An Ongoing Effort to Identify Near-Earth Asteroid Destination
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Onboard Determination of Vehicle Glide Capability for Shuttle Abort Flight Managment (Safm)
Source of Acquisition NASA Johnson Space Center ONBOARD DETERMINATION OF VEHICLE GLIDE CAPABILITY FOR SHUTTLE ABORT FLIGHT MANAGMENT (SAFM) Mark Jackson, Timothy Straube, Thomas Fill, Scott Nemeth, When one or more main engines fail during ascent, the flight crew of the Space Shuttle must make several critical decisions and accurately perform a series of abort procedures. One of the most important decisions for many aborts is the selection ofa landing site. Several factors influence the ability to reach a landing site, including the spacecraft point of atmospheric entry, the energy state at atmospheric entry, the vehicle glide capability from that energy state, and whether one or more suitable landing sites are within the glide capability. Energy assessment is further complicated by the fact that phugoid oscillations in total energy influence glide capability. Once the glide capability is known, the crew must select the "best" site option based upon glide capability and landing site conditions and facilities. Since most of these factors cannot currently be assessed by the crew in flight, extensive planning is required prior to each mission to script a variety of procedures based upon spacecraft velocity at the point of engine failure (or failures). The results of this pre flight planning are expressed in tables and diagrams on mission-specific cockpit checklists. Crew checklist procedures involve leafing through several pages of instructions and navigating a decision tree for site selection and flight procedures - all during a time critical abort situation. With the advent of the Cockpit Avionics Upgrade (CAU), the Shuttle will have increased on-board computational power to help alleviate crew workload during aborts and provide valuable situational awareness during nominal operations. -
Notes on Earth Atmospheric Entry for Mars Sample Return Missions
NASA/TP–2006-213486 Notes on Earth Atmospheric Entry for Mars Sample Return Missions Thomas Rivell Ames Research Center, Moffett Field, California September 2006 The NASA STI Program Office . in Profile Since its founding, NASA has been dedicated to the • CONFERENCE PUBLICATION. Collected advancement of aeronautics and space science. The papers from scientific and technical confer- NASA Scientific and Technical Information (STI) ences, symposia, seminars, or other meetings Program Office plays a key part in helping NASA sponsored or cosponsored by NASA. maintain this important role. • SPECIAL PUBLICATION. Scientific, technical, The NASA STI Program Office is operated by or historical information from NASA programs, Langley Research Center, the Lead Center for projects, and missions, often concerned with NASA’s scientific and technical information. The subjects having substantial public interest. NASA STI Program Office provides access to the NASA STI Database, the largest collection of • TECHNICAL TRANSLATION. English- aeronautical and space science STI in the world. language translations of foreign scientific and The Program Office is also NASA’s institutional technical material pertinent to NASA’s mission. mechanism for disseminating the results of its research and development activities. These results Specialized services that complement the STI are published by NASA in the NASA STI Report Program Office’s diverse offerings include creating Series, which includes the following report types: custom thesauri, building customized databases, organizing and publishing research results . even • TECHNICAL PUBLICATION. Reports of providing videos. completed research or a major significant phase of research that present the results of NASA For more information about the NASA STI programs and include extensive data or theoreti- Program Office, see the following: cal analysis. -
FCC-20-54A1.Pdf
Federal Communications Commission FCC 20-54 Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of ) ) Mitigation of Orbital Debris in the New Space Age ) IB Docket No. 18-313 ) REPORT AND ORDER AND FURTHER NOTICE OF PROPOSED RULEMAKING Adopted: April 23, 2020 Released: April 24, 2020 By the Commission: Chairman Pai and Commissioners O’Rielly, Carr, and Starks issuing separate statements; Commissioner Rosenworcel concurring and issuing a statement. Comment Date: (45 days after date of publication in the Federal Register). Reply Comment Date: (75 days after date of publication in the Federal Register). TABLE OF CONTENTS Heading Paragraph # I. INTRODUCTION .................................................................................................................................. 1 II. BACKGROUND .................................................................................................................................... 3 III. DISCUSSION ...................................................................................................................................... 14 A. Regulatory Approach to Mitigation of Orbital Debris ................................................................... 15 1. FCC Statutory Authority Regarding Orbital Debris ................................................................ 15 2. Relationship with Other U.S. Government Activities ............................................................. 20 3. Economic Considerations ....................................................................................................... -
