COUNTING DOWN TO THE LAUNCH OF POPACS

Size: px
Start display at page:

Download "COUNTING DOWN TO THE LAUNCH OF POPACS"

Transcription

1 COUNTING DOWN TO THE LAUNCH OF POPACS (Polar Orbiting Passive Atmospheric Calibration Spheres) Gil Moore Utah State University Walter Holemans Planetary Systems Corporation Jin Kang U.S. Naval Academy

2 A project to measure the effects of solar flares and coronal mass ejections on the density of Earth s upper atmosphere during Solar Cycles 24 and 25

3 Program Status Six 10-cm-diameter hollow spheres have been machined from 6061-T6 Aluminum These spheres have been filled with sand and Bismuth shot to make them weigh 1 kg, 1.5 kg and 2 kg, respectively

4 The spheres have been welded shut, three of them have been coated with space-proven AZ-93 flat white paint, and three have been polished Four lightweight Aluminum spacers have been designed by Drexel University to support the spheres during launch into orbit

5 Planetary Systems Corporation has provided one of its newly developed 3U Canisterized Satellite Dispensers (CSDs) to support this 6 kg payload during launch and deploy it into orbit Utah State University has purchased a 3U CubeSat slot on a SpaceX Falcon 9 that will be launched from Vandenberg AFB during Solar Maximum 24

6 The spheres and spacers will be deployed from the CSD aboard the Falcon 9 into an initial 325 km x 1500 km orbit, inclined 80 degrees to the earth s equator, with a 104 minute period The lightweight, high-drag spacers will de-orbit, due to atmospheric drag at perigee, and be consumed within a few months, while the much more dense spheres will orbit for approximately 10, 12.5 and 15 years, before de-orbiting and being consumed

7

8 Each sphere will be tracked by the Space Surveillance Network (SSN) Phased Array radars and GEODS optical sites of the U.S. Strategic Command s Joint Space Operations Center (JSPOC),

9

10 Atmospheric drag at perigee will cause the spheres orbits to decay at different rates, due to their different masses and, thus, their ballistic coefficients The JSPOC will periodically publish Two Line Element sets (TLEs), similar to those below, that define each sphere s orbital elements at the start of a given epoch U 98067A

11 An international network of amateur and university observers who own Go-To telescopes with built-in GPS receivers, computers and drives will use those TLEs to track the spheres during visible passes over their individual locations Using digital recorders attached to their telescopes, the observers will record frames of each sphere s position at a given moment within the background stars. They will then use a digitized star catalog and pattern recognition software to measure the sphere s right ascension and declination at the precise time of the observation.

12

13 The optical observers will use the Internet to share their measurements of sphere right ascension, declination and time, plus longitude, latitude and altitude of their own site, with other observers all over the world. They will then calculate each sphere s orbit, using the angles-only method of LaPlace or the Gooding method, and compute their own TLEs As the spheres orbits shrink, over time, due to atmospheric drag, the observers will be able to compute the density of the earth s upper atmosphere at the altitude, latitude and longitude of each sphere s perigee pass, using software provided to the POPACS project by Analytical Graphics, Inc. They will measure the global variations in Earth s upper atmospheric density before, during and after the occurrence of solar flares and coronal mass ejections

14 The optical teams will forecast atmospheric density variability in response to future solar stimuli during Solar Cycles 24 and 25 and compare their results with solar- terrestrial scientists of the U.S. Naval Research Laboratory (NRL), who use TLEs from thousands of satellites and an efficient fast algorithm to construct a database of atmospheric density The POPACS project will award periodic prizes to the individual observers whose sphere right ascension and declination measurements consistently come closest to those provided by the AFSPC using reference orbits derived from their radar and GEODS optical sites

15 The authors would like to thank the student team at Drexel University, Dr. T.S. Kelso and Wes Bradley of Analytical Graphics, Inc., Bruce Bowman of the Air Force Space Command, Dr. Judith Lean of the Naval Research Laboratory, Machine of Colorado Springs, CO, Petersen, Inc. of Ogden, UT, Dr. Jan Sojka and Joseph Jenkins of Utah State University, Dr. Alan Thurgood of the Space Dynamics Laboratory and Dustin Doud of SpaceX for helping us get this project started. If you have constructive suggestions for this work in progress and/or would like to become an observer, please contact Gil Moore, POPACS Project Director at or (cell)

COUNTING DOWN TO THE LAUNCH OF POPACS (POLAR ORBITING PASSIVE ATMOSPHERIC CALIBRATION SPHERES)

COUNTING DOWN TO THE LAUNCH OF POPACS (POLAR ORBITING PASSIVE ATMOSPHERIC CALIBRATION SPHERES) SSC12-X-3 COUNTING DOWN TO THE LAUNCH OF POPACS (POLAR ORBITING PASSIVE ATMOSPHERIC CALIBRATION SPHERES) Walter Holemans Planetary Systems Corporation 2303 Kansas Ave., Silver Spring, MD; 301-495-0737;

More information

How CubeSats are Helping Address the Space Debris Problem: Results from the Polar Orbiting Passive Atmospheric Calibration Spheres

How CubeSats are Helping Address the Space Debris Problem: Results from the Polar Orbiting Passive Atmospheric Calibration Spheres How CubeSats are Helping Address the Space Debris Problem: Results from the Polar Orbiting Passive Atmospheric Calibration Spheres 13th Annual Summer CubeSat Developers' Workshop Logan, UT 5/26/2016 Marcin

More information

Spacer Development and Analysis

Spacer Development and Analysis Spacer Development and Analysis Mission Overview POPACS MISSION To measure changes in the density of the auroral zone upper atmosphere in response to various solar stimuli DREXEL OBJECTIVE To design and

More information

UPPER ATMOSPHERIC DENSITIES DERIVED FROM STARSHINE SPACECRAFT ORBITS

UPPER ATMOSPHERIC DENSITIES DERIVED FROM STARSHINE SPACECRAFT ORBITS UPPER ATMOSPHERIC DENSITIES DERIVED FROM STARSHINE SPACECRAFT ORBITS R. G. Moore 1, J. Lean 2, J. M. Picone 2, S. Knowles, A. Hedin 2, and J. Emmert 2 1. 855 Sierra Vista Road, Monument CO 8012 2. Naval

More information

PW-Sat two years on orbit.

