An Album of the Orbital Behavior of the Tselina-2 Satellites
|
|
|
- Sheena Ferguson
- 5 years ago
- Views:
Transcription
1 An Album of the Orbital Behavior of the Tselina-2 Satellites Compiled August 9, 2008 Mean altitude in this album is defined as semimajor axis (SMA) of the orbit in kilometers minus SMA is computed from the period (86400/mean motion) via the formula SMA = ( * (period^(2/3))/1000. Mean motion is extracted from the usual two-line orbital elements (TLE). Several Tselina-2 satellites, also known as ELINT-4 and Cosmos 1603 type, have displayed prolonged and repeated periods during which the semi-major axis and thus the orbital energy increases. This is believed to be due to a 14-th order resonance with the Earth's gravitational field. Apparently this resonance is an intended feature of the orbits, but the reason for it is not known maintenance of the ELINT constellation and desired coverage characteristics has been the default speculation.
2 Soviet/Russian ELINT Satellites in the Cosmos 1603/ELINT-4/Tselina-2/11F644 Family Reported mass: ~ 3,000 kg
3 Cosmos 1603 Cosmos 1603, NORAD 15333, COSPAR A Mean altitude vs time
4 Cosmos 1656 Cosmos 1656, NORAD 15755, COSPAR A Mean altitude vs time
5 Cosmos 1697 Cosmos 1697, NORAD 16181, COSPAR A Mean altitude vs time
6 Cosmos 1833 Cosmos 1833, NORAD 17589, COSPAR A Mean altitude vs time Cosmos 1833 RB, NORAD 17590
7 Cosmos 1844 Cosmos 1844, NORAD 17973, COSPAR A Mean altitude vs time Mean altitude vs time
8 Cosmos 1943 Cosmos 1943, NORAD 19119, COSPAR A Mean altitude vs time
9 Cosmos 1980 Cosmos 2082, NORAD 19649, COSPAR A Mean altitude vs time
10 Cosmos 2082 Cosmos 2082, NORAD 20624, COSPAR A Mean altitude vs time
11 Cosmos 2219 Cosmos 2219, NORAD 22219, COSPAR A Mean altitude vs time
12 Cosmos 2227 Cosmos 2227, NORAD 22284, COSPAR A Mean altitude vs time
13 Cosmos 2237 Cosmos 2237, NORAD 22565, COSPAR A Mean altitude vs time
14 Cosmos 2263 Cosmos 2263, NORAD 22802, COSPAR A Mean altitude vs time
15 Cosmos 2278 Cosmos 2278, NORAD 23087, COSPAR A Mean altitude vs time
16 Cosmos 2297 Cosmos 2297, NORAD 23404, COSPAR A Mean altitude vs time
17 Cosmos 2322 Cosmos 2322, NORAD 23704, COSPAR A Mean altitude vs time
18 Cosmos 2333 Cosmos 2333, NORAD 24297, COSPAR A Mean altitude vs time
19 Cosmos 2360 Cosmos 2360, NORAD 25406, COSPAR A Mean altitude vs time
20 Cosmos 2369 COSMOS 2369, NORAD 26069, COSPAR A Mean altitude vs time
21 Cosmos 2406 COSMOS 2406, NORAD 28352, COSPAR A Mean altitude vs time
22 Cosmos 2428 COSMOS 2428, NORAD 31792, COSPAR A Mean altitude vs time
23 Composite of all Tselina-2 orbital mean altitudes Four other satellites (NORAD 02909, 05398, 12739, 20798) shown for comparison Surcal 150 B (NORAD 02909) passing through Tselina-2 orbital height
24 Comparison Satellites Newsgroups: sci.astro From: Date: 14 Dec 93 16:50:56 PST Local: Tues, Dec :50 pm Subject: Spherical satellites For those interested in following the details of satellite orbital behavior, the following information may be useful. Over the years, several countries have launched spherical satellites, initially for space surveillance system calibration and later as geodetic aids. All of them, particularly those in lower orbits, should be good for monitoring fluctuations in atmospheric density and for 'normalizing' the behavior of other objects at similar altitudes. [snip] Below is a table of the information I've found on the satellites, giving their masses and diameters; note that different sources give slightly different values for these numbers, so don't do anything with them that requires great precision. [snip] Int'l NORAD Name/Description Diameter Mass cm kg 64063C Calsphere E Calsphere C Lincoln Calibration Sphere E Tempsat (dull black) H Calsphere 4A (white) B Calsphere H Calsphere?? 67053J Surcal 150B E LCS 4/Gridsphere A Starlette (60 corner reflectors) A Lageos (426 corner reflectors) A EGP (318 mirrors & 120 corner reflectors) C Etalon 1 (> 2000 corner reflectors) C Etalon 2 (> 2000 corner reflectors) B Lageos II (426 corner reflectors) B Stella (60 corner reflectors) 24 48
