CIPHERING & DECIPHERING UNITS
|
|
- Thomas Hawkins
- 6 years ago
- Views:
Transcription
1 CIPHERING & DECIPHERING UNITS High throughput Ciphering / Deciphering Unit Telecommand Deciphering Unit
2 HIGH THROUGHPUT CIPHERING / DECIPHERING UNIT Satellite Telecommand / Telemeasure Protection, Spreading code generation, Payload Telemetry Protection Applications Observation and Navigation satellites and mission protection Military telecommunication satellites protection Main features Communication Security: Telecommand authentication, integrity check, anti-replay protection and deciphering Communication Security: Telemetry authentication, integrity check, antireplay protection and ciphering ESA packet standard compliant Communication Security: high data rate payload telemetry authentication, integrity check, anti-replay protection and ciphering CCSDS compliant Transmission security: Spreading sequence generation TT&C signal or navigation signal Key Management In flight re-keying Secret keys injection on the launch pad Attractive Mass and Power budget Up-to-date algorithms (AES, SHA, ) or national custom made algorithms Background HELIOS1 / SPOT 4 & 5 SYRACUSE3 PLEIADES GALILEO Key benefits ESA standard interface for TC & TM Compatible with most of the LEO platforms (MIL 1553 Bus command control, primary bus, ) Standard of the shelf algorithm High throughput for payload telemetry. Technical description Deciphering Ciphering Unit Highly integrated design based on ASIC and FPGA. TC decryption channel including BCH decoding and recoding TM encryption channel including Viterbi and Reed- Solomon decoding and re-coding Payload telemetry encryption at high data rate on CCSDS VCDU frames Key injection interface for initial key loading on the launch pad Possibility of up-loading new keys in flight RS422 or RS644 interface for TC and TM RS644 parallel interface or serial-link interface (ChannelLink or HotLink) for payload telemetry. MIL 1553 interface Hot-redundancy for TC and TM Cold redundancy for payload telemetry Centralised DCDC converter with distributed power regulation Radiation hardened processor & ASICs Possibility of getting a Common Criteria accreditation after evaluation by ITSEF Possibility of getting a TEMPEST certification
3 TYPICAL PERFORMANCES Parameters Performances TC rate TM rate Payload telemetry rate TM/TC interface Power interface DC Power consumption Dimensions Thermal environment 50kbps 50kbps 600Mbps MIL STD 1553B 24 to 35 Volts range <20 Watts 430*320*255 mm 3-10/+40 C (operating) -20/+50 C (qualification) This datasheet is not contractual and can be changed without any notice Updated August 2012 For further information, please contact Thales Alenia Space France Equipment Sales Department 26 avenue J.F. Champollion B.P Toulouse Cedex 1 France Tél.: + 33(0) Fax: + 33(0) Website :
4 TELECOMMAND DECIPHERING UNIT Satellite Telecommand Protection Applications Commercial telecommunication satellites protection Main features Communication Security: Telecommand authentication, integrity check, antireplay protection and deciphering ESA packet standard compliant External cryptographic unit Substitution cryptographic unit for Attractive Mass and Power budget Up-to-date algorithms (AES, SHA, ) or national custom made algorithms Background TURKSAT WORLDSTAR EUROPSTAR EURASIASAT SYRACUSE3 KOREASAT 5 AMC23H GALAXY 17 PLEIADES Key benefits Telecommand Deciphering Unit Technical description Highly integrated design based on ASIC and FPGA. TC decryption channel including BCH decoding and re-coding RS422 interface Hot redundancy Radiation hardened processor & ASICs Possibility of getting a Common Criteria accreditation after evaluation by ITSEF Possibility of getting a TEMPEST certification ESA standard interface for TC & TM Compatible with most of the LEO platforms (MIL 1553 Bus command control, primary bus, ) Standard of the shelf algorithm and/or customisation to the operator needs High throughput for payload telemetry.