Asteroid Retrieval Feasibility Study
Publications 4-2-2012 Asteroid Retrieval Feasibility Study John Brophy California Institute of Technology Fred Culick California Institute of Technology Louis Friedman The Planetary Society Pedro Llanos Embry-Riddle Aeronautical University - Daytona Beach, [email protected] et al. Follow this and additional works at: https://commons.erau.edu/publication Part of the Astrodynamics Commons, Space Vehicles Commons, and the The Sun and the Solar System Commons Scholarly Commons Citation Brophy, J., Culick, F., Friedman, L., Llanos, P., & al., e. (2012). Asteroid Retrieval Feasibility Study. , (). Retrieved from https://commons.erau.edu/publication/893 This Report is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Publications by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Asteroid Retrieval Feasibility Study 2 April 2012 Prepared for the: Keck Institute for Space Studies California Institute of Technology Jet Propulsion Laboratory Pasadena, California 1 2 Authors and Study Participants NAME Organization E-Mail Signature John Brophy Co-Leader / NASA JPL / Caltech [email protected] Fred Culick Co-Leader / Caltech [email protected] Co -Leader / The Planetary Louis Friedman [email protected] Society Carlton Allen NASA JSC [email protected] David Baughman Naval Postgraduate School [email protected] NASA ARC/Carnegie Mellon Julie Bellerose [email protected] University Bruce Betts The Planetary Society -
A Feasibility Study for Using Commercial Off the Shelf (COTS)
University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Masters Theses Graduate School 8-2011 A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2 Chad Lee Davis University of Tennessee - Knoxville, [email protected] Follow this and additional works at: https://trace.tennessee.edu/utk_gradthes Part of the Aerodynamics and Fluid Mechanics Commons, Other Aerospace Engineering Commons, and the Space Vehicles Commons Recommended Citation Davis, Chad Lee, "A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2. " Master's Thesis, University of Tennessee, 2011. https://trace.tennessee.edu/utk_gradthes/965 This Thesis is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by Chad Lee Davis entitled "A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the equirr ements for the degree of Master of Science, with a major in Aerospace Engineering. -
Uranus Atmospheric Entry Studies Final
Atmospheric Entry Studies for Uranus Parul Agrawal - ARC Gary Allen - ARC Helen Hwang -ARC Jose Aliaga - ARC Evgeniy Sklyanskiy - JPL MarkMarley - ARC Kathy McGuire - ARC LocHuynh - ARC Joseph Garcia - ARC Robert Moses- LaRC RickWinski - LaRC Funded by NASA In-Space Propulsion Program Questions and feedback : [email protected] Presentation: Outer Planet Assessment Group, Tucson, AZ, January 2014 Outline • Background ₋ Constraints ₋ Science Objectives ₋ Orbital Mechanics ₋ Atmosphere • Direct BallisticEntry • Aerocapture Entry • Conclusions& Recommendations 2 Background • Funded by Entry Vehicle Technology (EVT) project under In-Space Propulsion Technology (ISPT) • Concept studiesto understand the trade space for atmosphericentry, focusing on Venus, Saturn and Uranus ₋ Provide in-depth analysis of mission concepts outlined in the decadal survey for these planets ₋ These studies could be enabling for future Flagship and New Frontier missions designs • The results of this study will be published and presented at IEEE aerospace conference in Big Sky Montana, March 2014 In-Space Propulsion Technology (ISPT) . 3 Study Objectives • Establish a range of probe atmosphericentry environmentsbased on the UranusFlagship mission in the 2013-23 Planetary Science Decadal Survey ₋ Two Launch windows 2021 and 2034 are being considered for this study • Define Uranusentry trade space by performing parametricstudies, by varying ballisticcoefficient (vehicle mass, size) and Entry Flight Path Angle (EFPA) • Investigate entry trajectory options, including -
Photometric Study of Two Near-Earth Asteroids in the Sloan Digital Sky Survey Moving Objects Catalog