25 Calsphere 1 NORAD 00900, COSPAR C Mean Altitude vs Time Diameter: 36 cm Mass: 1 kg A/M = m^2/kg
26 CALSPHERE 2 NORAD 00902, COSPAR E Mean Altitude vs Time Diameter: 36 cm Mass: 10 kg A/M = m^2/kg
27 Calsphere 4A Calsphere 4A, NORAD 01520, COSPAR H Mean Altitude vs Time Diameter: 36 cm Mass: 2 kg A/M = m^2/kg
28 Calsphere Calsphere, NORAD 02825, COSPAR B Mean Altitude vs Time Diameter: 51 cm Mass: 2.4 kg A/M = m^2/kg
29 Calsphere Calsphere, NORAD 02874, COSPAR H Mean Altitude
30 Surcal 150 B Surcal 150B, NORAD 02909, COSPAR J Mean Altitude Diameter: 41 cm Mass: 1.5 kg A/M = m^2/kg
31 LCS 4 / Gridsphere 1 LCS 4 / Gridsphere 1, NORAD 05398, COSPAR E Mean Altitude Diameter: 113 cm Mass: 37 kg A/M = m^2/kg
32 Starlette Starlette, NORAD 07646, COSPAR A Mean Altitude Diameter: 25 cm Mass: 47 kg A/M = m^2/kg
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
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
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
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
SLR Graz: khz Satellite Laser Ranging & Co
Graz in Space 2014 KFU Graz 4. 5. September 2014 SLR Graz: khz Satellite Laser Ranging & Co Georg Kirchner, Franz Koidl, Oliver Baur Space Research Institute Austrian Academy of Sciences Outline What is
Explain how it is possible for the gravitational force to cause the satellite to accelerate while its speed remains constant.
YEAR 12 PHYSICS: GRAVITATION PAST EXAM QUESTIONS Name: QUESTION 1 (1995 EXAM) (a) State Newton s Universal Law of Gravitation in words (b) A satellite of mass (m) moves in orbit of a planet with mass (M).
Chapter 12 Gravity. Copyright 2010 Pearson Education, Inc.
Chapter 12 Gravity Units of Chapter 12 Newton s Law of Universal Gravitation Gravitational Attraction of Spherical Bodies Kepler s Laws of Orbital Motion Gravitational Potential Energy Energy Conservation
A TLE-BASED REPRESENTATION OF PRECISE ORBIT PREDICTION RESULTS. Jizhang Sang and Bin Li. School of Geodesy and Geomatics, Wuhan University
A TLE-BASED REPRESENTATION OF PRECISE ORBIT PREDICTION RESULTS Jizhang Sang and Bin Li School of Geodesy and Geomatics, Wuhan University ABSTRACT The computing efficiency of the analytic SGP4 algorithm
[2] Explain why values of gravitational potential near to an isolated mass are all negative [3]
![[2] Explain why values of gravitational potential near to an isolated mass are all negative [3]](/thumbs/81/84541203.jpg "[2] Explain why values of gravitational potential near to an isolated mass are all negative [3]")
1 (a) Define gravitational potential.... [2] (b) Explain why values of gravitational potential near to an isolated mass are all negative.... [3] (c) The Earth may be assumed to be an isolated sphere of
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
CHAPTER 10 TEST REVIEW
IB PHYSICS Name: Period: Date: # Marks: 69 Raw Score: IB Curve: DEVIL PHYSICS BADDEST CLASS ON CAMPUS CHAPTER 10 TEST REVIEW 1. A spacecraft travels away from Earth in a straight line with its motors shut
Modern Navigation. Thomas Herring
12.215 Modern Navigation Thomas Herring Today s Class Latitude and Longitude Simple spherical definitions Geodetic definition: For an ellipsoid Astronomical definition: Based on direction of gravity Relationships
This assignment is worth 20 points. Each part is worth 1 point, except for the last problem, in which each part is worth half a point.