5 BLOCK DIAGRAM CDU N J109 Power supply Data in/out TMTC J108 CDU-A CDU R J209 Power supply Data in/out TMTC J208 RX A&B J101 J201 RX 1&2 RX C&D J102 J202 RX 3&4 TC TEST J107 CIU N CIU R J207 TC TEST TM TC OUT J103 J105 SEC. PWR SUPPLY TC & TM TC & TM SEC. PWR SUPPLY J203 J205 TM TC OUT BR 100V BR 100V TC LLC J104 J106 DC/DC N DC/DC R J204 J206 TC LLC ACDU TYPICAL PERFORMANCES Parameters TC rate Command Control interface Power interface DC Power consumption Dimensions Thermal environment 100kbps LLC 50 to 100 Volts range 9 Watts 230*180*110 mm 3 3kg -10/+40 C (operating) -20/+50 C (qualification) Performances This datasheet is not contractual and can be changed without any notice Updated : August 2012 For further information, please contact Thales Alenia Space France Equipment Sales Department 26 avenue J.F. Champollion B.P Toulouse Cedex 1 France Tél.: + 33(0) Fax: + 33(0) Website :
Preliminary Design of the Electrical Power Subsystem for the European Student Moon Orbiter Mission
Preliminary Design of the Electrical Power Subsystem for the European Student Moon Orbiter Mission Steve Ulrich Jean-François Veilleux François Landry Corbin Picture courtesy of ESA Presentation Outline
More informationFormation Flying Experiments on the Orion-Emerald Mission. Introduction
Formation Flying Experiments on the Orion-Emerald Mission Philip Ferguson Jonathan P. How Space Systems Lab Massachusetts Institute of Technology Present updated Orion mission operations Goals & timelines
More informationGEO Dual Mode PPU & LEO HEMPT PPU
GEO Dual Mode PPU & LEO HEMPT PPU EPIC Workshop 2018 London 15-17 Oct 1 Presentation Plan Thales Alenia Space in Belgium, previously named ETCA was created in 1963, 54 years' experience in power supplies
More informationGEO Dual Mode PPU & LEO HEMPT PPU
GEO Dual Mode PPU & LEO HEMPT PPU EPIC Workshop 2017 Madrid 24-25 Oct 1 Presentation Plan Thales Alenia Space in Belgium, previously named ETCA was created in 1963, 54 years' experience in power supplies
More informationARCHIVED REPORT. For data and forecasts on current programs please visit or call
Space Systems Forecast - Satellites & Spacecraft ARCHIVED REPORT For data and forecasts on current programs please visit www.forecastinternational.com or call +1 203.426.0800 Outlook France and Italy have
More informationThinking Outside the Cube
CHANGING THE ECONOMICS OF SPACE Thinking Outside the Cube 34 th Space Symposium Colorado Springs Monday 16 th April 2018 Anita Bernie a.bernie@sstl.co.uk Commercial in Confidence. SSTL 2017 SpaceNews Home
More informationThe DoD Space Test Program Standard Interface Vehicle (ESPA) Class Program
The DoD Space Test Program Standard Interface Vehicle (ESPA) Class Program Mr. Mike Marlow STP-SIV Program Manager Co-Authors Lt Col Randy Ripley Capt Chris Badgett Ms. Hallie Walden 20 th Annual AIAA/USU
More informationPPU MK3 FOR 5 KW HALL EFFECT THRUSTERS 11TH EUROPEAN SPACE POWER CONFERENCE
E3S Web of Conferences 16, 15001 (2017 ) PPU MK3 FOR 5 KW HALL EFFECT THRUSTERS 11TH EUROPEAN SPACE POWER CONFERENCE Eric Bourguignon, Stéphane Fraselle Thales Alenia Space Belgium, B-6032, Mont-sur-Marchienne,
More informationA Control Moment Gyro for Dynamic Attitude Control of Small Satellites
A Control Moment Gyro for Dynamic Attitude Control of Small Satellites Craig Clark Clyde Space Ltd West of Scotland Science Park, Glasgow G20 0SP; +44 141 946 4440 craig.clark@clyde-space.com Dr Kevin
More informationAirbus Defence and Space Power Processing Units: New HET and GIT PPU developments Qualification Status
Airbus Defence and Space Power Processing Units: New HET and GIT PPU developments Qualification Status IEPC-2017-266 Presented at the 35th International Electric Propulsion Conference Georgia Institute
