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PREFACE This Draft Environmental Assessment for the Expansion of the Wallops Flight Facility Launch Range has been developed by URS Group, Inc. (URS) and EG&G Technical Services (EG&G) for the National Aeronautics and Space Administration (NASA) Goddard Space Flight Center’s (GSFC) Wallops Flight Facility (WFF) and the Mid-Atlantic Regional Spaceport (MARS). URS/EG&G have prepared this report for the exclusive use of WFF in accordance with the National Environmental Policy Act of 1969 (NEPA), as amended (42 U.S.C. 4321-4347), the Council on Environmental Quality (CEQ) regulations for implementing NEPA (40 CFR 1500- 1508), NASA’s regulations for implementing NEPA (14 CFR Subpart 1216.3), and the NASA Procedural Requirement (NPR) for implementing NEPA and Executive Order 12114 (NPR 8580.1) (NASA, 2001). Executive Summary DRAFT ENVIRONMENTAL ASSESSMENT EXPANSION OF THE WALLOPS FLIGHT FACILITY LAUNCH RANGE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION GODDARD SPACE FLIGHT CENTER WALLOPS FLIGHT FACILITY WALLOPS ISLAND, VA 23337 Lead Agency: National Aeronautics and Space Administration Cooperating Agency: Federal Aviation Administration Office of Commercial Space Transportation Proposed Action: Expansion of the Wallops Flight Facility Launch Range on Wallops Island For Further Information: Joshua A. Bundick NEPA Program Manager Code 250.W Goddard Space Flight Center’s Wallops Flight Facility National Aeronautics and Space Administration Wallops Island, VA 23337 (757) 824-2319 Date: April 2009 ABSTRACT This Environmental Assessment addresses the proposed expansion of the launch range at the National Aeronautics and Space Administration (NASA) Goddard Space Flight Center (GSFC) Wallops Flight Facility (WFF), which is located on the Eastern Shore of Virginia. -
Project Argonaut: a Proposal for a Mars Sample Return Mission ∗
Project Argonaut: A Proposal for a Mars Sample Return Mission ∗ Archit Arora, Courtney Best, Liam Durbin, Robert Groome, Duncan Harris, Henry Heim, Thomas Keane, Eric Miller, Annie Ping, and Alexandra Wyatt Purdue University, West Lafayette, Indiana, 47906, United States With increasing interest in colonizing Mars, multiple missions have been aimed at re- trieving more information about the red planet, such as the recent Mars Science Laboratory mission. The main focus of this interest is in determining whether Mars is capable of sup- porting life, which requires an analysis of the soil. The next major step in Martian science is a Mars Sample Return mission, which would allow scientists to conduct complicated and in-depth tests on the soil that are not possible with robotic instruments sent to Mars. This paper explores Project Argonaut, a mission proposal to retrieve a sample from the surface of Mars and bring it back to Earth. The name Argonaut reflects the legend of the band of heroes who sailed on the Argo to fetch the golden fleece from the field of Ares, as the mis- sion requires a journey to Mars in order to retrieve the prized sample. Project Argonaut integrates existing research with innovative concepts to propose a plausible solution to the key issues associated with the mission. ∗Copyright c 2016 by Archit Arora, Courtney Best, Liam Durbin, Robert Groome, Duncan Harris, Henry Heim, Thomas Keane, Eric Miller, Annie Ping, and Alexandra Wyatt. Published by the American Institute of Aeronautics and Astronautics, Inc, with permission. 1 of 51 American Institute of Aeronautics and Astronautics Contents I Introduction 6 A Mission Objective . -
Spacex's Expanding Launch Manifest
October 2013 SpaceX’s expanding launch manifest China’s growing military might Servicing satellites in space A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS SpaceX’s expanding launch manifest IT IS HARD TO FIND ANOTHER SPACE One of Brazil, and the Turkmensat 1 2012, the space docking feat had been launch services company with as di- for the Ministry of Communications of performed only by governments—the verse a customer base as Space Explo- Turkmenistan. U.S., Russia, and China. ration Technologies (SpaceX), because The SpaceX docking debunked there simply is none. No other com- A new market the myth that has prevailed since the pany even comes close. Founded only The move to begin launching to GEO launch of Sputnik in 1957, that space a dozen years ago by Elon Musk, is significant, because it opens up an travel can be undertaken only by na- SpaceX has managed to win launch entirely new and potentially lucrative tional governments because of the contracts from agencies, companies, market for SpaceX. It also puts the prohibitive costs and technological consortiums, laboratories, and univer- company into direct competition with challenges involved. sities in the U.S., Argentina, Brazil, commercial launch heavy hitters Ari- Teal Group believes it is that Canada, China, Germany, Malaysia, anespace of Europe with its Ariane mythology that has helped discourage Mexico, Peru, Taiwan, Thailand, Turk- 5ECA, U.S.-Russian joint venture Inter- more private investment in commercial menistan, and the Netherlands in a rel- national Launch Services with its Pro- spaceflight and the more robust growth atively short period. -