1 of 6 11/20/2009 3:43 PM 0/20 Tue Dec 1 2009 10:15 PM EST Question Points 1 2 3 4 5 6 7 8 9 0/20/20/30/10/30/10/20/20/4 Total 0/20 Description This assignment is worth 20 points. Each part is worth 1
THE INITIAL ORBIT DETERMINATION OF LEO SATELLITES OBSERVED NEAR THE LOCAL ZENITH
THE INITIAL ORBIT DETERMINATION OF LEO SATELLITES OBSERVED NEAR THE LOCAL ZENITH M.A. Earl (a) (a) Royal Military College of Canada, Kingston ON, earl-m@castor.ca Abstract Our large satellite population
Using the DSST Semi-Analytical Orbit Propagator Package via the N ondy Web Open Science Environment
Using the DSST Semi-Analytical Orbit Propagator Package via the N ondy Web Open Science Environment Astrody Web T ools T ools / J. F. San Juan, M. Lara, R. López, L. M. López, B. Weeden and P. J. Cefola
Determination of long-term changes in the Earth's gravity field from satellite laser ranging observations
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 102, NO. B10, PAGES 22,377-22,390, OCTOBER 10, 1997 Determination of long-term changes in the Earth's gravity field from satellite laser ranging observations M. K.
Physics Mechanics Lecture 30 Gravitational Energy
Physics 170 - Mechanics Lecture 30 Gravitational Energy Gravitational Potential Energy Gravitational potential energy of an object of mass m a distance r from the Earth s center: Gravitational Potential
Supplemental Questions 12U
Supplemental Questions 12U Gravitational, Electric and Magnetic Fields Questions A satellite of mass 5.00x10² kg is in a circular orbit of radius 2r around Earth. Then it is moved to a circular orbit radius
Earth gravity field recovery using GPS, GLONASS, and SLR satellites
Earth gravity field recovery using GPS, GLONASS, and SLR satellites Krzysztof Sośnica (1), Adrian Jäggi (1), Daniela Thaller (2), Ulrich Meyer (1), Gerhard Beutler (1), Rolf Dach (1) (1) Astronomical Institute,
Graz in Space Graz SLR System. Daniel Kucharski. IWF / SatGeo
Graz in Space 2008 Graz SLR System Daniel Kucharski IWF / SatGeo Satellite Laser Ranging Range measurements to the satellites - time of flight of the ultrashort laser pulses - mm precision station-satellite
Chapter 13: universal gravitation
Chapter 13: universal gravitation Newton s Law of Gravitation Weight Gravitational Potential Energy The Motion of Satellites Kepler s Laws and the Motion of Planets Spherical Mass Distributions Apparent
SECOND ANNOUNCEMENT International Technical Laser Workshop 2012 (ITLW-12)
SECOND ANNOUNCEMENT International Technical Laser Workshop 2012 (ITLW-12) Version 31/Oct/12 Satellite, Lunar and Planetary Laser Ranging: characterizing the space segment Frascati National Laboratories
USA Space Debris Environment, Operations, and Modeling Updates
USA Space Debris Environment, Operations, and Modeling Updates Presentation to the 51 st Session of the Scientific and Technical Subcommittee Committee on the Peaceful Uses of Outer Space United Nations
AP Physics Multiple Choice Practice Gravitation
AP Physics Multiple Choice Practice Gravitation 1. Each of five satellites makes a circular orbit about an object that is much more massive than any of the satellites. The mass and orbital radius of each
Chapter 13. Universal Gravitation 13.1: Newton's Law of Universal Gravitation 13.2: Free-Fall Acceleration and the Gravitational Force
Chapter 13 Universal Gravitation 13.1: Newton's Law of Universal Gravitation 13.2: Free-Fall Acceleration and the Gravitational Force 1 Planetary Motion A large amount of data had been collected by 1687.