PW-Sat two years on orbit. 13th of February 2014 is the second anniversary of launch of the first polish student-made satellite PW-Sat. Currently Students' Space Association on Warsaw University of Technology is working on another

More information

What Happened to BLITS? An Analysis of the 2013 Jan 22 Event

What Happened to BLITS? An Analysis of the 2013 Jan 22 Event What Happened to BLITS? An Analysis of the 2013 Jan 22 Event T.S. Kelso Center for Space Standards & Innovation N.N. Parkhomenko, V.D. Shargorodsky, V.P. Vasiliev, V.S. Yurasov Open Joint-Stock Company

More information

J. G. Miller (The MITRE Corporation), W. G. Schick (ITT Industries, Systems Division)

J. G. Miller (The MITRE Corporation), W. G. Schick (ITT Industries, Systems Division) Contributions of the GEODSS System to Catalog Maintenance J. G. Miller (The MITRE Corporation), W. G. Schick (ITT Industries, Systems Division) The Electronic Systems Center completed the Ground-based

More information

Absolute Radiometric Calibration Using a Solar Reflector in Near-Geosynchronous Orbit

Absolute Radiometric Calibration Using a Solar Reflector in Near-Geosynchronous Orbit Absolute Radiometric Calibration Using a Solar Reflector in Near-Geosynchronous Orbit Richard J. Rudy, Ray W. Russell, Dan J. Mabry, Andrea M. Gilbert, Paul V. Anderson, David J. Gutierrez (The Aerospace

More information

Final Examination 2015

Final Examination 2015 THE UNIVERSITY OF SYDNEY School of Aerospace, Mechanical and Mechatronic Engineering AERO 2705: Space Engineering 1 Final Examination 2015 READ THESE INSTRUCTIONS CAREFULLY! Answer at least 4 (four of

More information

Toshinori Kuwahara*, Yoshihiro Tomioka, Yuta Tanabe, Masato Fukuyama, Yuji Sakamoto, Kazuya Yoshida, Tohoku University, Japan

Toshinori Kuwahara*, Yoshihiro Tomioka, Yuta Tanabe, Masato Fukuyama, Yuji Sakamoto, Kazuya Yoshida, Tohoku University, Japan Toshinori Kuwahara*, Yoshihiro Tomioka, Yuta Tanabe, Masato Fukuyama, Yuji Sakamoto, Kazuya Yoshida, Tohoku University, Japan The 3 rd Nano-Satellite Symposium Micro/Nano Satellite & Debris Issues December

More information

Geometry of Earth Sun System

Geometry of Earth Sun System 12S56 Geometry of Earth Sun System Figure below shows the basic geometry Northern Hemisphere Winter ω equator Earth s Orbit Ecliptic ω ω SUN equator Northern Hemisphere Spring Northern Hemisphere Fall

More information

Orbit Design Marcelo Suárez. 6th Science Meeting; Seattle, WA, USA July 2010

Orbit Design Marcelo Suárez. 6th Science Meeting; Seattle, WA, USA July 2010 Orbit Design Marcelo Suárez Orbit Design Requirements The following Science Requirements provided drivers for Orbit Design: Global Coverage: the entire extent (100%) of the ice-free ocean surface to at

More information

SLR-based orbit determination and orbit prediction of space debris objects

SLR-based orbit determination and orbit prediction of space debris objects Geodätische Woche Congress Center Essen, 8.- 10. Oktober 2013 SLR-based orbit determination and orbit prediction of space debris objects Harald Wirnsberger, Oliver Baur, Georg Kirchner Space Research Institute

More information

Make Your Cubesat Overnight and Put it in Any Orbit (Well almost)

Make Your Cubesat Overnight and Put it in Any Orbit (Well almost) Make Your Cubesat Overnight and Put it in Any Orbit (Well almost) Jim White, Walter Holemans, Planetary Systems Inc. Dr. Adam Huang, University of Arkansas RAMPART Summary Main Components The Promise of

More information

Lunar Water Distribution (LWaDi)-- a 6U Lunar Orbiting spacecraft SSC14-WK-22

Lunar Water Distribution (LWaDi)-- a 6U Lunar Orbiting spacecraft SSC14-WK-22 Lunar Water -- a 6U Lunar Orbiting spacecraft SSC14-WK-22 Pamela Clark, PhD, Planetary Scientist, NASA GSFC and Catholic University Walter Holemans, Chief Engineer, PSC (Presenting) Wes Bradley, President,

More information

Leonid Meteor Observer in LEO: A Proposal for a University Microsatellite for the 2001 Leonids

Leonid Meteor Observer in LEO: A Proposal for a University Microsatellite for the 2001 Leonids Leonid Meteor Observer in LEO: A Proposal for a University Microsatellite for the 2001 Leonids Kazuya Yoshida* Hajime Yano** *Tohoku University **Institute of Space and Astronautical Science (ISAS) JAPAN

More information

Results and Analyses of Debris Tracking from Mt Stromlo

Results and Analyses of Debris Tracking from Mt Stromlo Results and Analyses of Debris Tracking from Mt Stromlo Jizhang Sang 1, Ian Ritchie, Matt Pearson, and Craig Smith EOS Space Systems Pty Ltd, Australia Abstract In the last 2 years, EOS Space Systems has

