies. We the undersigned committee hereby approve the attached thesis Dynamics of Spacecraft Orbital Refueling by Casey Clark Dr. Tiauw Go, Sc.D. Associate Professor. Mechanical & Aerospace Engineering Committee Chair Dr. Jay Kovats, Ph.D. Associate Professor Mathematics Outside Committee Member Dr. Markus Wilde, Ph.D. Assistant Professor Mechanical & Aerospace Engineering Committee Member Dr. Hamid Hefazi, Ph.D. Professor and Department Head Mechanical & Aerospace Engineering ABSTRACT Title: Dynamics of Spacecraft Orbital Refueling Author: Casey Clark Major Advisor: Dr. Tiauw Go, Sc.D. A quantitative collation of relevant parameters for successfully completed exper- imental on-orbit fuid transfers and anticipated orbital refueling future missions is performed. The dynamics of connected satellites sustaining fuel transfer are derived by treating the connected spacecraft as a rigid body and including an in- ternal mass fow rate. An orbital refueling results in a time-varying local center of mass related to the connected spacecraft. This is accounted for by incorporating a constant mass fow rate in the inertia tensor. Simulations of the equations of motion are performed using the values of the parameters of authentic missions in an endeavor to provide conclusions regarding the efect of an internal mass transfer on the attitude of refueling spacecraft. -
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 ......................................................................... -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 2 May–June 2019 CONTENTS FOCUS ..................................................................................................................... 1 European industrial leadership at stake ............................................................................ 1 SPACE POLICY AND PROGRAMMES .................................................................................... 2 EUROPE ................................................................................................................. 2 9th EU-ESA Space Council .......................................................................................... 2 Europe’s Martian ambitions take shape ......................................................................... 2 ESA’s advancements on Planetary Defence Systems ........................................................... 2 ESA prepares for rescuing Humans on Moon .................................................................... 3 ESA’s private partnerships ......................................................................................... 3 ESA’s international cooperation with Japan .................................................................... 3 New EU Parliament, new EU European Space Policy? ......................................................... 3 France reflects on its competitiveness and defence posture in space ...................................... 3 Germany joins consortium to support a European reusable rocket......................................... -
Next Generation Advanced Video Guidance Sensor: Low Risk Rendezvous and Docking Sensor
Next Generation Advanced Video Guidance Sensor: Low Risk Rendezvous and Docking Sensor Jimmy Lee1 and Connie Carrington2 NASA Marshall Space Flight Center, Huntsville, AL, 35812 Susan Spencer3 NASA Marshall Space Flight Center, Huntsville, AL, 35812 and Thomas Bryan, Ricky T. Howard, Jimmie Johnson4 NASA Marshall Space Flight Center, Huntsville, AL, 35812 The Next Generation Advanced Video Guidance Sensor (NGAVGS) is being built and tested at MSFC. This paper provides an overview of current work on the NGAVGS, a summary of the video guidance heritage, and the AVGS performance on the Orbital Express mission. This paper also provides a discussion of applications to ISS cargo delivery vehicles, CEV, and future lunar applications. I. Introduction ELATIVE navigation sensors are an enabling technology for exploration vehicles such as the National R Aeronautics and Space Administration’s (NASA’s) Crew Exploration Vehicle (CEV), cargo vehicles for logistics delivery to the International Space Station (ISS), and lunar landers. Additional applications are lunar sample return missions, satellite servicing, and future on-orbit assembly of space structures. The Next Generation Advanced Video Guidance Sensor (NGAVGS) is a third generation relative navigation sensor that incorporates the basic functions developed and flight proven in the Advanced Video Guidance Sensor (AVGS). The AVGS was the primary proximity operations and docking sensor in the first autonomous docking in the history of the U.S. space program, which was accomplished on May 5, 2007 during the Orbital Express (OE) mission. However, the AVGS hardware cannot be reproduced due to parts obsolescence, which has provided Marshall Space Flight Center (MSFC) an opportunity to replace an obsolete imager and processor with radiation tolerant parts, and to address critical CEV and ISS cargo vehicle relative navigation sensor requirements. -
External Payloads Proposer's Guide to the International Space Station