AP Physics QUIZ Gravitation
AP Physics QUIZ Gravitation Name: 1. If F1 is the magnitude of the force exerted by the Earth on a satellite in orbit about the Earth and F2 is the magnitude of the force exerted by the satellite on the
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
Chapter 13. Gravitation
Chapter 13 Gravitation 13.2 Newton s Law of Gravitation Here m 1 and m 2 are the masses of the particles, r is the distance between them, and G is the gravitational constant. G =6.67 x10 11 Nm 2 /kg 2
University Physics (Prof. David Flory) Chapt_14 Thursday, November 15, 2007 Page 1
University Physics (Prof. David Flory) Chapt_14 Thursday, November 15, 2007 Page 1 Name: Date: 1. An artificial satellite of Earth releases a bomb. Neglecting air resistance, the bomb will: A) strike Earth
Statistical methods to address the compliance of GTO with the French Space Operations Act
Statistical methods to address the compliance of GTO with the French Space Operations Act 64 th IAC, 23-27 September 2013, BEIJING, China H.Fraysse and al. Context Space Debris Mitigation is one objective
IMPACT OF THE ATMOSPHERIC DRAG ON STARLETTE, STELLA, AJISAI, AND LARES ORBITS
ARTIFICIAL SATELLITES, Vol. 50, No. 1 2015 DOI: 10.1515/arsa-2015-0001 IMPACT OF THE ATMOSPHERIC DRAG ON STARLETTE, STELLA, AJISAI, AND LARES ORBITS Krzysztof Sośnica 1,2 1 Astronomical Institute, University
PHYS 101 Previous Exam Problems. Gravitation
PHYS 101 Previous Exam Problems CHAPTER 13 Gravitation Newton s law of gravitation Shell theorem Variation of g Potential energy & work Escape speed Conservation of energy Kepler s laws - planets Orbits
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
Orbit Evolution of the Swarm Mission Detlef Sieg
Orbit Evolution of the Swarm Mission Detlef Sieg Content Orbit history absolute Aerodynamic scale factors from orbit determination Altitude history and prediction RAAN/LTAN (orbit plane rotation) Orbital
CHARACTERIZING THE EFFECTS OF LOW ORDER PERTURBATIONS ON GEODETIC SATELLITE PRECISION ORBIT DETERMINATION
(Preprint) AAS 15-778 CHARACTERIZING THE EFFECTS OF LOW ORDER PERTURBATIONS ON GEODETIC SATELLITE PRECISION ORBIT DETERMINATION Eric Eiler, and John G. Warner, INTRODUCTION Satellite operations often rely
End-of-Chapter Exercises
End-of-Chapter Exercises Exercises 1 12 are primarily conceptual questions that are designed to see if you have understood the main concepts of the chapter. Treat all balls with mass as point masses. 1.
Updates on CMA FENGYUN Meteorological Satellite Programs
Updates on CMA FENGYUN Meteorological Satellite Programs Peng ZHANG National Satellite Meteorological Center, China Meteorological Administration (NSMC/CMA) 29 Nov. - 5 Dec. 2017, Darmstadt, Germany 1.
