Communications Enabling Science from the 2050 Heliophysics System Observatory 1 2 3 4 2 Authors: S
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NASA's STEREO Mission
NASA’s STEREO Mission J.B. Gurman STEREO Project Scientist W.T. Thompson STEREO Chief Observer Solar Physics Laboratory, Helophysics Division NASA Goddard Space Flight Center 1 The STEREO Mission • Science and technology definition team report, 1997 December: • Understand the origin and consequences of coronal mass ejections (CMEs) • Two spacecraft in earth-leading and -lagging orbits near 1 AU (Solar Terrestrial Probe line) • “Beacon” mode for near-realtime warning of potentially geoeffective events 2 Level 1 Requirements • Understand the causes and mechanisms of CME initiation • Characterize the propagation of CMEs through the heliosphere • Discover the mechanisms and sites of energetic particle acceleration in the low corona and the interplanetary medium • Develop a 3D, time-dependent model of the magnetic topology, temperature, density, and velocity structure of the ambient solar wind 3 Implementation • Two nearly identical spacecraft launched by a single ELV • Bottom spacecraft in stack has adapter ring, some strengthening • Spacecraft built at Johns Hopkins University APL • Four science investigations 4 Scientific Instruments • S/WAVES - broad frequency response RF detection of Type II, III bursts • PLASTIC - solar wind plasma and suprathermal ion composition measurements • IMPACT - energetic electrons and ions, magnetic field • SECCHI - EUV, coronagraphs and heliospheric imagers (surface to 1.5 AU) 5 Instrument Hardware • PLASTIC IMPACT boom IMPACT boom SECCHI SCIP SECCHI HI S/WAVES 6 Orbit Design • Science team selected a separation -
Nustar Observatory Guide
NuSTAR Guest Observer Program NuSTAR Observatory Guide Version 3.2 (June 2016) NuSTAR Science Operations Center, California Institute of Technology, Pasadena, CA NASA Goddard Spaceflight Center, Greenbelt, MD nustar.caltech.edu heasarc.gsfc.nasa.gov/docs/nustar/index.html i Revision History Revision Date Editor Comments D1,2,3 2014-08-01 NuSTAR SOC Initial draft 1.0 2014-08-15 NuSTAR GOF Release for AO-1 Addition of more information about CZT 2.0 2014-10-30 NuSTAR SOC detectors in section 3. 3.0 2015-09-24 NuSTAR SOC Update to section 4 for release of AO-2 Update for NuSTARDAS v1.6.0 release 3.1 2016-05-10 NuSTAR SOC (nusplitsc, Section 5) 3.2 2016-06-15 NuSTAR SOC Adjustment to section 9 ii Table of Contents Revision History ......................................................................................................................................................... ii 1. INTRODUCTION ................................................................................................................................................... 1 1.1 NuSTAR Program Organization ..................................................................................................................................................................................... 1 2. The NuSTAR observatory .................................................................................................................................... 2 2.1 NuSTAR Performance ........................................................................................................................................................................................................ -
Collision Avoidance Operations in a Multi-Mission Environment
AIAA 2014-1745 SpaceOps Conferences 5-9 May 2014, Pasadena, CA Proceedings of the 2014 SpaceOps Conference, SpaceOps 2014 Conference Pasadena, CA, USA, May 5-9, 2014, Paper DRAFT ONLY AIAA 2014-1745. Collision Avoidance Operations in a Multi-Mission Environment Manfred Bester,1 Bryce Roberts,2 Mark Lewis,3 Jeremy Thorsness,4 Gregory Picard,5 Sabine Frey,6 Daniel Cosgrove,7 Jeffrey Marchese,8 Aaron Burgart,9 and William Craig10 Space Sciences Laboratory, University of California, Berkeley, CA 94720-7450 With the increasing number of manmade object orbiting Earth, the probability for close encounters or on-orbit collisions is of great concern to spacecraft operators. The presence of debris clouds from various disintegration events amplifies these concerns, especially in low- Earth orbits. The University of California, Berkeley currently operates seven NASA spacecraft in various orbit regimes around the Earth and the Moon, and actively participates in collision avoidance operations. NASA Goddard Space Flight Center and the Jet Propulsion Laboratory provide conjunction analyses. In two cases, collision avoidance operations were executed to reduce the risks of on-orbit collisions. With one of the Earth orbiting THEMIS spacecraft, a small thrust maneuver was executed to increase the miss distance for a predicted close conjunction. For the NuSTAR observatory, an attitude maneuver was executed to minimize the cross section with respect to a particular conjunction geometry. Operations for these two events are presented as case studies. A number of experiences and lessons learned are included. Nomenclature dLong = geographic longitude increment ΔV = change in velocity dZgeo = geostationary orbit crossing distance increment i = inclination Pc = probability of collision R = geostationary radius RE = Earth radius σ = standard deviation Zgeo = geostationary orbit crossing distance I. -