More information

ACCURACY ASSESSMENT OF GEOSTATIONARY-EARTH-ORBIT WITH SIMPLIFIED PERTURBATIONS MODELS

ACCURACY ASSESSMENT OF GEOSTATIONARY-EARTH-ORBIT WITH SIMPLIFIED PERTURBATIONS MODELS ARTIFICIAL SATELLITES, Vol. 51, No. 2 2016 DOI: 10.1515/arsa-2016-0005 ACCURACY ASSESSMENT OF GEOSTATIONARY-EARTH-ORBIT WITH SIMPLIFIED PERTURBATIONS MODELS Lihua Ma, Xiaojun Xu, Feng Pang National Astronomical

More information

Satellite communications and the environment of space. V 1.1 Swiss Space Summer Camp 2016 Images: NASA 1

Satellite communications and the environment of space. V 1.1 Swiss Space Summer Camp 2016 Images: NASA 1 Satellite communications and the environment of space Swiss Space Summer Camp 2016 Images: NASA 1 Can you name these satellites? Sputnik The first man made satellite Launched in 1957 by The USSR Mass 84kg,

More information

Results from the Atmospheric Neutral Density Experiment Risk Reduction Mission

Results from the Atmospheric Neutral Density Experiment Risk Reduction Mission Results from the Atmospheric Neutral Risk Reduction Mission A.C. Nicholas, S.A. Budzien, J. DeYoung, L. Healy Naval Research Laboratory M. Davis Honeywell TSI Outline Mission Description C D Modeling Data

More information

Operations, Orbit Determination, and Formation Control of the AeroCube-4 CubeSats

Operations, Orbit Determination, and Formation Control of the AeroCube-4 CubeSats SSC-X- Operations, Orbit Determination, and Formation Control of the AeroCube- CubeSats Joseph W. Gangestad, Brian S. Hardy, and David A. Hinkley The Aerospace Corporation E. El Segundo Blvd, El Segundo,

More information

PRELIMINARY RESULTS TO SUPPORT EVIDENCE OF THERMOSPHERIC CONTRACTION

PRELIMINARY RESULTS TO SUPPORT EVIDENCE OF THERMOSPHERIC CONTRACTION PRELIMINARY RESULTS TO SUPPORT EVIDENCE OF THERMOSPHERIC CONTRACTION Arrun Saunders, Graham G. Swinerd, Hugh G. Lewis School of Engineering Sciences University of Southampton, Highfield, Southampton, SO17

More information

Modern Navigation. Thomas Herring

Modern Navigation. Thomas Herring 12.215 Modern Navigation Thomas Herring Review of Monday s Class Spherical Trigonometry Review plane trigonometry Concepts in Spherical Trigonometry Distance measures Azimuths and bearings Basic formulas:

More information

MAE 180A: Spacecraft Guidance I, Summer 2009 Homework 2 Due Tuesday, July 14, in class.

MAE 180A: Spacecraft Guidance I, Summer 2009 Homework 2 Due Tuesday, July 14, in class. MAE 180A: Spacecraft Guidance I, Summer 2009 Homework 2 Due Tuesday, July 14, in class. Guidelines: Please turn in a neat and clean homework that gives all the formulae that you have used as well as details

More information

Figure 1. View of ALSAT-2A spacecraft

Figure 1. View of ALSAT-2A spacecraft ALSAT-2A TRANSFER AND FIRST YEAR OPERATIONS M. Kameche (1), A.H. Gicquel (2), D. Joalland (3) (1) CTS/ASAL, 1 Avenue de la Palestine, BP 13, Arzew 31200 Oran, Algérie, email:mo_kameche@netcourrier.com

More information

Stephen H. Knowles Integrity Applications, Inc. Chantilly, VA apps.com

Stephen H. Knowles Integrity Applications, Inc. Chantilly, VA apps.com Long Term Behavior of the Thermosphere Determined from Satellite Drag Measurements Stephen H. Knowles Integrity Applications, Inc. Chantilly, VA sknowles@integrity- apps.com Abstract Archived satellite

More information

Atmospheric density calibration using satellite drag observations

Atmospheric density calibration using satellite drag observations Atmospheric density calibration using satellite drag observations Eelco Doornbos (TU Delft) Heiner Klinkrad (ESA/ESOC) Second European Space Weather Week Tuesday, 15 November, 2005 Outline Applications

More information

PERFORMANCES OF ATMOSPHERIC DENSITY MODELS DURING SATELLITE REENTRY PREDICTION CAMPAIGNS AT SUNSPOT MINIMUM

PERFORMANCES OF ATMOSPHERIC DENSITY MODELS DURING SATELLITE REENTRY PREDICTION CAMPAIGNS AT SUNSPOT MINIMUM PERFORMANCES OF ATMOSPHERIC DENSITY MODELS DURING SATELLITE REENTRY PREDICTION CAMPAIGNS AT SUNSPOT MINIMUM Carmen Pardini (1), Luciano Anselmo (2) Space Flight Dynamics Laboratory, ISTI/CNR, Via G. Moruzzi

More information

These notes may contain copyrighted material! They are for your own use only during this course.