HW Chapter 5 Q 7,8,18,21 P 4,6,8. Chapter 5. The Law of Universal Gravitation Gravity
HW Chapter 5 Q 7,8,18,21 P 4,6,8 Chapter 5 The Law of Universal Gravitation Gravity Newton s Law of Universal Gravitation Every particle in the Universe attracts every other particle with a force that
ORBITS WRITTEN Q.E. (June 2012) Each of the five problems is valued at 20 points. (Total for exam: 100 points)
ORBITS WRITTEN Q.E. (June 2012) Each of the five problems is valued at 20 points. (Total for exam: 100 points) PROBLEM 1 A) Summarize the content of the three Kepler s Laws. B) Derive any two of the Kepler
Earth gravity field recovery using GPS, GLONASS, and SLR satellites
13-01-08 Earth gravity field recovery using GPS, GLONASS, and SLR satellites Krzysztof Sośnica (1), Adrian Jäggi (1), Daniela Thaller (2), Ulrich Meyer (1), Christian Baumann (1), Rolf Dach (1), Gerhard
Universal Gravitation
Universal Gravitation Newton s Law of Universal Gravitation Every particle in the Universe attracts every other particle with a force that is directly proportional to the product of their masses and inversely
Welcome back to Physics 215
Welcome back to Physics 215 Today s agenda: Gravity 15-2 1 Current assignments HW#15 due Monday, 12/12 Final Exam, Thursday, Dec. 15 th, 3-5pm in 104N. Two sheets of handwritten notes and a calculator
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
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
Gravitation and Newton s Synthesis
Lecture 10 Chapter 6 Physics I 0.4.014 Gravitation and Newton s Synthesis Course website: http://faculty.uml.edu/andriy_danylov/teaching/physicsi Lecture Capture: http://echo360.uml.edu/danylov013/physics1spring.html
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
RADAR-OPTICAL OBSERVATION MIX
RADAR-OPTICAL OBSERVATION MIX Felix R. Hoots + Deep space satellites, having a period greater than or equal to 225 minutes, can be tracked by either radar or optical sensors. However, in the US Space Surveillance
Physics 111. Tuesday, November 9, Universal Law Potential Energy Kepler s Laws. density hydrostatic equilibrium Pascal s Principle
ics Tuesday, ember 9, 2004 Ch 12: Ch 15: Gravity Universal Law Potential Energy Kepler s Laws Fluids density hydrostatic equilibrium Pascal s Principle Announcements Wednesday, 8-9 pm in NSC 118/119 Sunday,
Outline for Today: Newton s Law of Universal Gravitation The Gravitational Field Orbital Motion Gravitational Potential Energy. Hello!
PHY131H1F - Class 13 Outline for Today: Newton s Law of Universal Gravitation The Gravitational Field Orbital Motion Gravitational Potential Energy Under the Flower of Kent apple tree in the Woolsthorpe
Atmospheric Drag. Modeling the Space Environment. Manuel Ruiz Delgado. European Masters in Aeronautics and Space
Atmospheric Drag p. 1/29 Atmospheric Drag Modeling the Space Environment Manuel Ruiz Delgado European Masters in Aeronautics and Space E.T.S.I. Aeronáuticos Universidad Politécnica de Madrid April 2008
Copyright 2010 Pearson Education, Inc. GRAVITY. Chapter 12
GRAVITY Chapter 12 Units of Chapter 12 Newton s Law of Universal Gravitation Gravitational Attraction of Spherical Bodies Kepler s Laws of Orbital Motion Gravitational Potential Energy Energy Conservation
Chapter 12 Gravity. Copyright 2010 Pearson Education, Inc.