A Methodology for Cubesat Mission Selection Luis Zea, Victor Ayerdi, Sergio Argueta, and Antonio Muñoz Universidad Del Valle De Guatemala, Guatemala City, Guatemala
Zea, L. et al. (2016): JoSS, Vol. 5, No. 3, pp. 483–511 (Peer-reviewed article available at www.jossonline.com) www.DeepakPublishing.com www. JoSSonline.com A Methodology for CubeSat Mission Selection Luis Zea, Victor Ayerdi, Sergio Argueta, and Antonio Muñoz Universidad del Valle de Guatemala, Guatemala City, Guatemala Abstract Over 400 CubeSats have been launched during the first 13 years of existence of this 10 cm cube-per unit standard. The CubeSat’s flexibility to use commercial-off-the-shelf (COTS) parts and its standardization of in- terfaces have reduced the cost of developing and operating space systems. This is evident by satellite design projects where at least 95 universities and 18 developing countries have been involved. Although most of these initial projects had the sole mission of demonstrating that a space system could be developed and operated in- house, several others had scientific missions on their own. The selection of said mission is not a trivial process, however, as the cost and benefits of different options need to be carefully assessed. To conduct this analysis in a systematic and scholarly fashion, a methodology based on maximizing the benefits while considering program- matic risk and technical feasibility was developed for the current study. Several potential mission categories, which include remote sensing and space-based research, were analyzed for their technical requirements and fea- sibility to be implemented on CubeSats. The methodology helps compare potential missions based on their rele- vance, risk, required resources, and benefits. The use of this flexible methodology—as well as its inputs and outputs—is demonstrated through a case study. -
Aerospace Frontiers April 2019
VOLUME 21 • ISSUE 3 • APRIL 2019 Glenn Keeps X–57 Cool Page 4 Senior Leaders Move On Page 5 Your Records Count Sharing #MoontoMars Page 9 Pages 2–3 Moon to Mars Event Valuable Contributions to Draws Media, Crew Dragon Demo-1 Mission Success Social Influencers On March 8, the SpaceX Crew Dragon NASA Glenn joined centers throughout the agency Demo-1 completed its 5-day mission to the International Space Station (ISS), in welcoming members of the media and social media the first orbital test of this spacecraft. for a Moon to Mars event on March 11. This spacecraft has been years in the making and Glenn touched on many Photo by Bridget Caswell aspects of its success. The docking to GRC-2019-C-00582 the ISS was safely accomplished in part by the Glenn Seals team who developed the unique seals for the main interface to prevent cabin air leakage. The Plum Brook Station team provided test verifi- cation in complex space environments. I appreciate all our contributions to this mission, a mission that will lead to the United States’ first crew transport to the ISS since the space shuttle. Thank you for working with our commercial partners to assure safety and mission success! AeroSpace Frontiers is an official publication of Glenn Research Center, National Aeronautics and Space Administration. It is published the second Space Flight Systems Director Bryan Smith, left, and Chief Financial Officer Friday of each month by the Office of Larry Sivic, right, answer questions about the Orion spacecraft from local media. Communications & External Relations in the interest of the Glenn workforce, retirees, government officials, business leaders and the general public. -
Near Earth Asteroid (NEA) Scout
Near Earth Asteroid (NEA) Scout Les Johnson, Jared Dervan and Leslie McNutt NASA George C. Marshall Space Flight Center Julie Castillo-Rogez NASA Jet Propulsion Laboratory 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 (EM-1/2018) • 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 Sponsoring Organization within NASA • Human Exploration and Operations Mission Directorate (HEOMD) Advanced Exploration Systems (AES) selected 3 cubesats for flight on the first flight of the Space Launch System • Primary selection criteria: - Relevance to Space Exploration Strategic Knowledge Gaps (SKGs) - Life cycle cost - Synergistic use of previously demonstrated technologies Payload Strategic Knowledge Gaps Mission Concept NASA Centers Addressed BioSentinel Human health/performance in high- Study radiation-induced DNA ARC/JSC radiation space environments damage of live organisms in cis- • Fundamental effects on biological systems lunar space; correlate with of ionizing radiation in space environments measurements on ISS and Earth Lunar -
A Sample AMS Latex File