SSP 51071 Baseline External Payloads Proposer’s Guide to the International Space Station International Space Station Program Baseline August 2017 National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas This Document Is Uncontrolled When Printed. Verify Current version before use. SSP 51071 Baseline REVISION AND HISTORY REV. DESCRIPTION PUB. DATE - Initial Release (Reference per SSCD 15774, EFF. 09-29-2017) 10-02-17 Public access authorization obtained via the Document Availability Authorization Control Number: “40352” This Document Is Uncontrolled When Printed. Verify Current Version Before Use. SSP 51071 Baseline TABLE OF CONTENTS PARAGRAPH PAGE 1.0 INTRODUCTION ................................................................................................................... 1-1 2.0 GENERAL INFORMATION FOR OPERATING ON ISS ........................................................ 2-1 2.1 HOW TO GET STARTED ...................................................................................................... 2-1 2.2 ISS FEASIBILITY RESOURCE ACCOMMODATION ASSESSMENT PROCESS ................ 2-2 2.3 WHAT YOU SHOULD KNOW ............................................................................................... 2-5 2.4 ORGANIZATIONAL ROLES/RESPONSIBILITIES ................................................................ 2-7 2.5 ROLES/RESPONSIBILITIES OF PAYLOAD PROVIDERS ................................................... 2-8 3.0 COMMON ACCOMMODATIONS, RESOURCES, AND ENVIRONMENTS -
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 -
Space Activities 2019
Space Activities in 2019 Jonathan McDowell [email protected] 2020 Jan 12 Rev 1.3 Contents Preface 3 1 Orbital Launch Attempts 3 1.1 Launch statistics by country . 3 1.2 Launch failures . 4 1.3 Commercial Launches . 4 2 Satellite Launch Statistics 6 2.1 Satellites of the major space powers, past 8 years . 6 2.2 Satellite ownership by country . 7 2.3 Satellite manufacture by country . 11 3 Scientific Space Programs 11 4 Military Space Activities 12 4.1 Military R&D . 12 4.2 Space surveillance . 12 4.3 Reconnaissance and Signals Intelligence . 13 4.4 Space Weapons . 13 5 Special Topics 13 5.1 The Indian antisatellite test and its implications . 13 5.2 Starlink . 19 5.3 Lightsail-2 . 24 5.4 Kosmos-2535/2536 . 25 5.5 Kosmos-2542/2543 . 29 5.6 Starliner . 29 5.7 OTV-5 and its illegal secret deployments . 32 5.8 TJS-3 . 33 6 Orbital Debris and Orbital Decay 35 6.1 Disposal of launch vehicle upper stages . 36 6.2 Orbituaries . 39 6.3 Retirements in the GEO belt . 42 6.4 Debris events . 43 7 Acknowledgements 43 Appendix 1: 2019 Orbital Launch Attempts 44 1 Appendix 2a: Satellite payloads launched in 2018 (Status end 2019) 46 Appendix 2b: Satellite payloads deployed in 2018 (Revised; Status end 2019) 55 Appendix 2c: Satellite payloads launched in 2019 63 Appendix 2d: Satellite payloads deployed in 2019 72 Rev 1.0 - Jan 02 Initial version Rev 1.1 - Jan 02 Fixed two incorrect values in tables 4a/4b Rev 1.2 - Jan 02 Minor typos fixed Rev 1.3 - Jan 12 Corrected RL10 variant, added K2491 debris event, more typos 2 Preface In this paper I present some statistics characterizing astronautical activity in calendar year 2019. -
A Summary of the Rendezvous, Proximity Operations, Docking, And
NASA/TM-2011-217088 NESC-RP-10-00628 A Summary of the Rendezvous, Proximity Operations, Docking, and Undocking (RPODU) Lessons Learned from the Defense Advanced Research Project Agency (DARPA) Orbital Express (OE) Demonstration System Mission Cornelius J. Dennehy/NESC Langley Research Center, Hampton, Virginia J. Russell Carpenter Goddard Space Flight Center, Greenbelt, Maryland April 2011 NASA STI Program . in Profile Since its founding, NASA has been dedicated to • CONFERENCE PUBLICATION. Collected the advancement of aeronautics and space science. papers from scientific and technical The NASA scientific and technical information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or co-sponsored by NASA. this important role. • SPECIAL PUBLICATION. Scientific, The NASA STI program operates under the technical, or historical information from NASA auspices of the Agency Chief Information Officer. It programs, projects, and missions, often collects, organizes, provides for archiving, and concerned with subjects having substantial disseminates NASA’s STI. The NASA STI program public interest. provides access to the NASA Aeronautics and Space Database and its public interface, the NASA Technical • TECHNICAL TRANSLATION. English- Report Server, thus providing one of the largest language translations of foreign scientific and collections of aeronautical and space science STI in technical material pertinent to NASA’s mission. the world. Results are published in both non-NASA channels and by NASA in the NASA STI Report Specialized services also include creating custom Series, which includes the following report types: thesauri, building customized databases, and organizing and publishing research results. • TECHNICAL PUBLICATION. Reports of completed research or a major significant phase For more information about the NASA STI of research that present the results of NASA program, see the following: programs and include extensive data or theoretical analysis. -
Guidelines and Metrics for Assessing Space System Cost Estimates