These notes may contain copyrighted material! They are for your own use only during this course. Licensed for Personal Use Only DO NOT DISTRIBUTE These notes may contain copyrighted material! They are for your own use only during this course. Distributing them in anyway will be considered a breach

More information

Overview of JAXA Activities on Sustainable Space Development and Space Situational Awareness

Overview of JAXA Activities on Sustainable Space Development and Space Situational Awareness Overview of JAXA Activities on Sustainable Space Development and Space Situational Awareness 26 February 2015 Shizuo YAMAMOTO Vice President, JAXA CONTENTS 1. Japan s Space Activities Structure 2. JAXA

More information

Operational Impacts of Space Weather

Operational Impacts of Space Weather Operational Impacts of Space Weather R. Lambour, A. J. Coster, R. Clouser, L. E. Thornton, J. Sharma, and A. Cott 2001 Space Control Conference 3 April 2001 2001 Space Control Conf. -1 Outline Introduction

More information

INTEROPERABILITY AND STANDARDS ACROSS THE ENTIRE SPACE ENTERPRISE. GSAW 2007 Manhattan Beach, CA March 2007

INTEROPERABILITY AND STANDARDS ACROSS THE ENTIRE SPACE ENTERPRISE. GSAW 2007 Manhattan Beach, CA March 2007 INTEROPERABILITY AND STANDARDS ACROSS THE ENTIRE SPACE ENTERPRISE. GSAW 2007 Manhattan Beach, CA 26-29 March 2007 DAVID FINKLEMAN, CENTER FOR SPACE STANDARDS AND INNOVATION ANALYTICAL GRAPHICS INC. Pg

More information

Lecture 8. October 25, 2017 Lab 5

Lecture 8. October 25, 2017 Lab 5 Lecture 8 October 25, 2017 Lab 5 News Lab 2 & 3 Handed back next week (I hope). Lab 4 Due today Lab 5 (Transiting Exoplanets) Handed out and observing will start Friday. Due November 8 (or later) Stellar

More information

Propagation of Forecast Errors from the Sun to LEO Trajectories: How Does Drag Uncertainty Affect Conjunction Frequency?

Propagation of Forecast Errors from the Sun to LEO Trajectories: How Does Drag Uncertainty Affect Conjunction Frequency? Propagation of Forecast Errors from the Sun to LEO Trajectories: How Does Drag Uncertainty Affect Conjunction Frequency? John Emmert, Jeff Byers, Harry Warren, and Alan Segerman Naval Research Laboratory

More information

Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts

Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts. Chandra Fun Facts What Space Shuttle was launched aboard? was launched aboard Space Shuttle Columbia on July 23, 1999 from the Kennedy Space Center in Florida. How high does orbit? flies more than 1/3 of the way to the

More information

The Characteristics and Consequences of the Break-up of the Fengyun-1C Spacecraft

The Characteristics and Consequences of the Break-up of the Fengyun-1C Spacecraft The Characteristics and Consequences of the Break-up of the Fengyun-1C Spacecraft N. Johnson, E. Stansbery, J.-C. Liou, M. Horstman, C. Stokely, D. Whitlock NASA Orbital Debris Program Office NASA Johnson

More information

PROBA 1. F. Teston ESA/ESTEC D/TEC-EL

PROBA 1. F. Teston ESA/ESTEC D/TEC-EL PROBA 1 F. Teston ESA/ESTEC D/TEC-EL Frederic.Teston@esa.int PROBA 1 launch PROBA 1 has been launched on 21 October 2001 Orbital parameters: Altitude: 681-561 km Near polar (inclination of 97.9 ) Sun-synchronous

More information

Major fragmentation of Atlas 5 Centaur upper stage B (SSN #40209)

Major fragmentation of Atlas 5 Centaur upper stage B (SSN #40209) Major fragmentation of Atlas 5 Centaur upper stage 2014 055B (SSN #40209) Vladimir Agapov IAA Space Debris Committee meeting Bremen, 29 Sep 2018 Outline Atlas 5 Centaur overview 30 Aug 2018 anomaly in

More information

1 2 3 US Air Force 557 th Weather Wing maintains a website with many operational products both on terrestrial as on space weather. The operational holy grail for the military are stoplight charts, indicating

More information

Theoretical Test Astronomy Time: 45 Minutes Maximum Marks: 28.5

Theoretical Test Astronomy Time: 45 Minutes Maximum Marks: 28.5 Theoretical Test Astronomy Time: 45 Minutes Maximum Marks: 28.5 Instructions: 1. Please write your student code on the cover page as well as on the top right of every page of answer sheet / calculations

More information

Chapter S1 Lecture. The Cosmic Perspective Seventh Edition. Celestial Timekeeping and Navigation Pearson Education, Inc.

Chapter S1 Lecture. The Cosmic Perspective Seventh Edition. Celestial Timekeeping and Navigation Pearson Education, Inc. Chapter S1 Lecture The Cosmic Perspective Seventh Edition Celestial Timekeeping and Navigation 2014 Pearson Education, Inc. Celestial Timekeeping and Navigation 2014 Pearson Education, Inc. S1.1 Astronomical

More information

Research Article The Impact on Geographic Location Accuracy due to Different Satellite Orbit Ephemerides

Research Article The Impact on Geographic Location Accuracy due to Different Satellite Orbit Ephemerides Mathematical Problems in Engineering Volume 2009, Article ID 856138, 9 pages doi:10.1155/2009/856138 Research Article The Impact on Geographic Location Accuracy due to Different Satellite Orbit Ephemerides

More information

Accuracy Assessment of SGP4 Orbit Information Conversion into Osculating Elements

Accuracy Assessment of SGP4 Orbit Information Conversion into Osculating Elements Accuracy Assessment of SGP4 Orbit Information Conversion into Osculating Elements Saika Aida (1), Michael Kirschner (2) (1) DLR German Space Operations Center (GSOC), Oberpfaffenhofen, 82234 Weßling, Germany,

More information

Name Class Date. For each pair of terms, explain how the meanings of the terms differ.

Name Class Date. For each pair of terms, explain how the meanings of the terms differ. Skills Worksheet Chapter Review USING KEY TERMS 1. Use each of the following terms in a separate sentence: year, month, day, astronomy, electromagnetic spectrum, constellation, and altitude. For each pair

More information

Chapter S1 Celestial Timekeeping and Navigation. How do we define the day, month, year, and planetary time periods?