PLEASE SEE CORRECTED APPENDIX A IN CORRIGENDUM, JOSS VOL. 6, NO. 3, DECEMBER 2017 Zea, L. et al. (2016): JoSS, Vol. 5, No. 3, pp. 483–511 (Peer-reviewed article available at www.jossonline.com) www.DeepakPublishing.com www. JoSSonline.com A Methodology for CubeSat Mission Selection Luis Zea, Victor Ayerdi, Sergio Argueta, and Antonio Muñoz Universidad del Valle de Guatemala, Guatemala City, Guatemala Abstract Over 400 CubeSats have been launched during the first 13 years of existence of this 10 cm cube-per unit standard. The CubeSat’s flexibility to use commercial-off-the-shelf (COTS) parts and its standardization of in- terfaces have reduced the cost of developing and operating space systems. This is evident by satellite design projects where at least 95 universities and 18 developing countries have been involved. Although most of these initial projects had the sole mission of demonstrating that a space system could be developed and operated in- house, several others had scientific missions on their own. The selection of said mission is not a trivial process, however, as the cost and benefits of different options need to be carefully assessed. To conduct this analysis in a systematic and scholarly fashion, a methodology based on maximizing the benefits while considering program- matic risk and technical feasibility was developed for the current study. Several potential mission categories, which include remote sensing and space-based research, were analyzed for their technical requirements and fea- sibility to be implemented on CubeSats. The methodology helps compare potential missions based on their rele- vance, risk, required resources, and benefits. -
Pawlikowski Tenure Marked by Effectiveness, Air Force Readiness
PRSRT STD US POSTAGE PAID TULLAHOMA TN Vol. 65, No. 16 Arnold AFB, Tenn. PERMIT NO. 29 August 20, 2018 Pawlikowski tenure marked by effectiveness, Air Force readiness By Marisa Alia-Novobilski Air Force Materiel Command WRIGHT-PATTERSON AIR FORCE BASE, Ohio – It’s the little things that our command does every day that enable the Air Force to be effective, and it’s so important that our Airmen fully appreciate their impact, said Air Force Gen. Ellen M. Pawlikowski, as she reflected on her three years at the helm of Air Force Materiel Command and read- ies to retire from 40 years of Air Force service this September. “We don’t fly airplanes, and we don’t drop the bombs, but we make sure the airplanes can fly, and that the bombs are reliable, and their radars work,” she said. “AFMC Airmen need to understand that what they do is important. They literally hold in their hands the health and the safety of our Airmen.” Pawlikowski took command of AFMC in 2015 during a time when the Air Force was highly focused on efficien- cy and cost consciousness, punctuating years of sequestration and resource re- duction across the military fiscal domain. The command had just experienced a 33 percent reduction in headquarters staff, and across the board, said Pawlikowski, everything drove toward maintaining the bottom line. Gen. Ellen M. Pawlikowski, Air Force Materiel Command commander, greets well-wishers, Aug. 7 on the Wright-Pat- terson Air Force Base, Ohio, flight line following her fini flight. Pawlikowski relinquished command Aug. -
Guidance, Navigation, and Control of Small Satellite Attitude Using Micro-Thrusters
GUIDANCE, NAVIGATION, AND CONTROL OF SMALL SATELLITE ATTITUDE USING MICRO-THRUSTERS A DISSERTATION SUBMITTED TO THE GRADUATE DIVISION OF THE UNIVERSITY OF HAWAI‘I AT MANOA¯ IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN MECHANICAL ENGINEERING DECEMBER 2016 by Cullen Matsumoto Dissertation Committee: Dilmurat Azimov, Chairperson Peter Berkelman Reza Ghorbani ABSTRACT In this study, a new and automated Navigation, Guidance and Control system is designed, analyzed, simulated and tested for small satellites. As is known, this system represents the primary unit of on-board control of a flight vehicle. It consists of a set of system software algorithms and hardware elements, including various sets of sensors and electronics depending on the type of the vehicle. This study is focused on small satellites, which are becoming one of the primary tools for a wide range of low Earth and deep space missions. The Navigation subsystem has been described in terms of its sensors and filtering technique, known as the Extended Kalman Filter. This subsystem provides the estimates of the satellite’s state vector. It is assumed that this vehicle’s Navigation subsystem includes GPS receiver, and accelerometer and gyro, which are considered as Inertial measurement Unit (IMU) component subsystems. The Guidance subsystem provides guidance commands for satellite’s actuators, which are assumed to include a set of micro-thrusters. The Control subsystem provides control commands for increments of torque of actuation. This study deals with the development, design and integration of the Navigation, Guidance and Control (known as GNC) subsystems into a unique framework that can be executed on-board in real time to perform satellite attitude maneuvers. -
Us Rocket Propulsion Industrial Base Assessment