More informationEMI INPUT FILTER 28 VOLT INPUT
FEATURES 55 to +125 C operation 28 volt input Up to 2.7 amps throughput current Up to 55 db attenuation at 500 khz Up to 60 db attenuation at 1 MHz and 5 MHz Compliant to MIL-STD-461C, CE03 Compatible
More informationDA 35/70 EFI MIL SPEC
DA 35/70 EFI MIL SPEC Electronic Fuel Injected Engines OWNER S MANUAL Table of Contents Section Page 1. General Safety 3 2. Un-Packing Your Engine 4 3. Getting Started 7 4. Maintenance 9 5. Absolute Ratings
More informationPOWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE BELGIUM (ETCA) SPC-2014
POWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE BELGIUM (ETCA) SPC-2014 Presented at the Space Propulsion 2014, 19 to 22 May 2014, Cologne, Germany Eric Bourguignon 1, Stéphane Fraselle 2, Thierry
More informationModular Reconfigurable Spacecraft Small Rocket/Spacecraft Technology Platform SMART
Modular Reconfigurable Spacecraft Small Rocket/Spacecraft Technology Platform SMART Micro-Spacecraft Prototype Demonstrates Modular Open Systems Architecture for Fast Life-Cycle Missions Jaime Esper *,
More informationARIANEGROUP ORBITAL PROPULSION ROBERT-KOCH-STRASSE TAUFKIRCHEN GERMANY
www.ariane.group ARIANEGROUP ORBITAL PROPULSION ROBERT-KOCH-STRASSE 1 82024 TAUFKIRCHEN GERMANY SUSANA CORTÉS BORGMEYER SUSANA.CORTES-BORGMEYER@ARIANE.GROUP PHONE: +49 (0)89 6000 29244 WWW.SPACE-PROPULSION.COM
More informationUSER MANUAL. 1U Solar Panel
USER MANUAL 1U Solar Panel 1 Change Log... 3 2 Acronyms List... 4 3 Description... 5 4 Product Performance and Properties... 5 4.1 Solar Panel Features and Characteristics...5 4.2 Solar Cell Features and
More informationAdrestia. A mission for humanity, designed in Delft. Challenge the future
Adrestia A mission for humanity, designed in Delft 1 Adrestia Vision Statement: To inspire humanity by taking the next step towards setting a footprint on Mars Mission Statement Our goal is to design an
More informationSB30-28 Series FEATURES DESCRIPTION
RADIATION HARDENED ISOLATED DC/DC CONERTERS SB30-28-FAMILY 28 dc In 30 Watts Total Power Single, Dual, Triple Output +2.5dc, +3.3dc, +5dc, +7dc, +12dc, +18dc DESCRIPTION The SB series of DC-DC converters
More informationCALL FOR IDEAS FOR THE RE-USE OF THE MARS EXPRESS PLATFORM PLATFORM CAPABILITIES. D. McCoy
Mars Express Reuse: Call for Ideas CALL FOR IDEAS FOR THE RE-USE OF THE MARS EXPRESS PLATFORM PLATFORM CAPABILITIES D. McCoy PARIS 23 MARCH 2001 page 1 Mars Express Reuse: Call for Ideas PRESENTATION CONTENTS
More informationSOLAR ARRAY ROOT HINGE BASED ON SHAPE MEMORY ALLOY (SMA) ACTUATOR
SOLAR ARRAY ROOT HINGE BASED ON SHAPE MEMORY ALLOY (SMA) ACTUATOR Alain BLANC (1), Damien CHASSOULIER (2), Fabrice CHAMPANDARD (3), Xavier FRANCOIS (3) (1) TAS, 5 allée des gabians - 06156 Cannes la Bocca,
More informationMichael J. Cully Director of Civil and Commercial Space Swales Aerospace Beltsville, Maryland
SSC03-IX-7 I-CONE FOR RAPID RESPONSE AND LOW COST ACCESS TO SPACE 1 Director of Civil and Commercial Space Swales Aerospace Beltsville, Maryland Peter Alea Manager of Thermal Products Swales Aerospace
More informationTHE KOREASAT5 PROGRAM
THE KOREASAT5 PROGRAM - Design, AI&T, Launch and Operation KT CORPORTION Contents I. Introduction II. Design III. Assembly, Integration and Test (AI&T) IV. Launch V. Operation VI. Q & A THE KOREASAT 5
More informationfor Critical Applications in Extreme Environments
for Critical Applications in Extreme Environments Electronic Controllers M-CONTROL Electronic Controllers provide control for systems requiring fluid pressure and flow control via pumps, fans and compressors.