SSC Tenant Meeting: NASA Near Earth Network (NENJ Overview
https://ntrs.nasa.gov/search.jsp?R=20180001495 2019-08-30T12:23:41+00:00Z SSC Tenant Meeting: NASA Near Earth Network (NENJ Overview --- --- ~ I - . - - Project Manager: David Carter Deputy Project Manager: Dave Larsen Chief Engineer: Philip Baldwin Financial Manager: Cristy Wilson Commercial Service Manager: LaMont Ruley ============== February ==============21, 2018 Agenda > NEN Overview > NEN / SSC Relationship > NEN Missions > Future Trends S1ide2 The Near Earth Network (NEN) consists of globally distributed tracking stations that are strategically located throughout the world which provide Telemetry, Tracking, and Commanding (TT&C) services support to a variety of orbital and suborbital flight missions, including Low Earth Orbit (LEO), Geosynchronous Earth Orbit (GEO), highly elliptical, and lunar orbits Network: The NEN is one of.three networks that together comprise the NASA1s Space Communications and Navigation (SCaN) Networks The NEN provides cost-effective, high data rate services from a global set of NASA, commercial, and partner ground stations to a mission set that requires hourly to daily contacts Missions: The NEN provides communication services to: - Earth Science missions such as Aqua, Aura, OC0-2, QuikSCAT, and SMAP - Space Science missions including AIM, FSGT, IRIS, NuSTAR, and Swift - Lunar orbiting missions such as LRO - CubeSat missions including the upcoming CryoCube, iSAT, and SOCON Stations: The NEN consists of several polar stations which are vital to polar orbiting missions since they enable communications services -
The Deep Space Network - a Technology Case Study and What Improvements to the Deep Space Network Are Needed to Support Crewed Missions to Mars?
The Deep Space Network - A Technology Case Study and What Improvements to the Deep Space Network are Needed to Support Crewed Missions to Mars? A Master’s Thesis Presented to Department of Telecommunications State University of New York Polytechnic Institute Utica, New York In Partial Fulfillment of the Requirements for the Master of Science Degree By Prasad Falke May 2017 Abstract The purpose of this thesis research is to find out what experts and interested people think about Deep Space Network (DSN) technology for the crewed Mars mission in the future. The research document also addresses possible limitations which need to be fix before any critical missions. The paper discusses issues such as: data rate, hardware upgrade and new install requirement and a budget required for that, propagation delay, need of dedicated antenna support for the mission and security constraints. The Technology Case Study (TCS) and focused discussion help to know the possible solutions and what everyone things about the DSN technology. The public platforms like Quora, Reddit, StackExchange, and Facebook Mars Society group assisted in gathering technical answers from the experts and individuals interested in this research. iv Acknowledgements As the thesis research was challenging and based on the output of the experts and interested people in this field, I would like to express my gratitude and appreciation to all the participants. A special thanks go to Dr. Larry Hash for his guidance, encouragement, and support during the whole time. Additionally, I also want to thank my mother, Mrs. Mangala Falke for inspiring me always. Last but not the least, I appreciate the support from Maricopa County Emergency Communications Group (MCECG) and Arizona Near Space Research (ANSR) Organization for helping me to find the experts in space and communications field. -
Complete List of Contents
Complete List of Contents Volume 1 Cape Canaveral and the Kennedy Space Center ......213 Publisher’s Note ......................................................... vii Chandra X-Ray Observatory ....................................223 Introduction ................................................................. ix Clementine Mission to the Moon .............................229 Preface to the Third Edition ..................................... xiii Commercial Crewed vehicles ..................................235 Contributors ............................................................. xvii Compton Gamma Ray Observatory .........................240 List of Abbreviations ................................................. xxi Cooperation in Space: U.S. and Russian .................247 Complete List of Contents .................................... xxxiii Dawn Mission ..........................................................254 Deep Impact .............................................................259 Air Traffic Control Satellites ........................................1 Deep Space Network ................................................264 Amateur Radio Satellites .............................................6 Delta Launch Vehicles .............................................271 Ames Research Center ...............................................12 Dynamics Explorers .................................................279 Ansari X Prize ............................................................19 Early-Warning Satellites ..........................................284 -
Should We Manage to a Single Data Point? a NASA/Goddard Space Flight Center Perspective