Chapter 12 Gravity Units of Chapter 12 Newton s Law of Universal Gravitation Gravitational Attraction of Spherical Bodies Kepler s Laws of Orbital Motion Gravitational Potential Energy Energy Conservation
Collision Risk Assessment for Spacecraft with CASS
Collision Risk Assessment for Spacecraft with CASS Ma Chaowei 2011, 17-18 Oct 2011 Beijing Institute of Tracking and Telecommunications Technology Ma Chaowei 2 Contents Introduction Basic Information of
SPACE SITUATIONAL AWARENESS AND SPACE DEBRIS ACTIVITIES IN INDIA
SPACE SITUATIONAL AWARENESS AND SPACE DEBRIS ACTIVITIES IN INDIA P Soma, Adjunct Faculty, NIAS Agenda The Growth of Space Objects since 1957 Space Situational Awareness India s Space Assets and SSA Space
Questions Chapter 13 Gravitation
Questions Chapter 13 Gravitation 13-1 Newton's Law of Gravitation 13-2 Gravitation and Principle of Superposition 13-3 Gravitation Near Earth's Surface 13-4 Gravitation Inside Earth 13-5 Gravitational
Orbits. Objectives. Orbits and unbalanced forces. Equations 4/7/14
Orbits Objectives Describe and calculate how the magnitude of the gravitational force between two objects depends on their masses and the distance between their centers. Analyze and describe orbital circular
Outline for Today: Newton s Law of Universal Gravitation The Gravitational Field Orbital Motion Gravitational Potential Energy
PHY131H1F - Class 13 Outline for Today: Newton s Law of Universal Gravitation The Gravitational Field Orbital Motion Gravitational Potential Energy Under the Flower of Kent apple tree in the Woolsthorpe
Assessment of the International Terrestrial Reference System 2014 realizations by Precise Orbit Determination of SLR Satellites
Deutsches Geodätisches Forschungsinstitut (DGFI-TUM) Technische Universität München Assessment of the International Terrestrial Reference System 2014 realizations by Precise Orbit Determination of SLR
Q1. (a) Explain what is meant by the gravitational potential at a point in a gravitational field (2)
PhysicsAndMathsTutor.com 1 Q1. (a) Explain what is meant by the gravitational potential at a point in a gravitational field............. Use the following data to calculate the gravitational potential
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,
Name Period Date. Record all givens, draw a picture, arrow all vectors, write the formula, substitute and solve. units
Example Problems 12.1 E1. Doc Fizzix, whose mass is 65.0 kg, is doing a physics demonstration at the front of the classroom. How much gravitational force does Doc Fizzix exert on Rob, whose mass is 55
Inertial Frame frame-dragging
Frame Dragging Frame Dragging An Inertial Frame is a frame that is not accelerating (in the sense of proper acceleration that would be detected by an accelerometer). In Einstein s theory of General Relativity
Gravity 3. Gravity 3. Gravitational Potential and the Geoid. Chuck Connor, Laura Connor. Potential Fields Geophysics: Week 2.
Gravitational Potential and the Geoid Chuck Connor, Laura Connor Potential Fields Geophysics: Week 2 Objectives for Week 1 Gravity as a vector Gravitational Potential The Geoid Gravity as a vector We can
New Observation Results from A Rotating-drift-scan CCD System
New Observation Results from A Rotating-drift-scan CCD System TANG Zhenghong, MAO Yindun, LI Yan, YU Yong Shanghai Astronomical Observatory 2011-10 TANG Zhenghong 1 Background Up to now, the number of
Gravitation and Newton s Synthesis
Lecture 10 Chapter 6 Physics I 0.4.014 Gravitation and Newton s Synthesis Course website: http://faculty.uml.edu/andriy_danylov/teaching/physicsi Lecture Capture: http://echo360.uml.edu/danylov013/physics1spring.html
Prediction accuracy analysis from orbital elements generated for a new space object catalogue
Prediction accuracy analysis from orbital elements generated for a new space object catalogue James Bennett, Michael Lachut, Ben Greene SERC Limited, Mt Stromlo Observatory, Cotter Road, Weston Creek,
ORBITAL DECAY PREDICTION AND SPACE DEBRIS IMPACT ON NANO-SATELLITES
Journal of Science and Arts Year 16, No. 1(34), pp. 67-76, 2016 ORIGINAL PAPER ORBITAL DECAY PREDICTION AND SPACE DEBRIS IMPACT ON NANO-SATELLITES MOHAMMED CHESSAB MAHDI 1 Manuscript received: 22.02.2016;
Think of a car turning a corner, or the fun carnival ride, or a satellite orbiting the earth.