More informationAlternative technologies and possible competitors in the satellite business
Allianz Global Corporate & Specialty Alternative technologies and possible competitors in the satellite business By AGCS Space Risks Department 1 Table of contents 1 2 HAPS (High Altitude Pseudo-Satellites)
More informationMars Express Bus: Simplified User Manual
Issue : Draft Rev. : 01 Date : 09/04/01 Page : i Title Mars Express Bus: Simplified User Manual Name and Function Date Signature Prepared by MARS EXPRESS team 04/01 Verified by Approved by Authorized by
More informationSpace Products. A subsidiary of Data Device Corporation
Space Products A subsidiary of Data Device Corporation QUALIFICATIONS AND CERTIFICATIONS Beta has manufactured space-qualified standard and custom products for over 15 years. This experience includes being
More informationLPT6510 Pulse-tube Cooler for K applications
1 LPT6510 Pulse-tube Cooler for 60-150 K applications R. Arts, J. Mullié, J. Tanchon 1, T. Trollier 1. Thales Cryogenics B.V., Eindhoven, The Netherlands 1 Absolut System SAS, Seyssinet-Pariset, France
More informationCHAPTER 8 LAUNCH SITE OPERATION
Launch Site Operation mainly includes: LV Checkouts and Processing; SC Checkouts and Processing; SC and LV Combined Operations. LAUNCH SITE OPERATION The typical working flow and requirements of the launch
More informationDevelopment, Qualification and Delivery Status of the HEMPT based Ion Propulsion System for SmallGEO
Development, Qualification and Delivery Status of the HEMPT based Ion Propulsion System for SmallGEO IEPC-2011-148 Presented at the 32nd International Electric Propulsion Conference, Wiesbaden Germany
More informationPENGUIN C UAS OPERATIONS & MAINTENANCE TRAINING 20 HOURS FLIGHT ENDURANCE 100KM RANGE ITAR - FREE CREW OF TWO
PENGUIN C UAS LONG ENDURANCE UNMANNED AERIAL SYSTEM 20 HOURS FLIGHT ENDURANCE OPERATIONS & MAINTENANCE TRAINING 100KM RANGE ITAR - FREE CREW OF TWO U AV FAC T O RY LT D., E U R O P E U AV FAC T O RY U
More informationDigital Power Corporation designs, manufactures, and markets highly efficient, flexible, and custom power supply solutions...
Digital Power Corporation designs, manufactures, and markets highly efficient, flexible, and custom power supply solutions...... for the medical, military, telecom, and industrial markets. 1 Advanced Custom
More informatione-smart 2009 Low cost fault injection method for security characterization
e-smart 2009 Low cost fault injection method for security characterization Jean-Max Dutertre ENSMSE Assia Tria CEA-LETI Bruno Robisson CEA-LETI Michel Agoyan CEA-LETI Département SAS Équipe mixte CEA-LETI/ENSMSE
More informationNext Steps in Human Exploration: Cislunar Systems and Architectures
Next Steps in Human Exploration: Cislunar Systems and Architectures Matthew Duggan FISO Telecon August 9, 2017 2017 The Boeing Company Copyright 2010 Boeing. All rights reserved. Boeing Proprietary Distribution
More informationSCOPE OF ACCREDITATION TO ISO/IEC 17025:2005
SCOPE OF ACCREDITATION TO ISO/IEC 17025:2005 ELITE ELECTRONIC ENGINEERING, INC. 1 1516 Centre Circle Downers Grove, IL 60515 Stephen Laya (QA Manager) Phone: 630 495 9770 ext. 119 Email: sglaya@elitetest.com
More informationSystem Testing by Flight Operators the Rosetta Experience
European Space Operations Center System Testing by Flight Operators the Rosetta Experience E. Montagnon, P. Ferri, L. O Rourke, A. Accomazzo, I. Tanco, J. Morales, M. Sweeney Spaceops 2004, Montréal, Canada,
More informationNanoRacks External Payload Platform
NanoRacks External Payload Platform Introduction NanoRacks has developed a hosted payload service, NanoRacks External Payload Platform (NREP) NREP will be installed on the JEM EF Hosted payloads will utilize
More informationMGE TM Galaxy TM 7000
MGE TM Galaxy TM 7000 Power efficiency for business continuity 160/200/250/300/400/500 kva > Performance 3 Phase Power Protection with high adaptability to meet the unique requirements of Medium to Large
More informationMIMO Zen Series. Dual Band 2x2 MIMO ac/b/g/n Enterprise Indoor Access Point 560MHz CPU / 2.4GHz at 300Mbps / 5GHz at 867Mbps