Goddard Space Flight Center Flight Projects Directorate Performance Management Should We Manage to a Single Data Point? A NASA/Goddard Space Flight Center Perspective Dr. Wanda Peters Deputy Director for Planning and Business Management 2019 Project Management Symposium Turning Knowledge into Practice University of Maryland May 10, 2019 Goddard Overview Project Management at Goddard Business Change Initiative Optimization State of Business Why is this Important? 2 Best Place to Work in the Federal Government 2018 3 Goddard Overview 4 Goddard Space Flight Center ONE World-Class Science and Engineering Organization SIX Distinctive Facilities & Installations Independent Greenbelt Wallops Flight White Sands Test Columbia Goddard Institute Validation & Main Campus Facility Facility Ground Balloon for Space Studies Verification 1,270 Acres 6,188 Acres Stations Facility Facility Executing NASA’s most Launching Payloads for Understanding our Providing Software Communicating with Directing High Altitude complex science missions NASA & the Nation Planet Assurance Assets in Earth’s Orbit Investigations Est. 1959 Est. 1945 Est. 1961 Est. 1993 Est. 1963 Est. 1982 MARYLAND VIRGINIA NEW YORK WEST VIRGINIA NEW MEXICO TEXAS 2 Who We Are THE GODDARD COMMUNITY Technicians and Others 6% Clerical 5% Professional & Administrative 28% Scientists & Engineers GSFC CS Employees 61% with Degrees Bachelors – 37% Advanced Degrees – 48% Associate/Technical – 2% Number of Employees High School – 13% A diverse community of scientists, engineers, ~3,000 Civil Service technologists, and administrative personnel ~6,000 Contractor dedicated to the exploration of space ~1,000 Other* Total - ~10,000 *Including off-site contractors, interns, and Emeritus The Nation’s largest community of scientists, engineers, and technologists Goddard Space Flight Center Employees Receive Worldwide Accolades for Their Work Dr. -
LCS Onepager
National Aeronautics and Space Administration NASA’s Launch communications segment: Advanced Communications Capabilities for the Florida Spaceport NASA Goddard Space Flight Center’s Near Earth Network Launch Communications Segment (LCS) consists of two modern ground stations designed to complement the U.S. Air Force’s Eastern Range, enabling next-generation space missions and launch vehicles departing from, or returning to, the Florida spaceport. The LCS stations provide the critical link between astronauts and mission controllers on crewed flights, and augment FEATURED launch vehicle telemetry and orbital tracking communications CAPABILITIES for robotic missions. LCS provides a broad array of communications services: • Pre-launch, launch, ascent and landing communications services • Agile, tailored and robust solutions for a variety of customer needs • Simultaneous transmitting and receiving via S-band • Support of IRIG and CCSDS space link standards, advanced modulation and encoding, and 2 Mbps data rates • Remote monitor and control for routine events and pre-mission testing • Common Space Link Extension (SLE) user gatewayIP baseband data interfaces • Orbital communications services to near-Earth users • Standard service scheduling through the Near Earth Network Scheduling Office • Antenna auto-tracking with automatic fail-over to Launch Trajectory Acquisition System (LTAS) or predicted vectors • Doppler and ranging capabilities Strategic Locations LCS consists of two strategically placed permanent ground stations: the Kennedy Uplink Station on site at NASA’s Kennedy Space Center (KSC) and the Ponce de Leon Station 40 miles north in New Smyrna Beach, Florida. Each of these sites has a 6.1-meter antenna capable of simultaneously transmitting and receiving S-band signals. The two-site architecture ensures continuous signal coverage during launch, as well as for vehicles returning to the launch site or the Shuttle Landing Facility. -
Scan-MOCS-0001
SCaN-MOCS-0001 SPACE COMMUNICATIONS AND NAVIGATION PROGRAM Space Communications and Navigation (SCaN) Mission Operations and Communications Services (MOCS) Revision 2 Effective Date: March 15, 2019 Expiration Date: March 15, 2024 National Aeronautics and NASA Headquarters Space Administration Washington, D. C. CHECK THE SCaN NEXT GENERATION INTEGRATED NETWORK (NGIN) AT: https://scanngin.gsfc.nasa.gov TO VERIFY THAT THIS IS THE CORRECT VERSION PRIOR TO USE. Space Communications and Navigation (SCaN) Mission Operations and Communications Services (MOCS) Effective Date: March 15, 2019 Approved and Prepared by: John J. Hudiburg 3/15/19 J ohn J. Hudiburg Date Mission Integration and Commitment Manager, SCaN Network Services Division Human Exploration and Operations Mission Directorate NASA Headquarters Washington, D. C. SCaN-MOCS-0001 Revision 2 Preface This document is under configuration management of the SCaN Integrated Network Configuration Control Board (SINCCB). This document will be changed by Documentation Change Notice (DCN) or complete revision. Proposed changes to this document must be submitted to the SCaN Configuration Management Office along with supportive material justifying the proposed change. Comments or questions concerning this document and proposed changes shall be addressed to: Configuration Management Office [email protected] Space Communications and Navigation Office NASA Headquarters Washington, D. C. ii SCaN-MOCS-0001 Revision 2 Change Information Page List of Effective Pages Page Number Issue Title Rev 2 iii -