University of North Dakota UND Scholarly Commons Theses and Dissertations Theses, Dissertations, and Senior Projects January 2020 Photometric Study Of Two Near-Earth Asteroids In The Sloan Digital Sky Survey Moving Objects Catalog Christopher James Miko Follow this and additional works at: https://commons.und.edu/theses Recommended Citation Miko, Christopher James, "Photometric Study Of Two Near-Earth Asteroids In The Sloan Digital Sky Survey Moving Objects Catalog" (2020). Theses and Dissertations. 3287. https://commons.und.edu/theses/3287 This Thesis is brought to you for free and open access by the Theses, Dissertations, and Senior Projects at UND Scholarly Commons. It has been accepted for inclusion in Theses and Dissertations by an authorized administrator of UND Scholarly Commons. For more information, please contact [email protected]. PHOTOMETRIC STUDY OF TWO NEAR-EARTH ASTEROIDS IN THE SLOAN DIGITAL SKY SURVEY MOVING OBJECTS CATALOG by Christopher James Miko Bachelor of Science, Valparaiso University, 2013 A Thesis Submitted to the Graduate Faculty of the University of North Dakota in partial fulfillment of the requirements for the degree of Master of Science Grand Forks, North Dakota August 2020 Copyright 2020 Christopher J. Miko ii Christopher J. Miko Name: Degree: Master of Science This document, submitted in partial fulfillment of the requirements for the degree from the University of North Dakota, has been read by the Faculty Advisory Committee under whom the work has been done and is hereby approved. ____________________________________ Dr. Ronald Fevig ____________________________________ Dr. Michael Gaffey ____________________________________ Dr. Wayne Barkhouse ____________________________________ Dr. Vishnu Reddy ____________________________________ ____________________________________ This document is being submitted by the appointed advisory committee as having met all the requirements of the School of Graduate Studies at the University of North Dakota and is hereby approved. -
Planned Yet Uncontrolled Re-Entries of the Cluster-Ii Spacecraft
PLANNED YET UNCONTROLLED RE-ENTRIES OF THE CLUSTER-II SPACECRAFT Stijn Lemmens(1), Klaus Merz(1), Quirin Funke(1) , Benoit Bonvoisin(2), Stefan Löhle(3), Henrik Simon(1) (1) European Space Agency, Space Debris Office, Robert-Bosch-Straße 5, 64293 Darmstadt, Germany, Email:[email protected] (2) European Space Agency, Materials & Processes Section, Keplerlaan 1, 2201 AZ Noordwijk, Netherlands (3) Universität Stuttgart, Institut für Raumfahrtsysteme, Pfaffenwaldring 29, 70569 Stuttgart, Germany ABSTRACT investigate the physical connection between the Sun and Earth. Flying in a tetrahedral formation, the four After an in-depth mission analysis review the European spacecraft collect detailed data on small-scale changes Space Agency’s (ESA) four Cluster II spacecraft in near-Earth space and the interaction between the performed manoeuvres during 2015 aimed at ensuring a charged particles of the solar wind and Earth's re-entry for all of them between 2024 and 2027. This atmosphere. In order to explore the magnetosphere was done to contain any debris from the re-entry event Cluster II spacecraft occupy HEOs with initial near- to southern latitudes and hence minimise the risk for polar with orbital period of 57 hours at a perigee altitude people on ground, which was enabled by the relative of 19 000 km and apogee altitude of 119 000 km. The stability of the orbit under third body perturbations. four spacecraft have a cylindrical shape completed by Small differences in the highly eccentric orbits of the four long flagpole antennas. The diameter of the four spacecraft will lead to various different spacecraft is 2.9 m with a height of 1.3 m. -
Statistical Survey and Analysis of Photometric and Spectroscopic Data on Neas
Global Journal of Environmental Science and Research ISSN: 2349-7335 Volume 3, No. 2 (April – June 2016) STATISTICAL SURVEY AND ANALYSIS OF PHOTOMETRIC AND SPECTROSCOPIC DATA ON NEAS J. Rukmini1, G. Raghavendra2, S.A.Ahmed1, D. Shanti Priya1 and Syeda Azeem Unnisa3 1Department of Astronomy, Osmania University, Hyderabad 2Nizam College, Osmania University, Hyderabad 3Department of Environmental Science, Osmania University, Hyderabad ABSTRACT Studies on Near Earth Asteroids (NEAs) throw light on discoveries, identification, orbit prediction and civil alert capabilities, including potential asteroid impact hazards. Due to various new observational programs, the discovery rate of NEAs has drastically increased over the last few years. In this paper we present the statistical survey and analysis of fundamental parameters (derived from Photometric and Spectroscopic observations) of a large sample of NEAs from various databases like IAU Minor Planet Center, European Asteroid Research Node (E.A.R.N.), Near Earth Objects - Dynamic Site (NEODyS- 2), M4AST and SMASSMTT portals. We also discuss the characterization of NEAs on the basis of the correlations between the parameters studied from different observations and their physical implications in understanding the nature and physical properties of these objects. Keywords: NEOs; Apollo; Amor; Aten; Observations: Photometric, Spectroscopic. INTRODUCTION Johannes Schmidt proposed that asteroids repre- sented an arrested stage of planet formation which Asteroids are rocky and metallic objects which could not coalesce into a single large body. To- are assumed to be left over pieces from the early day around 700,000 asteroids have been discov- solar system, 4.6 billion years ago. Asteroids have ered with known orbits, giving insight into the been discovered within the solar system and are Asteroid Belt’s dynamic past. -
1 ABSTRACT Aside from the Exploration of Mars, the Objects That