MIMO Zen Series Dual Band 2x2 MIMO 802.11ac/b/g/n Enterprise Indoor Access Point 560MHz CPU / at 300Mbps / at 867Mbps Model: MMZ344 KEY FEATURES Qualcomm Atheros 560MHz Processor AR9344 IEEE 802.11ac/a/b/g/n
More informationCHAPTER 6 ENVIRONMENTAL CONDITIONS
ENVIRONMENTAL CONDITIONS 6.1 Summary This chapter introduces the natural environment of launch site, thermal environment during SC operation, thermal and mechanical environments (vibration, shock & noise)
More informationUAV KF-1 helicopter. CopterCam UAV KF-1 helicopter specification
UAV KF-1 helicopter The provided helicopter is a self-stabilizing unmanned mini-helicopter that can be used as an aerial platform for several applications, such as aerial filming, photography, surveillance,
More informationCanisterized Satellite Dispenser (CSD) As A Standard For Integrating and Dispensing Hosted Payloads on Large Spacecraft and Launch Vehicles
Canisterized Satellite Dispenser (CSD) As A Standard For Integrating and Dispensing Hosted Payloads on Large Spacecraft and Launch Vehicles Ryan Hevner, Ryan Williams and (Presented by) Walter Holemans
More informationOshkosh Corporation MTVR On Board Vehicle Power Program Update. May 5, Built Strong. Building for the Future.
Oshkosh Corporation MTVR On Board Vehicle Power Program Update May 5, 2009 Built Strong. Building for the Future. Outline ONR OBVP Program Review Vehicle Design Aberdeen Testing Results Program Milestones
More informationMGE TM Galaxy TM 7000 GFC
MGE TM Galaxy TM 7000 GFC Grid Frequency Converter (GFC) for Shore Connection solution 500 kva Performance 3 Phase Power Protection with high adaptability to meet the unique requirements of Shore Connection
More informationSmallSats mission opportunities for the Vega launch system: the Small Spacecraft Mission Service 7 th August, 2016
SmallSats mission opportunities for the Vega launch system: the Small Spacecraft Mission Service F. Caramelli 7 th August, 2016 Vega Future Missions and Production Project Manager LAU/EVF ESRIN 1. SmallSat
More informationSolely EP based Orbit Control System on Small GEO Satellite
Solely EP based Orbit Control System on Small GEO Satellite IEPC-2007-274 30 th International Electric Propulsion Conference, Florence, Italy H. Lübberstedt *, Th. Miesner, A. Winkler OHB-System AG, D-28359
More informationSMARTSat. Shape Memory Alloy Research Technology Satellite. Allison Barnard Alicia Broederdorf. Texas A&M University Space Engineering Institute
SMARTSat Shape Memory Alloy Research Technology Satellite Allison Barnard Alicia Broederdorf Texas A&M University Space Engineering Institute Outline Introduction / Mission Objectives Systems Overview
More informationSmart Grid What is it all about? Smart Grid Scenarios. Incorporation of Electric Vehicles. Vehicle-to-Grid Interface applying ISO/IEC 15118
Corporate Technology Security Considerations for the Electric Vehicle Charging Infrastructure Rainer Falk Siemens AG, CT RTC ITS : +49 89 636 51653 : rainer.falk@siemens.com Steffen Fries Siemens AG, CT
More informationUpper Stage Evolution
Upper Stage Evolution Mark Wilkins Atlas Product Line VP United Launch Alliance AIAA_JPC080309 Copyright 2009 United Launch Alliance, LLC. All Rights Reserved. EELV Sustainment Through 2030 ULA s Evolution
More information54ACxxxx, 54ACTxxxx. Rad-hard advanced high-speed 5 V CMOS logic series. Features. Description
Rad-hard advanced high-speed 5 V CMOS logic series Features Data brief Flat-14 Flat-16 Flat-20 DIL-14 DIL-16 DIL-20 AC: 2 to 6 V operating voltage ACT: 4.5 to 5.5 V operating voltage High speed T PD =
More informationStatus & evolutions of Telemetry Services for Profiling Floats. Brice Robert Patrick Bradley (CLS America)
Status & evolutions of Telemetry Services for Profiling Floats Brice Robert brobert@cls.fr Patrick Bradley (CLS America) pbradley@clsamerica.fr COMPANY PROFILE CLS is a subsidiary of the French Space Agency
More informationMULTI-LAYER INSULATION I STRATOSPHERIC BALLOONS I ISR TETHERED BALLOONS I INFLATABLE TECHNOLOGIES RELIABLE. ADAPTABLE. MULTIPURPOSE. PERSISTENT.