OMB Control Number: ####-#### Expiration Date: 12/31/2017 U.S. ROCKET PROPULSION INDUSTRIAL BASE ASSESSMENT: Propulsion Survey SCOPE OF ASSESSMENT The U.S. Department of Commerce, Bureau of Industry and Security (BIS), Office of Technology Evaluation (OTE), in coordination with the U.S. National Aeronautics and Space Administration (NASA) and U.S. Department of Defense (DOD) co-chaired Joint Army, Navy, NASA, Air Force Interagency Propulsion Committee (JANNAF) is conducting a survey and assessment of organizations responsible for the research, design, engineering, development, manufacture, testing, and integration of rocket propulsion-related products, components, and services. The principal goal of this assessment is to gain an understanding of the intricate supply chain network supporting the development, production, and sustainment of products and services across both the U.S. Government and commercial propulsion-related sectors. With the data collected in this survey, U.S. Government agencies will be better informed and able to develop targeted planning, acquisition, and investment strategies to ensure industry's ability to support critical defense and civil missions and programs. RESPONSE TO THIS SURVEY IS REQUIRED BY LAW A response to this survey is required by law (50 U.S.C. App. Sec. 2155). Failure to respond can result in a maximum fine of $10,000, imprisonment of up to one year, or both. Information furnished herewith is deemed confidential and will not be published or disclosed except in accordance with Section 705 of the Defense Production Act of 1950, as amended (50 U.S.C App. Sec. 2155). Section 705 prohibits the publication or disclosure of this information unless the President determines that its withholding is contrary to the national defense. -
SMALL SATELLITES – Economic Trends
SMALL SATELLITES Economic Trends Giovanni Facchinetti Intern – Defence SA – Space Industry and R&D Collaborations Master’s candidate – Universita’ Commerciale Luigi Bocconi, Milano Supervisors: Nicola Sasanelli AM Director – Space Industry and R&D Collaborations Defence SA Government of South Australia Michael Davis Chair SIAA – Space Industry Association of Australia www.spaceindustry.com.au Giovanni Cucinella Director, General IMT – Ingegneria Marketing Tecnologia www.imtsrl.it December 2016 “Quod Invenias Explorans Spatium Progressus Est Humanitatis” - Human Progress is in Space Exploration Hon Jay Weatherill - Premier of South Australia Facchinetti G, Sasanelli N, Davis M, Cucinella G SMALL SATELLITES – economic trends Disclaimer While every effort has been made to ensure the accuracy of the information contained in this report, the conclusions and the recommendations included in it constitute the opinions of the authors and should not be taken as representative of the views of Defence SA and the South Australian Government. No warranty, express or implied is made regarding the accuracy, adequacy, completeness, reliability or usefulness of the whole or any part of the information contained in this document. You should seek your own independent expert advice and make your own enquiries and satisfy yourself of all aspects of the information contained in this document. Any use or reliance on any of information contained in this document is at your own risk in all things. The Government of South Australia and its servants and its agents disclaim all liability and responsibility (including for negligence) for any direct or indirect loss or damage which may be suffered by any person through using or relying on any of the information contained in this document. -
Testing Program for Kysat‐1
University of Kentucky UKnowledge University of Kentucky Master's Theses Graduate School 2010 TESTING PROGRAM FOR KYSAT‐1 Jason Robert Bratcher University of Kentucky, [email protected] Right click to open a feedback form in a new tab to let us know how this document benefits ou.y Recommended Citation Bratcher, Jason Robert, "TESTING PROGRAM FOR KYSAT‐1" (2010). University of Kentucky Master's Theses. 3. https://uknowledge.uky.edu/gradschool_theses/3 This Thesis is brought to you for free and open access by the Graduate School at UKnowledge. It has been accepted for inclusion in University of Kentucky Master's Theses by an authorized administrator of UKnowledge. For more information, please contact [email protected]. ABSTRACT OF THESIS TESTING PROGRAM FOR KYSAT‐1 Years of success in the aerospace industry has taught Kentucky Space several lessons. This thesis will summarize the accomplishments in an attempt to formulate a well-defined program for designing and testing small spacecraft in an environment with strict financial restraints. The motivation for producing this well-defined platform for testing small spacecraft arose when Kentucky Space became the liaison between NASA and its customers for the NanoRacks and CubeLab module program. Having a solid program for testing small spacecraft will allow future student programs to easily set standards for experiment payloads. Also by discussing obstacles for smaller programs such as restraints on funding, scheduling restrictions, and testing facility procurement, this thesis will provide a basis that other programs can use to start or expand a space research program that may be struggling due to mistakes that programs face in the early years due to the lack of experience and maturity of a veteran program.