IAC-07-B3.5.06 INTO THE BEYOND: A CREWED MISSION TO A NEAR-EARTH OBJECT David J. Korsmeyer, NASA Ames Research Center, Intelligent Systems Division, Moffett Field, CA, USA, [email protected] Rob R. Landis, NASA Johnson Space Center, Mission Operations Directorate, Houston, TX, USA [email protected] Paul A. Abell, NASA Johnson Space Center, Astromaterials Research & Exploration Science, Houston, TX, USA [email protected] ABSTRACT utility and opportunities for the developing Aside from the exploration of Mars, the Constellation infrastructure, particularly, the objects that most capture our interest for a Ares Launch vehicles and the Orion crewed new human visit are the Near-Earth Objects spacecraft, to be used for missions that were (NEOs). These objects are ideal candidates not directly in the design specifications (aka for deep space operations and explorations as non-lunar missions). The Ares and Orion we extend the human presence out into the systems are designed to launch 4-6 crew to solar system. The notion of a crewed mission the International Space Station (ISS), and to to a NEO was first discussed in the Apollo eventually take 4 crew back to lunar orbit era. The most recent assessment has been where a lunar lander would take the crew to undertaken by the Advanced Projects Office the surface. within NASA’s Constellation Program. This particular study examined the feasibility of The NASA Constellation Program wanted to sending NASA’s new Orion spacecraft (also understand what are some other feasible, referred to as the Crew Exploration Vehicle, high-value uses of the Orion spacecraft and or CEV) to a NEO. -
Asteroid Retrieval Mission Concept – Trailblazing Our Future in Space and Helping to Protect Us from Earth Impactors
Asteroid Retrieval Mission Concept – Trailblazing Our Future in Space and Helping to Protect Us from Earth Impactors Presented by Dan Mazanek1 Co-authors: John Brophy2 and Gabe Merrill1 1NASA Langley Research Center; 2Jet Propulsion Laboratory April 16, 2013 2013 Planetary Defense Conference Flagstaff, USA Paper No: IAA-PDC13-04-14 1 Background The idea of utilizing asteroidal resources is not new • 1903 – Konstantin Tsiolkovskii included the concept of using asteroids for resources in his most famous publication, The Exploration of Cosmic Space by Means of Reaction Motors • 1977 – NASA’s Dr. Brian O’Leary proposed using mass drivers to move Earth- approaching Apollo and Amor asteroids to Earth’s vicinity • 1997 – Dr. John S. Lewis detailed how we can extract the vast resources available from our solar system in the influential book Mining the Sky: Untold Riches from the Asteroids, Comets, and Planets September 2011 and February 2012 – Asteroid Retrieval Mission (ARM) Study at Caltech’s Keck Institute for Space Studies (KISS) • Examined the feasibility of returning a small (~7 m diameter) near-Earth asteroid (NEA), or part of a large NEA, to cislunar space • Utilize robotic 50 kW-class solar electric propulsion (SEP) vehicle and currently available technologies (40 kW available to the electric propulsion system) • John Brophy (Co-Leader along with Louis Friedman and Fred Culick) and Dan Mazanek were KISS ARM study members 2 Recent Events Recent events have elevated the public’s awareness of the potential of space resources and have -
Asteroids + Comets
Datasets for Asteroids and Comets Caleb Keaveney, OpenSpace intern Rachel Smith, Head, Astronomy & Astrophysics Research Lab North Carolina Museum of Natural Sciences 2020 Contents Part 1: Visualization Settings ………………………………………………………… 3 Part 2: Near-Earth Asteroids ………………………………………………………… 5 Amor Asteroids Apollo Asteroids Aten Asteroids Atira Asteroids Potentially Hazardous Asteroids (PHAs) Mars-crossing Asteroids Part 3: Main-Belt Asteroids …………………………………………………………… 12 Inner Main Asteroid Belt Main Asteroid Belt Outer Main Asteroid Belt Part 4: Centaurs, Trojans, and Trans-Neptunian Objects ………………………….. 15 Centaur Objects Jupiter Trojan Asteroids Trans-Neptunian Objects Part 5: Comets ………………………………………………………………………….. 19 Chiron-type Comets Encke-type Comets Halley-type Comets Jupiter-family Comets C 2019 Y4 ATLAS About this guide This document outlines the datasets available within the OpenSpace astrovisualization software (version 0.15.2). These datasets were compiled from the Jet Propulsion Laboratory’s (JPL) Small-Body Database (SBDB) and NASA’s Planetary Data Service (PDS). These datasets provide insights into the characteristics, classifications, and abundance of small-bodies in the solar system, as well as their relationships to more prominent bodies. OpenSpace: Datasets for Asteroids and Comets 2 Part 1: Visualization Settings To load the Asteroids scene in OpenSpace, load the OpenSpace Launcher and select “asteroids” from the drop-down menu for “Scene.” Then launch OpenSpace normally. The Asteroids package is a big dataset, so it can take a few hours to load the first time even on very powerful machines and good internet connections. After a couple of times opening the program with this scene, it should take less time. If you are having trouble loading the scene, check the OpenSpace Wiki or the OpenSpace Support Slack for information and assistance.