Chapter S1 Celestial Timekeeping and Navigation. How do we define the day, month, year, and planetary time periods? Chapter S1 Celestial Timekeeping and Navigation S1.1 Astronomical Time Periods Our goals for learning:! How do we define the day, month, year, and planetary time periods?! How do we tell the time of day?!

More information

Introduction to Satellite Orbits

Introduction to Satellite Orbits Introduction to Satellite Orbits Dinesh Manandhar Center for Spatial Information Science The University of Tokyo Contact Information: dinesh@iis.u-tokyo.ac.jp Slide : 1 Basics of Satellite Orbits The speed

More information

Development of the Space Debris Sensor (SDS) Joe Hamilton SDS Principal Investigator January

Development of the Space Debris Sensor (SDS) Joe Hamilton SDS Principal Investigator January Development of the Space Debris Sensor (SDS) Joe Hamilton SDS Principal Investigator January 31. 2017 Outline Background Orbital Debris Measurement Coverage What is SDS? Detection Principles Example 0.4

More information

LOCATING CELESTIAL OBJECTS: COORDINATES AND TIME. a. understand the basic concepts needed for any astronomical coordinate system.

LOCATING CELESTIAL OBJECTS: COORDINATES AND TIME. a. understand the basic concepts needed for any astronomical coordinate system. UNIT 2 UNIT 2 LOCATING CELESTIAL OBJECTS: COORDINATES AND TIME Goals After mastery of this unit, you should: a. understand the basic concepts needed for any astronomical coordinate system. b. understand

More information

A SYSTEMATIC EXAMINATION OF GROUND-BASED AND SPACE-BASED APPROACHES TO OPTICAL DETECTION AND TRACKING OF SATELLITES

A SYSTEMATIC EXAMINATION OF GROUND-BASED AND SPACE-BASED APPROACHES TO OPTICAL DETECTION AND TRACKING OF SATELLITES 31 st Space Symposium - Technical Track April 14 th, 2015 A SYSTEMATIC EXAMINATION OF GROUND-BASED AND SPACE-BASED APPROACHES TO OPTICAL DETECTION AND TRACKING OF SATELLITES Mark R. Ackermann, Sandia Labs

More information

Kepler: A Search for Terrestrial Planets

Kepler: A Search for Terrestrial Planets Kepler: A Search for Terrestrial Planets Stellar Classification Program Plan NASA Ames Research Center Moffett Field, CA. 94035 Warning! This printed copy may not be the latest released version. It is

More information

AIR FORCE INSTITUTE OF TECHNOLOGY

AIR FORCE INSTITUTE OF TECHNOLOGY INVESTIGATING ANALYTICAL AND NUMERICAL METHODS TO PREDICT SATELLITE ORBITS USING TWO-LINE ELEMENT SETS THESIS Adam T. Rich, Captain, USAF AFIT-ENY-MS-17-M-286 DEPARTMENT OF THE AIR FORCE AIR UNIVERSITY

More information

Overview of the SORCE Mission

Overview of the SORCE Mission Overview of the SORCE Mission LASP University of Colorado 1 The SORCE mission is one element of NASA s Earth Science Enterprise. Primary science objective of SORCE is: measurement of solar irradiance both

More information

MODELLING OF PERTURBATIONS FOR PRECISE ORBIT DETERMINATION

MODELLING OF PERTURBATIONS FOR PRECISE ORBIT DETERMINATION MODELLING OF PERTURBATIONS FOR PRECISE ORBIT DETERMINATION 1 SHEN YU JUN, 2 TAN YAN QUAN, 3 TAN GUOXIAN 1,2,3 Raffles Science Institute, Raffles Institution, 1 Raffles Institution Lane, Singapore E-mail:

More information

Theoretical Test Astronomy Time: 45 Minutes Maximum Marks: 28.5

Theoretical Test Astronomy Time: 45 Minutes Maximum Marks: 28.5 Theoretical Test Astronomy Time: 45 Minutes Maximum Marks: 28.5 Instructions: 1. Please write your student code on the cover page as well as on the top right of every page of answer sheet / calculations

More information

The Space-based Telescopes for Actionable Refinement of Ephemeris (STARE) mission

The Space-based Telescopes for Actionable Refinement of Ephemeris (STARE) mission LLNL-PRES-641541 Performance Measures x.x, x.x, and x.x SSC13-XI-11 The Space-based Telescopes for Actionable Refinement of Ephemeris (STARE) mission Vincent Riot, Willem de Vries, Lance Simms, Brian Bauman,

More information

Phoenix Upgrades in Support of Real-time Space Object Capture and Handoff at AMOS

Phoenix Upgrades in Support of Real-time Space Object Capture and Handoff at AMOS Phoenix Upgrades in Support of Real-time Space Object Capture and Handoff at AMOS Bryan Law, Dennis Liang, Tom Kelecy, Andrew Alday, Jake Barros, Paul Sydney, and John Africano Air Force Maui Optical and

More information

STUDY THE SPACE DEBRIS IMPACT IN THE EARLY STAGES OF THE NANO-SATELLITE DESIGN

STUDY THE SPACE DEBRIS IMPACT IN THE EARLY STAGES OF THE NANO-SATELLITE DESIGN ARTIFICIAL SATELLITES, Vol. 51, No. 4 2016 DOI: 10.1515/arsa-2016-0014 STUDY THE SPACE DEBRIS IMPACT IN THE EARLY STAGES OF THE NANO-SATELLITE DESIGN Mohammed Chessab Mahdi Al-Furat Al-Awsat Technical

