News Nov. 2014 TX power of Rosetta is 28 W using a antenna dish sized 1.8 m The effective isotropic radiated power from Rosetta (HGA in X-Band) is 57 dBW.

Slides:



Advertisements
Similar presentations
Satellite Communication
Advertisements

Lecture 4: Propagation Models, Antennas and Link Budget Anders Västberg
Overview of new technologies Jørgen Bach Andersen, Aalborg University, Denmark Sven Kuhn, Rasmus Krigslund, Troels B. Sørensen.
Lab 3 Antennas.
Satellite Television 1 It’s out of sight! 22,300 miles in fact!
Communications - Access Schemes 1 Introduction to Space Systems and Spacecraft Design Space Systems Design.
Rapidly Deployable Radio Network 5.3 GHz Microstrip Patch Antennas
Polytechnic University© 2002 by H. L. Bertoni1 III. Spherical Waves and Radiation Antennas radiate spherical waves into free space Receiving antennas,
Communications - Access Schemes 1 Introduction to Space Systems and Spacecraft Design Space Systems Design.
Council for Technical Education & Vocational Training Rapti Engineering College Ghorahi, Dang Presentation on Satellite Communication Presented by Shailendra.
Lect 05© 2012 Raymond P. Jefferis III1 Satellite Communications Link budget analysis Transmitted power Transmitting antenna gain Path loss Receiving antenna.
SATELLITE LINK DESIGN By S.Sadhish Prabhu.
Lecture 2: Introduction to case studies: Radiolink Anders Västberg
Communication and Ground Station 12 October 2008.
ECE 5233 Satellite Communications
Ron Milione Ph.D. W2TAP W2TAP InformationModulatorAmplifier Ant Feedline Transmitter InformationDemodulatorPre-Amplifier Ant Feedline Receiver Filter.
Sistem Jaringan dan Komunikasi Data #3. Overview  guided - wire / optical fibre  unguided - wireless  characteristics and quality determined by medium.
VSOP-2 Ground Link Station - Tracking Station Requirements - National Astronomical Observatory of Japan Y. Kono.
Satellite Microwave MMG Rashed Sr. Lecturer, Dept. of ETE Daffodil International University.
Namaste Project 3.4 GHz Interference Study Preliminary document - Work in Progress updated The intent of this study is to collect data which may.
Student Satellite Project Tracking, Telemetry & Command UASat Progress Review Tracking, Telemetry and Command (TTC) January 26, 1999 Dana Irvin, Team Leader.
2.4 GHz CubeSat Communications System Robert Bui Communications Subsystem Lead.
Oct. 16, 2006 Midterm Next Class Assignment #4 is Marked
Chapter 3 Radio Frequency Components, Measurements, and Mathematics
Author: Bill Buchanan Wireless LAN Unit 6 Radio and RF Wireless LAN Unit 6 Radio and RF.
THE PAST THE PAST 3 SPUTNIK l Sputnik – Oct 4, st satellite. 20 MHz beacon. 47 years ago. l Oscar 1 – Dec 12, st amateur satellite l.
Section Number - 1 NASA’s Goddard Space Flight Center Communication Systems Jason A. Soloff NASA/GSFC Code 567 August 16-17, 2005.
24/03/2003Jacques MdM / REF France1 HF Receivers desensitisation from wideband noise spurious in HF bands (1.8 to 30 MHZ) Impact of spurious radiations.
ECE 4710: Lecture #36 1 Chapter 8  Chapter 8 : Wired and Wireless Communication Systems  Telephone  Fiber Optic  DSL  Satellite  Digital & Analog.
Wireless Communication Fundamentals David Holmer
Oct. 23, 2006 Midterm Marked. –Average: 73%. 6 below, 9 above –Answer Key posted: s/nten216/Tests/NTEN216_Midterm1WithAns.
The Ultimate DX Experience: Mars! By Marc. C. Tarplee, Ph.D. N4UFP
RF Propagation No. 1  Seattle Pacific University Basic RF Transmission Concepts.
BASIC LINK BUDGETS SATELLITE LINKS
NASA’s Goddard Space Flight Center Lunar Reconnaissance Orbiter Ground System Requirements.
Modulation What is modulation?
Final Version Frank Stocklin Ron Vento Bob Summers May Data Systems Micro-Arcsecond Imaging Mission, Pathfinder (MAXIM-PF)
Mars Data Workshop Mars Express Radio Science MaRS
Technician Licensing Class Talk to Outer Space Valid July 1, 2014 Through June 30, 2018.
Earth stations radio monitoring system of Ukraine Ukrainian State Centre of Radio Frequencies Space Radio Monitoring Station.
Basic Satellite Communication (3) Components of Communications Satellite Dr. Joseph N. Pelton.
The effective isotropic radiated power from Rosetta (HGA in X-Band) is 57 dBW At Rosetta’s current distance (2.7AU), received power in air will be -225.
From you host … Dr. H. Introduction Communications design requires us to think about the following issues: Communications design requires us to think.
Design WLAN Politeknik Telkom Design WLAN Step to design WLAN : 1. Location Survey 2. Topology 3. Distance calculating 4. Antenna design 5. Towering.
8.5 SATELLITE COMMUNICATIONS
 This chapter describes how the link- power budget calculations are made.  In this text [square] bracket are used to denote decibel quantities using.
EEE381B Pulsed radar A pulsed radar is characterized by a high power transmitter that generates an endless sequence of pulses. The rate at which the pulses.
EEE 441 Wireless And Mobile Communications
SHAHEEM TM | S7 | 24. A communications satellite exists to provide a platform in relaying of voice,video and data communications.all other subsystems.
AMSAT-SA Digital Transponder, telemetry and command system.
Dr. Yeffry Handoko Putra, M.T
Wireless Radio Technology
A study on the coexistence between Direct Air to Ground Communication (DA2GC) and Radars in the 5 GHz band Peter Trommelen, Rob van Heijster,
Satellite uplink and downlink Analysis and Design
Satellite Communications Engineering
Antennas.
Trellis Coded Modulation
Technician Licensing Class
Net425:Satellite Communications
Net425:Satellite Communications
Why do we have EIRP Limits?
Transmission Medias 2nd semester
EagleSat 2: Implementation of Improved Communications Systems on UHF Steven Buck Dr. Gary Yale, Embry-Riddle Aeronautical University Arizona Space Grant.
5G Micro Cell Deployment in Coexistence with Fixed Service
Communication Systems.
خطوط انتقال ، آنتن و انتشار امواج
Submission Title: Link Budget for m
Technician Licensing Class
EERF 6395 Navigation & Communication System for Deep Space Missions
Radio Links.
Presentation transcript:

News Nov. 2014 TX power of Rosetta is 28 W using a antenna dish sized 1.8 m The effective isotropic radiated power from Rosetta (HGA in X-Band) is 57 dBW At Rosetta’s current distance (2.7AU), the received power will be -225 dBW ESA’s New Norcia 35m station as a reference, and thanks to its 1000m2 antenna collecting surface and gain of 68 dBi Rosetta’s weak signal is captured and results in a received power of -157 dBW – just 1.8 Femto-Watts. LNA is operated at -2600 C  Noise Floor kT equals -183 dBm/Hz

News Nov. 2014 100 kHz/Div ©Bertrand Pinel, setileague.org Rosetta is presently sending signals to the ground stations at about 28 Kbps X-Band 8.421 GHz. Downlink telemetry commands 2 kbit/s, Instrument data 26 kbit/s with a square wave subcarrier of 260 kHz which is BPSK modulated Command telemetry: PM with a square wave subcarrier of 16 kHz which is BPSK modulated (high Doppler resistant)