MULTI-LAYER INSULATION I STRATOSPHERIC BALLOONS I ISR TETHERED BALLOONS I INFLATABLE TECHNOLOGIES RELIABLE. ADAPTABLE. MULTIPURPOSE. PERSISTENT. 1 TABLE OF CONTENTS Multi-layer insulation p.4 Stratospheric
More informationM o t o r C o n t r o l l e r s
Motor Controllers Sensitron 221 West Industry Court Deer Park, NY 11729-4681 Phone (631) 586 7600 Fax (631) 242 9798 World Wide Web - www.sensitron.com E-mail - sales@sensitron.com 146-1109 Total Motion
More informationWATTSYS Power distribution system
www.axon-cable.com WATTSYS Power distribution system WATTSYS Power distribution systems As vital components for electrical power distribution in telecommunication satellites and landbased weapon systems,
More informationLAUNCHERONE: REVOLUTIONARY ORBITAL TRANSPORT FOR SMALL SATELLITES
William Pomerantz, A.C. Charania, Steve Isakowitz, Brian Morse, Kevin Sagis 13 August 2013 LAUNCHERONE: REVOLUTIONARY ORBITAL TRANSPORT FOR SMALL SATELLITES 2 VG Overview World s first spaceline Privately
More informationCHAPTER 2 GENERAL DESCRIPTION TO LM-3C
GENERAL DESCRIPTION TO LM-3C 2.1 Summary Long March 3C (LM-3C) is developed on the basis of LM-3A launch vehicle. China Academy of Launch Vehicle Technology (CALT) started to design LM-3A in mid-1980s.
More informationElectronic Test Fuze. Hamish Malin. NSWCDD G33 Precision and Advanced Systems Branch
Electronic Test Fuze Hamish Malin NSWCDD G33 Precision and Advanced Systems Branch Program Overview Electronic Test Fuze (ETF) designed to support Guidance Integrated Fuze (GIF) program GPS SAASM Receiver
More informationLUNAR INDUSTRIAL RESEARCH BASE. Yuzhnoye SDO proprietary
LUNAR INDUSTRIAL RESEARCH BASE DESCRIPTION Lunar Industrial Research Base is one of global, expensive, scientific and labor intensive projects which is to be implemented by the humanity to meet the needs
More informationThe current issue is the electronic copy available through SPRINT on line. All paper copies are for information only.