More information

ASEN 6008: Interplanetary Mission Design Lab Spring, 2015

ASEN 6008: Interplanetary Mission Design Lab Spring, 2015 ASEN 6008: Interplanetary Mission Design Lab Spring, 2015 Lab 4: Targeting Mars using the B-Plane Name: I d like to give credit to Scott Mitchell who developed this lab exercise. He is the lead Astrodynamicist

More information

Improvement of Orbits of Geostationary Satellites from Observations Over a Time Interval of Days

Improvement of Orbits of Geostationary Satellites from Observations Over a Time Interval of Days Improvement of Orbits of Geostationary Satellites from Observations Over a Time Interval of 15-2 Days * Konstantin V.Grigoriev, ** Felix R. Hoots * Pulkovo Observatory, St-Petersburg, Russia ** GRC International,

More information

Larger Optics and Improved Calibration Techniques for Small Satellite Observations with the ERAU OSCOM System

Larger Optics and Improved Calibration Techniques for Small Satellite Observations with the ERAU OSCOM System Larger Optics and Improved Calibration Techniques for Small Satellite Observations with the ERAU OSCOM System Sergei Bilardi 1, Aroh Barjatya 1, Forrest Gasdia 2 1 Space and Atmospheric Instrumentation

More information

Coordinates on the Sphere

Coordinates on the Sphere Survey Observations Coordinates on the Sphere Any position on the surface of a sphere (such as the Earth or the night sky) can be expressed in terms of the angular coordinates latitude and longitude Latitude

More information

Coordinate Systems for Astronomy or: How to get your telescope to observe the right object

Coordinate Systems for Astronomy or: How to get your telescope to observe the right object Coordinate Systems for Astronomy or: How to get your telescope to observe the right object Figure 1: Basic definitions for the Earth Definitions - Poles, Equator, Meridians, Parallels The rotation of the

More information

Satellite Communications

Satellite Communications Satellite Communications Lecture (3) Chapter 2.1 1 Gravitational Force Newton s 2nd Law: r r F = m a Newton s Law Of Universal Gravitation (assuming point masses or spheres): Putting these together: r

More information

Identifying Satellite Launch Origins with Historical Examples Michael E. Stringer Bob Teets Robin Thurston ξ

Identifying Satellite Launch Origins with Historical Examples Michael E. Stringer Bob Teets Robin Thurston ξ INTRODUCTION Identifying Satellite Launch Origins with Historical Examples Michael E. Stringer Bob Teets Robin Thurston ξ The 1 st Command and Control Squadron s (1 CACS) mission is to maintain the most

More information

Orbital Debris Observation via Laser Illuminated Optical Measurement Techniques

Orbital Debris Observation via Laser Illuminated Optical Measurement Techniques Orbital Debris Observation via Laser Illuminated Optical Measurement Techniques Makoto TAGAWA Kyushu University Toshiya HANADA Kyushu University Kozue HASHIMOTO, Yukihito KITAZAWA, Aritsune KAWABE IHI

More information

SOLAR ORBITER Linking the Sun and Inner Heliosphere. Daniel Müller

SOLAR ORBITER Linking the Sun and Inner Heliosphere. Daniel Müller SOLAR ORBITER Linking the Sun and Inner Heliosphere Outline Science goals of Solar Orbiter Focus of HELEX joint mission Mission requirements Science payload Status update Top level scientific goals of

More information

10/17/2012. Observing the Sky. Lecture 8. Chapter 2 Opener

10/17/2012. Observing the Sky. Lecture 8. Chapter 2 Opener Observing the Sky Lecture 8 Chapter 2 Opener 1 Figure 2.1 Figure 2.2 2 Figure 2.6 Figure 2.4 Annotated 3 The Celestial Sphere The celestial sphere is the vast hollow sphere on which the stars appear fixed.

More information

New Observation Results from A Rotating-drift-scan CCD System

New Observation Results from A Rotating-drift-scan CCD System New Observation Results from A Rotating-drift-scan CCD System TANG Zheng-Hong, MAO Yin-Dun, LI Yan, YU Yong Shanghai Astronomical Observatory, Chinese Academy of Sciences Abstract: A Rotating-drift-scan

More information

An Optical Survey for Space Debris on Highly Eccentric MEO Orbits

An Optical Survey for Space Debris on Highly Eccentric MEO Orbits An Optical Survey for Space Debris on Highly Eccentric MEO Orbits T. Schildknecht 1), A. Hinze 1), A. Vananti 1), T. Flohrer ) 1) Astronomical Institute, University of Bern, Sidlerstr. 5, CH-31 Bern, Switzerland

More information

Astrophysics/Astronomy Problems

Astrophysics/Astronomy Problems Astrophysics/Astronomy Problems Every question counts as a single point, except starred problems (*) which count as 2 points. Double starred problems (**) also count as 2 points, and will be used to decide

More information

PAYLOAD ORBITAL DELIVERY SYSTEM (PODS) The Payload Orbital Delivery System (PODS) enables frequent, cost-effective access to near GEO for SmallSats

PAYLOAD ORBITAL DELIVERY SYSTEM (PODS) The Payload Orbital Delivery System (PODS) enables frequent, cost-effective access to near GEO for SmallSats PAYLOAD ORBITAL DELIVERY SYSTEM (PODS) The Payload Orbital Delivery System (PODS) enables frequent, cost-effective access to near GEO for SmallSats /sslmda PAYLOAD ORBITAL DELIVERY SYSTEM (PODS) Mission

More information

Fundamentals of Satellite technology

Fundamentals of Satellite technology Fundamentals of Satellite technology Prepared by A.Kaviyarasu Assistant Professor Department of Aerospace Engineering Madras Institute Of Technology Chromepet, Chennai Orbital Plane All of the planets,

More information

INCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT

INCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Presentation Outline Mission Overview Mission Relevance

More information

INCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT

INCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Mission Overview Mission Relevance ConOps INCA Payload