Uniform Circular Motion Objects moving in curved(arc, semi circular, circular) path at constant speeds. Think of a car turning a corner, or the fun carnival ride, or a satellite orbiting the earth. When
Algebra Based Physics Newton's Law of Universal Gravitation
Algebra Based Physics Newton's Law of Universal Gravitation 2016 01 19 www.njctl.org Newton's Law of Universal Gravitation Gravitational Force Click on the topic to go to that section Gravitational Field
Chapter 5 Centripetal Force and Gravity. Copyright 2010 Pearson Education, Inc.
Chapter 5 Centripetal Force and Gravity v Centripetal Acceleration v Velocity is a Vector v It has Magnitude and Direction v If either changes, the velocity vector changes. Tumble Buggy Demo v Centripetal
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
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
PHY131H1F - Class 13 Harlow s Last Class this semester on Monday Prof. Meyertholen takes over!
PHY131H1F - Class 13 Harlow s Last Class this semester on Monday Prof. Meyertholen takes over! Today, Chapter 8 Sections 8.1-8.3: Dynamics in Two Dimensions Dynamics of Uniform Circular Motion Banked Curves
Chapter 13. Universal Gravitation
Chapter 13 Universal Gravitation Planetary Motion A large amount of data had been collected by 1687. There was no clear understanding of the forces related to these motions. Isaac Newton provided the answer.
Use of FY-3C/GNOS Data for Assessing the on-orbit Performance of Microwave Sounding Instruments
Use of FY-3C/GNOS Data for Assessing the on-orbit Performance of Microwave Sounding Instruments Xiuqing Hu 1 Xueyan Hou 2, and Mi Liao 1 1 National Satellite Meteorological Center (NSMC), CMA 2 Chinese
Newton s Gravitational Law
1 Newton s Gravitational Law Gravity exists because bodies have masses. Newton s Gravitational Law states that the force of attraction between two point masses is directly proportional to the product of
Investigations of Radioactive Contamination of Near-Earth Space
Investigations of Radioactive Contamination of Near-Earth Space N. Bakhtigaraev Institute of Astronomy of RAS M. Anikeeva - JSC «VNIIEM Corporation» K. Boyarchuk - JSC «NIIEM» S. Kuzin - Lebedev Physical
Accuracy of Earth s Thermospheric Neutral Density Models
AIAA 2006-6167 Accuracy of Earth s Thermospheric Neutral Density Models Frank A. Marcos 1 Air Force Research Laboratory Hanscom AFB, MA 01731-3010 Bruce R. Bowman 2 Air Force Space Command Colorado Springs,
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
4.8 The Normal Force. Apparent Weight
4.8 The Normal Force Apparent Weight Definition: The apparent weight of an object is the reading of the scale. It is equal to the normal force the man exerts on the scale. For a man standing on a scale
Lecture 1d: Satellite Orbits
Lecture 1d: Satellite Orbits Outline 1. Newton s Laws of Motion 2. Newton s Law of Universal Gravitation 3. Kepler s Laws 4. Putting Newton and Kepler s Laws together and applying them to the Earth-satellite
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
ORBIT DETERMINATION ANALYSIS FOR A JOINT UK-AUSTRALIAN SPACE SURVEILLANCE EXPERIMENT
ORBIT DETERMINATION ANALYSIS FOR A JOINT UK-AUSTRALIAN SPACE SURVEILLANCE EXPERIMENT M. Rutten, * T. Bessell, * N. Gordon, *, * NSID, Defence Science and Technology Organisation, Australia School of ITEE,
Conceptual Physical Science 6 th Edition
1 2 1 Conceptual Physical Science 6 th Edition Chapter 4: GRAVITY, PROJECTILES, AND SATELLITES Sections 4.1, 4.5-4.9 only 3 2017 Pearson Education, Inc. This lecture will help you understand: The Universal
IAC-10.A Carolin Früh. 1 Astronomical Institute, University of Bern, Switzerland, Thomas Schildknecht 1
IAC-1.A6.1.9 ANALYSIS OF OBSERVED AND SIMULATED LIGHT CURVES OF SPACE DEBRIS Carolin Früh Astronomical Institute, University of Bern, Switzerland frueh@aiub.unibe.ch Thomas Schildknecht 1 Since 24, the
Nm kg. The magnitude of a gravitational field is known as the gravitational field strength, g. This is defined as the GM
Copyright FIST EDUCATION 011 0430 860 810 Nick Zhang Lecture 7 Gravity and satellites Newton's Law of Universal Gravitation Gravitation is a force of attraction that acts between any two masses. The gravitation
The spheres are now separated until the force of attraction is. What is the force of gravitational attraction between the satellite and the planet?