The current issue is the electronic copy available through SPRINT on line. All paper copies are for information only. Page 2 of 8 CONTENTS 2.1 Introduction... 3 2.2 Scope... 3 2.3 Guidelines... 3 3 Applicable
More informationSPARTAN. Date: All rights reserved 2011, Thales Alenia Space. Business Unit Space Infrastructures & Transportation
SPARTAN Date: Business Unit Space Infrastructures & Transportation February the 17 2011 All rights reserved 2011, Thales Alenia Space Project Overview 2 From 3 rd Fp7 Space Call Grant Agreement n. 262837
More informationPOWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE BELGIUM (ETCA) SPACE PROPULSION 2016 MARRIOTT PARK HOTEL, ROME, ITALY / 2 6 MAY 2016
POWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE BELGIUM (ETCA) SPACE PROPULSION 2016 MARRIOTT PARK HOTEL, ROME, ITALY / 2 6 MAY 2016 Eric Bourguignon (1), Stéphane Fraselle (2), Thierry Scalais
More informationSCOPE OF ACCREDITATION TO ISO/IEC 17025:2005
SCOPE OF ACCREDITATION TO ISO/IEC 17025:2005 ELITE ELECTRONIC ENGINEERING, INC. 1 1516 Centre Circle Downers Grove, IL 60515 Larry Brooks (QA Manager) Phone: 630 495 9770 ext. 166 Email: lbrooks@elitetest.com
More informationUSA DELTA DELTA Mc DONNELL DOUGLAS SPACE SYSTEMS
1. IDENTIFICATION 1.1 Name DELTA 2-6925 1.2 Classification Family : DELTA Series : DELTA 2 Version : 6925 Category : SPACE LAUNCH VEHICLE Class : Medium Launch Vehicle (MLV) Type : Expendable Launch Vehicle
More informationU- Pilot User Manual -
V 1.30 2017/04/05 U- Pilot User Manual - Table of Contents 1 General System troduction...3 1.1 Concept of system operation...4 2 Controllable Air vehicles...5 2.1 Fixed wing...5 2.1.1 Conventional configuration
More informationAMSAT-NA FOX Satellite Program
AMSAT-NA FOX Satellite Program Review, Status, and Future JERRY BUXTON, NØJY, AUTHOR AMSAT VP-ENGINEERING Review FOX-1 - WHY IT IS, WHAT IT IS Fox Development Strategy Take advantage of large and growing
More informationThinking Outside the Cube
Thinking Outside the Cube Anita Bernie 1, Alex da Silva Curiel 1, Nikki Antoniou 1, Luis Gomes 1, Rob Goddard 1, Jonathan Friend 1, Sir Martin Sweeting 2 1) Surrey Satellite Technology Ltd., Tycho House,
More informationr bulletin 96 november 1998 Figure 1. Overall ATV configuration (ESA/D. Ducros)
r bulletin 96 november 1998 Figure 1. Overall ATV configuration (ESA/D. Ducros) atv The Automated Transfer Vehicle P. Amadieu Head of ATV/CTV Projects Division, ESA Directorate of Manned Spaceflight and
More informationCHAPTER 8 LAUNCH SITE OPERATION
8.1 Briefing to Launch Site Operation Launch Site Operation mainly includes: LV Checkouts and Processing; SC Checkouts and Processing; SC and LV Combined Operations. LAUNCH SITE OPERATION The typical working
More informationSPACE LOW DISTURBANCE TECHNOLOGY LOW DISTURBANCE TECHNOLOGY
SPACE LOW DISTURBANCE TECHNOLOGY LOW DISTURBANCE TECHNOLOGY ONE MOOG For more than 60 years, Moog Space has been developing control solutions to meet the demanding requirements of our customers and the
More informationLi-ion battery and super-capacitor Hybrid energy system for low temperature SmallSat applications
Li-ion battery and super-capacitor Hybrid energy system for low temperature SmallSat applications K.B. Chin*, M.C. Smart, E.J. Brandon, G.S. Bolotin, N.K. Palmer Jet Propulsion Laboratory, California Institute
More informationDevelopment of a Low Cost Suborbital Rocket for Small Satellite Testing and In-Space Experiments
Development of a Low Cost Suborbital Rocket for Small Satellite Testing and In-Space Experiments Würzburg, 2015-09-15 (extended presentation) Dr.-Ing. Peter H. Weuta Dipl.-Ing. Neil Jaschinski WEPA-Technologies
More informationMedium Rate Hybrid Pouch Cell