More information

INTER-AGENCY SPACE DEBRIS COORDINATION COMMITTEE (IADC) SPACE DEBRIS ISSUES IN THE GEOSTATIONARY ORBIT AND THE GEOSTATIONARY TRANSFER ORBITS

INTER-AGENCY SPACE DEBRIS COORDINATION COMMITTEE (IADC) SPACE DEBRIS ISSUES IN THE GEOSTATIONARY ORBIT AND THE GEOSTATIONARY TRANSFER ORBITS INTER-AGENCY SPACE DEBRIS COORDINATION COMMITTEE (IADC) SPACE DEBRIS ISSUES IN THE GEOSTATIONARY ORBIT AND THE GEOSTATIONARY TRANSFER ORBITS Presented to: 37-th Session of the SCIENTIFIC AND TECHNICAL

More information

HNRS 227 Fall 2007 Chapter 14. Earth in Space presented by Prof. Geller 25 October 2007

HNRS 227 Fall 2007 Chapter 14. Earth in Space presented by Prof. Geller 25 October 2007 HNRS 227 Fall 2007 Chapter 14 Earth in Space presented by Prof. Geller 25 October 2007 Key Points of Chapter 14 Shape, Size and Motions of the Earth Rotation and Revolution Precession Coordinate Systems

More information

IADC Re-Entry Prediction Campaigns

IADC Re-Entry Prediction Campaigns IADC Re-Entry Prediction Campaigns H. Klinkrad, ESA IADC chair UNCOPUOS STSC, Feb 2009 page 1 Presentation Outline terms of reference of the Inter-Agency Space Debris Coordination Committee (IADC) concept

More information

Large FOV Mobile E-O Telescope for Searching and Tracking Low-earth Orbit Micro-satellites and Space Debris

Large FOV Mobile E-O Telescope for Searching and Tracking Low-earth Orbit Micro-satellites and Space Debris Large FOV Mobile E-O Telescope for Searching and Tracking Low-earth Orbit Micro-satellites and Space Debris WANG Jian-li, ZHAO Jin-yu, ZHANG Shi-xue Changchun Institute of Optics, Fine Mechanics and Physics,

More information

Increasing the Accuracy of Orbital Position Information from NORAD SGP4 Using Intermittent GPS Readings

Increasing the Accuracy of Orbital Position Information from NORAD SGP4 Using Intermittent GPS Readings Increasing the Accuracy of Orbital Position Information from NORAD SGP4 Using Intermittent GPS Readings Michael Greene Robert E. Zee Space Flight Laboratory University of Toronto 12 August 2009 23 rd Annual

More information

Space Debris Mapping Services for use by LEO Satellite Operators. Adam Archuleta DigitalGlobe,

Space Debris Mapping Services for use by LEO Satellite Operators. Adam Archuleta DigitalGlobe, Space Debris Mapping Services for use by LEO Satellite Operators Adam Archuleta DigitalGlobe, adam.archuleta@digitalglobe.com Michael Nicolls LeoLabs, mike@leolabs.net ABSTRACT Space situational awareness

More information

ANALYSIS OF THE EGLIN RADAR DEBRIS FENCE

ANALYSIS OF THE EGLIN RADAR DEBRIS FENCE ANALYSIS OF THE EGLIN RADAR DEBRIS FENCE Thomas J. Settecerri, Alan D. Skillicorn (The MITRE Corporation), Paul C. Spikes (AFMC ESC/Det. 5) BACKGROUND The Eglin FPS-85 space surveillance radar is a bi-static

More information

Analytical Method for Space Debris propagation under perturbations in the geostationary ring

Analytical Method for Space Debris propagation under perturbations in the geostationary ring Analytical Method for Space Debris propagation under perturbations in the geostationary ring July 21-23, 2016 Berlin, Germany 2nd International Conference and Exhibition on Satellite & Space Missions Daniel

More information

Benefits of a Geosynchronous Orbit (GEO) Observation Point for Orbit Determination

Benefits of a Geosynchronous Orbit (GEO) Observation Point for Orbit Determination Benefits of a Geosynchronous Orbit (GEO) Observation Point for Orbit Determination Ray Byrne, Michael Griesmeyer, Ron Schmidt, Jeff Shaddix, and Dave Bodette Sandia National Laboratories ABSTRACT Determining

More information

Astrodynamics 103 Part 1: Gauss/Laplace+ Algorithm

Astrodynamics 103 Part 1: Gauss/Laplace+ Algorithm Astrodynamics 103 Part 1: Gauss/Laplace+ Algorithm unknown orbit Observer 1b Observer 1a r 3 object at t 3 x = r v object at t r 1 Angles-only Problem Given: 1a. Ground Observer coordinates: ( latitude,

More information

BeiDou and Galileo, Two Global Satellite Navigation Systems in Final Phase of the Construction, Visibility and Geometry

BeiDou and Galileo, Two Global Satellite Navigation Systems in Final Phase of the Construction, Visibility and Geometry http://www.transnav.eu the International Journal on Marine Navigation and Safety of Sea Transportation Volume 10 Number 3 September 2016 DOI: 10.12716/1001.10.03.01 BeiDou and Galileo, Two Global Satellite

More information

Space Physics: Recent Advances and Near-term Challenge. Chi Wang. National Space Science Center, CAS

Space Physics: Recent Advances and Near-term Challenge. Chi Wang. National Space Science Center, CAS Space Physics: Recent Advances and Near-term Challenge Chi Wang National Space Science Center, CAS Feb.25, 2014 Contents Significant advances from the past decade Key scientific challenges Future missions