Q1.Two identical uniform spheres each of radius R are placed in contact. The gravitational force between them is F. The spheres are now separated until the force of attraction is. What is the distance
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
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
Real-time optical space situational awareness of low-earth orbit with small telescopes
Real-time optical space situational awareness of low-earth orbit with small telescopes Peter Zimmer J.T. McGraw and Associates, LLC John T. McGraw J.T. McGraw and Associates, LLC Mark R. Ackermann J.T.
Optical Surveys for Space Debris in MEO
Optical Surveys for Space Debris in MEO T. Schildknecht, A. Vananti, J. Herzog, A. Hinze Astronomical Institute, University of Bern, Switzerland H. Krag, T. Flohrer ESA / ESOC, Darmstadt, Germany 9 th
Midterm 3 Thursday April 13th
Welcome back to Physics 215 Today s agenda: rolling friction & review Newtonian gravity Planetary orbits Gravitational Potential Energy Physics 215 Spring 2017 Lecture 13-1 1 Midterm 3 Thursday April 13th
Testing General Relativity and gravitational physics using the LARES satellite
Eur. Phys. J. Plus (2012) 127: 133 DOI 10.1140/epjp/i2012-12133-8 Regular Article THE EUROPEAN PHYSICAL JOURNAL PLUS Testing General Relativity and gravitational physics using the LARES satellite Ignazio
Chapter 6 Gravitation and Newton s Synthesis
Chapter 6 Gravitation and Newton s Synthesis If the force of gravity is being exerted on objects on Earth, what is the origin of that force? Newton s realization was that the force must come from the Earth.
3.4.2 International Laser Ranging Service (ILRS)
3 Reports of IERS components 3.4 Technique Centres 3.4.2 International Laser Ranging Service (ILRS) Introduction Network The International Laser Ranging Service (ILRS), established in 1998, is responsible
Static Equilibrium Gravitation
Static Equilibrium Gravitation Lana Sheridan De Anza College Dec 6, 2017 Overview One more static equilibrium example Newton s Law of Universal Gravitation gravitational potential energy little g Example
arxiv: v1 [gr-qc] 6 Nov 2012
![arxiv: v1 [gr-qc] 6 Nov 2012](/thumbs/96/127056791.jpg "arxiv: v1 [gr-qc] 6 Nov 2012")
1 arxiv:1211.1374v1 [gr-qc] 6 Nov 2012 Testing General Relativity and gravitational physics using the LARES satellite Ignazio Ciufolini 1, Antonio Paolozzi 2, Erricos Pavlis 3, John Ries 4, Vahe Gurzadyan
COUNTING DOWN TO THE LAUNCH OF POPACS
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
Evaluation of the EGM2008 Gravity Model
Evaluation of the EGM2008 Gravity Model Minkang Cheng, John C. Ries and Don P. Chambers Center for Space Research, University of Texas at Austin, USA 3925 West Braker Lane, STE 200, Austin, TX 78759, USA
Satellite Orbital Maneuvers and Transfers. Dr Ugur GUVEN
Satellite Orbital Maneuvers and Transfers Dr Ugur GUVEN Orbit Maneuvers At some point during the lifetime of most space vehicles or satellites, we must change one or more of the orbital elements. For example,