THE ARTS This PDF document was made available from www.rand.org as a public CHILD POLICY service of the RAND Corporation. CIVIL JUSTICE EDUCATION ENERGY AND ENVIRONMENT Jump down to document6 HEALTH AND HEALTH CARE INTERNATIONAL AFFAIRS NATIONAL SECURITY The RAND Corporation is a nonprofit research POPULATION AND AGING organization providing objective analysis and effective PUBLIC SAFETY solutions that address the challenges facing the public SCIENCE AND TECHNOLOGY and private sectors around the world. SUBSTANCE ABUSE TERRORISM AND HOMELAND SECURITY TRANSPORTATION AND INFRASTRUCTURE WORKFORCE AND WORKPLACE Support RAND Purchase this document Browse Books & Publications Make a charitable contribution For More Information Visit RAND at www.rand.org Explore RAND Project AIR FORCE View document details Limited Electronic Distribution Rights This document and trademark(s) contained herein are protected by law as indicated in a notice appearing later in this work. This electronic representation of RAND intellectual property is provided for non-commercial use only. Unauthorized posting of RAND PDFs to a non-RAND Web site is prohibited. RAND PDFs are protected under copyright law. Permission is required from RAND to reproduce, or reuse in another form, any of our research documents for commercial use. For information on reprint and linking permissions, please see RAND Permissions. This product is part of the RAND Corporation technical report series. Reports may include research findings on a specific topic that is limited in scope; present discus- sions of the methodology employed in research; provide literature reviews, survey instruments, modeling exercises, guidelines for practitioners and research profes- sionals, and supporting documentation; or deliver preliminary findings. -
Getting in Your Space: Learning from Past Rendezvous and Proximity Operations
CENTER FOR SPACE POLICY AND STRATEGY MAY 2018 GETTING IN YOUR SPACE: LEARNING FROM PAST RENDEZVOUS AND PROXIMITY OPERATIONS REBECCA REESMAN, ANDREW ROGers THE AEROSPACE CORPORATION © 2018 The Aerospace Corporation. All trademarks, service marks, and trade names contained herein are the property of their respective owners. Approved for public release; distribution unlimited. OTR201800593 REBECCA REESMAN Dr. Rebecca Reesman is a member of the technical staff in The Aerospace Corporation’s Performance Modeling and Analysis Department, where she supports government customers in the national security community. Before joining Aerospace in 2017, she was an American Institute of Physics Congressional Fellow handling space, cybersecurity, and other technical issues for a member of Congress. Prior to the fellowship, she was a research scientist at the Center for Naval Analysis, providing technical and analytical support to the Department of Defense, with particular focus on developing and executing wargames. Reesman received her Ph.D. in physics from the Ohio State University and a bachelor’s degree from Carnegie Mellon University. ANDREW ROGERS Dr. Andrew Rogers is a member of the technical staff in The Aerospace Corporation’s Mission Analysis and Operations Department. His expertise is in relative motion astrodynamics, control theory, and space mission design. Rogers supports government customers in the areas of concept- of-operations development, orbital analysis, and small satellite technology development. Prior to joining Aerospace in 2016, Rogers received his Ph.D. in aerospace engineering and a bachelor of science in mechanical engineering from Virginia Polytechnic Institute and State University. CONTRIBUTORS The authors would like to acknowledge contributions from Greg Richardson, Josh Davis, Jose Guzman, George Pollock, Karen L. -
Falconsat‐7, a Deployable Membrane Optic Telescope
31st Space Symposium, Technical Track, Colorado Springs, Colorado, United States of America Presented on April 13, 2015 1 FalconSAT‐7, A Deployable Membrane Optic Telescope Brian A. Smith, [email protected] Geoff P. Andersen, [email protected], Olha Asmolova, [email protected], Anthony J. Hillesheim, [email protected], Matthew G. McHarg, [email protected], Jacob K. Snow, [email protected] ABSTRACT We report on the development of the flight model of FalconSAT‐7 (FS‐7), a 3U CubeSat with a deployable diffractive membrane solar telescope. The program is managed by undergraduate cadets at the Air Force Academy and is supported by graduate students at the Air Force Institute of Technology. The purpose of the mission is to demonstrate a deployable telescope with an aperture significantly larger than the spacecraft structure. The primary element deploys from one end of FS‐7 and has a clear aperture of 20 cm, twice the cross‐section of the host spacecraft structure. This novel payload is made possible by use of a thin (28 μm) membrane optic using diffractive principles to focus H‐alpha light from the Sun onto an onboard camera. The diffractive optic is deployed using a set of spring‐loaded pantographs that tension the membrane and hold it flat. The Colony‐II program office provided the 3U bus that is built by the Boeing Company. The FS‐7 mission is supported by the Defense Advanced Research Projects Agency (DARPA)’s Tactical Technology Office. The Air Force Academy plans to deliver FS‐7 to the Space Test Program for launch integration in late 2015 and expects FS‐7 to launch on STP‐2 in the spring of 2016.