More information

Coverage, Responsiveness, and Accessibility for Various Responsive Orbits

Coverage, Responsiveness, and Accessibility for Various Responsive Orbits 3rd Responsive Space Conference RS3-2005-2002 Coverage, Responsiveness, and Accessibility for Various Responsive Orbits James R. Wertz Microcosm, Inc. El Segundo, CA 3rd Responsive Space Conference April

More information

Experimental Analysis of Low Earth Orbit Satellites due to Atmospheric Perturbations

Experimental Analysis of Low Earth Orbit Satellites due to Atmospheric Perturbations Experimental Analysis of Low Earth Orbit Satellites due to Atmospheric Perturbations Aman Saluja #1, Manish Bansal #2, M Raja #3, Mohd Maaz #4 #Aerospace Department, University of Petroleum and Energy

More information

Falcon-9 stage 2 post-burn fuel dump observation from Australia May 10, Jim Oberg July 10, 2018 ROUGH REVIEW DRAFT

Falcon-9 stage 2 post-burn fuel dump observation from Australia May 10, Jim Oberg July 10, 2018 ROUGH REVIEW DRAFT Falcon-9 stage 2 post-burn fuel dump observation from Australia May 10, 2018 Jim Oberg jameseoberg@comcast.net July 10, 2018 ROUGH REVIEW DRAFT OUTLINE Accidentally-observed double-spiral fuel dump from

More information

Sensor Calibration as an Application of Optimal Sequential Estimation toward Maintaining the Space Object Catalog

Sensor Calibration as an Application of Optimal Sequential Estimation toward Maintaining the Space Object Catalog Sensor Calibration as an Application of Optimal Sequential Estimation toward Maintaining the Space Object Catalog John H. Seago James W. Woodburn Page 1 of 27 Overview In our paper: We propose the application

More information

ORBIT PERTURBATION ANALYSIS OF WEST FORD NEEDLES CLUSTERS

ORBIT PERTURBATION ANALYSIS OF WEST FORD NEEDLES CLUSTERS AIAA-2000-4236 ORBIT PERTURBATION ANALYI OF WET FORD NEEDLE CLUTER Bruce R. Bowman pace Warfare Center, Analysis and Engineering Division chriever AFB, Colorado William N. Barker, and William G. chick

More information

Proton Launch System Mission Planner s Guide APPENDIX F. Proton Launch System Options and Enhancements

Proton Launch System Mission Planner s Guide APPENDIX F. Proton Launch System Options and Enhancements Proton Launch System Mission Planner s Guide APPENDIX F Proton Launch System Options and Enhancements F. PROTON LAUNCH SYSTEM OPTIONS AND ENHANCEMENTS The missions presented in the previous sections represent

More information

Analysis of Debris from the Collision of the Cosmos 2251 and the Iridium 33 Satellites

Analysis of Debris from the Collision of the Cosmos 2251 and the Iridium 33 Satellites Science & Global Security, 18:87 118, 2010 Copyright C Taylor & Francis Group, LLC ISSN: 0892-9882 print / 1547-7800 online DOI: 10.1080/08929882.2010.493078 Analysis of Debris from the Collision of the

More information

Planetary Science Unit Map Grade 8

Planetary Science Unit Map Grade 8 Planetary Science Unit Map Grade 8 Course Goal and Description: In Planetary Science students study the Earth as a celestial object before progressing to lunar science/exploration, and then to Solar System

More information

Sunbeams from Space Mirrors Feeding Solar Farms on the Ground at Dusk and Dawn. Lewis M Fraas EUEC 2013 Phoenix, AZ Jan

Sunbeams from Space Mirrors Feeding Solar Farms on the Ground at Dusk and Dawn. Lewis M Fraas EUEC 2013 Phoenix, AZ Jan Sunbeams from Space Mirrors Feeding Solar Farms on the Ground at Dusk and Dawn Lewis M Fraas EUEC 2013 Phoenix, AZ Jan 29 2013 Outline 1. Introduction 2. Background 3. Concept 4. Economics 5. Satellite

More information

The 2013 MAVEN Mission To Mars. Bruce Jakosky MAVEN Principal Investigator University of Colorado

The 2013 MAVEN Mission To Mars. Bruce Jakosky MAVEN Principal Investigator University of Colorado The 2013 MAVEN Mission To Mars Bruce Jakosky MAVEN Principal Investigator University of Colorado Summary of MAVEN Status We ve been developing MAVEN since 2003; now under 3 months to launch! All science

More information

ERTH 455 / GEOP 555 Geodetic Methods. Lecture 04: GPS Overview, Coordinate Systems

ERTH 455 / GEOP 555 Geodetic Methods. Lecture 04: GPS Overview, Coordinate Systems ERTH 455 / GEOP 555 Geodetic Methods Lecture 04: GPS Overview, Coordinate Systems Ronni Grapenthin rg@nmt.edu MSEC 356 x5924 August 30, 2017 1 / 22 2 / 22 GPS Overview 1973: Architecture approved 1978:

More information

LEO cubesats tracking with a network of Polish optical SST sensors

LEO cubesats tracking with a network of Polish optical SST sensors LEO cubesats tracking with a network of Polish optical SST sensors Krzysztof Kamiński, Edwin Wnuk, Justyna Gołębiewska, Mikołaj Krużyński, Monika K. Kamińska Astronomical Observatory Institute, Faculty

More information

An Astrophysics Mission of Opportunity on the International Space Station

An Astrophysics Mission of Opportunity on the International Space Station GSFC 1 An Astrophysics Mission of Opportunity on the International Space Station Science: Understanding ultra-dense matter through observations of neutron stars in the soft X-ray band Launch: October 2016,

More information

Useful Formulas and Values

Useful Formulas and Values Name Test 1 Planetary and Stellar Astronomy 2017 (Last, First) The exam has 20 multiple choice questions (3 points each) and 8 short answer questions (5 points each). This is a closed-book, closed-notes

More information