The Decade of Light: Innovations in Space Communications and Navigation Technologies
Journal of Space Operations & Communicator (ISSN 2410-0005) Vol. 16, No. 1, Year 2019 The Decade of Light: Innovations in Space Communications and Navigation Technologies Philip Liebrecht Donald Cornwell David Israel Gregory Heckler NASA Headquarters NASA Headquarters Goddard Space Flight Center NASA Headquarters 300 E Street SW 300 E Street SW 8800 Greenbelt Road 300 E Street SW Washington, D.C Washington, D.C. Greenbelt, Md. 20771 Washington, D.C. 202-358-1701 202-358-0570 301-286-5294 202-358-1626 [email protected] [email protected] [email protected] [email protected] INTRODUCTION NASA’s Space Communications and Navigation (SCaN) program office’s vision of a fully interoperable network of space communications assets is known as the Decade of Light. Through relentless advancement of current technologies, NASA is progressing toward a future of seamless mission enabling space communications and navigation. This futuristic, interoperable system will include the development of optical communications, wideband Ka-band, hybrid optical and radio frequency (RF) antennas, user- initiated services (UIS), a cognitive network with disruption-tolerant networking (DTN) capabilities and autonomous navigation. This vision, although vastly complex, will introduce dramatic increases in performance and is already being worked at NASA Headquarters, NASA’s Goddard Space Flight Center, NASA’s Glenn Research Center, and Jet Propulsion Laboratory. Teams from around the country continue to investigate and strive for innovative solutions to the many complex challenges space communications and navigation faces. CURRENT CAPABILITIES For the past 50 years, NASA has primarily used RF to communicate mission data from satellites orbiting in our solar system to data users on Earth. -
The Deep Space Network: a Functional Description
Chapter 2 The Deep Space Network: A Functional Description Jim Taylor All deep-space missions—defined as those operating at or beyond the orbit of the Earth’s Moon—require some form of telecommunications network with a ground system to transmit to and receive data from the spacecraft. The Deep Space Network or DSN is one of the largest and most sophisticated of such networks. NASA missions in low Earth orbit communicate through either the Near Earth Network (NEN) or the SN (Space Network), with the SN, both operated by the NASA Goddard Space Flight Center (GSFC). The SN has of a number of Tracking and Data Relay Satellites (TDRS) in geosynchronous orbits. In addition, the European Space Agency operates a number of ground stations that may be used to track NASA deep space missions during the hours after launch. In addition, commercial companies operate ground stations that can communicate with NASA missions. The remainder of this book describes only the Deep Space Network operated for NASA by JPL. The lessons and techniques of the DSN replicate many comparable issues of the other networks. The lessons from the missions described in the following chapters are widely applicable to all deep space telecommunications systems. This includes post-launch support that was negotiated and planned using stations belonging to networks other than the DSN. The description and performance summary of the DSN in this chapter come from the DSN Telecommunications Link Design Handbook, widely known 15 16 Chapter 2 within NASA as the 810-5 document [1]. This modular handbook has been approved by the DSN Project Office, and its modules are updated to define current DSN capabilities. -
The Orion Spacecraft As a Key Element in a Deep Space Gateway
The Orion Spacecraft as a Key Element in a Deep Space Gateway A Technical Paper Presented by: Timothy Cichan Lockheed Martin Space [email protected] Kerry Timmons Lockheed Martin Space [email protected] Kathleen Coderre Lockheed Martin Space [email protected] Willian D. Pratt Lockheed Martin Space [email protected] July 2017 © 2014 Lockheed Martin Corporation Abstract With the Orion exploration vehicle and Space Launch System (SLS) approaching operational status, NASA and the international community are developing the next generation of habitats to serve as a deep space platform that will be the first of its kind, a cislunar Deep Space Gateway (DSG). The DSG is evolvable, flexible, and modular. It would be positioned in the vicinity of the Moon and allow astronauts to demonstrate they can operate for months at a time well beyond Low Earth Orbit. Orion is the next generation human exploration spacecraft being developed by NASA. It is designed to perform deep space exploration missions, and is capable of carrying a crew of 4 astronauts on independent free-flight missions up to 21 days, limited only by consumables. Because Orion meets the strict requirements for deep space flight environments (reentry conditions, deep-space communications, safety, radiation, and life support for example) it is a key element in a DSG and is more than just a transportation system. Orion has the capability to act as the command deck of any deep space piloted vehicle. To increase affordability and reduce the complexity and number of subsystem functions the early DSG must be responsible for, the DSG can leverage these unique deep space qualifications of Orion.