LCF-134 Medium Rate Hybrid Pouch Cell Li/CF x -MnO 2 Hybrid Highly reliable, lightweight cell with 2X the capacity of Li-SO 2 and impressive rate capability over a wide temperature range. Features & Benefits
More informationDeployment and Drop Test for Inflatable Aeroshell for Atmospheric Entry Capsule with using Large Scientific Balloon
, Germany Deployment and Drop Test for Inflatable Aeroshell for Atmospheric Entry Capsule with using Large Scientific Balloon Kazuhiko Yamada, Takashi Abe (JAXA/ISAS) Kojiro Suzuki, Naohiko Honma, Yasunori
More informationELECTRIC PROPULSION: EUTELSAT STANDPOINT
ELECTRIC PROPULSION: EUTELSAT STANDPOINT COSMO CASAREGOLA EPIC Electric Propulsion Innovation & Competitiveness 24-25 October 2017, Madrid EUTELSAT: A KEY PLAYER IN THE SPACE BUSINESS Pioneer in space
More informationLEOSTAR A Small Spacecraft for LEO Communication Missions. (1) G. Barresi - (1) G. Rondinelli - (1) C. Soddu (2) D. 1. Brown
LEOSTAR A Small Spacecraft for LEO Communication Missions (1) G. Barresi - (1) G. Rondinelli - (1) C. Soddu (2) D. 1. Brown (1) TALSPAZO Consorzio ndustriale per e Attivita Spaziali Via V.E. Orlando, 83-00185
More informationVoltage B = 50 C = 100. Temperature Characteristic
MIL-PRF-123 HOW TO ORDER Military Type Designation: Capacitors, Fixed, Ceramic Dielectric, (Temperature Stable and General Purpose), High Reliability M123 A 01 BX B 103 K C Mil-Spec Number Modification
More informationLinear Line Voltage LED Engine
Linear Line Voltage LED Engine Product Specification Introduction The TERRALUX Linear LED Engine is a fully integrated, self-contained, plug-and-play LED solution for lighting fixture manufacturers and
More informationWIDE TEMPERATURE RANGE PLANAR POWER SUPPLIES AND CONVERTERS
WIDE TEMPERATURE RANGE PLANAR POWER SUPPLIES AND CONVERTERS AC/DC Power supplies series JETA Standard input: 230 VAC, 115 VAC range: up to -50 C...+85 C Output Power: from 60W to 3000W Metal Case Efficiency
More informationCHAPTER 1 INTRODUCTION
CHAPTER 1 INTRODUCTION The development of Long March (LM) launch vehicle family can be traced back to the 1960s. Up to now, the Long March family of launch vehicles has included the LM-2C Series, the LM-2D,
More informationD.A. Barnhart*, J.M. McCombet, D.L. Tilley$ Air Force Phillips Laboratory Edwards A.F.B., CA
131 IEPC-93-011 ELECTRIC PROPULSION INTEGRATION ACTIVITIES ON THE MSTI SPACECRAFT D.A. Barnhart*, J.M. McCombet, D.L. Tilley$ Air Force Phillips Laboratory Edwards A.F.B., CA "Chief, Spacecraft Design
More informationSilvertel. Ag Features. 2 Description. Power-Over-Ethernet Module. IEEE802.3af compliant. Small SIL package size - 56mm (L) x 14mm (H) Low cost
Silvertel V2.5 Feb 2014 Datasheet Pb 1 Features IEEE802.3af compliant Small SIL package size - 56mm (L) x 14mm (H) Low cost Input voltage range 36V to 57V Minimal (low cost) external components required
More information3GPP TS V ( )
TS 26.453 V13.0.0 (2016-03) Technical Specification 3rd Generation Partnership Project; Technical Specification Group Services and System Aspects; Speech codec speech processing functions; Codec for Enhanced
More informationMIMO Zen Series. Dual Band 3x3 MIMO ac/b/g/n High Bandwidth Indoor Access Point 700MHz CPU / 2.4GHz at 450Mbps / 5GHz at 1300Mbps
MIMO Zen Series Dual Band 3x3 MIMO 802.11ac/b/g/n High Bandwidth Indoor Access Point 700MHz CPU / at 450Mbps / at 1300Mbps Model: MMZ558 KEY FEATURES Qualcomm Atheros 700MHz Processor QCA9558 IEEE 802.11ac/a/b/g/n
More informationFlexCore Low-Cost Attitude Determination and Control Enabling High-Performance Small Spacecraft
FlexCore Low-Cost Attitude Determination and Control Enabling High-Performance Small Spacecraft Dan Hegel Director, Advanced Development Blue Canyon Technologies hegel@bluecanyontech.com BCT Overview BCT
More informationHewlett-Packard Company 5400/8200 zl Switch Series. FIPS Non-Proprietary Security Policy
Hewlett-Packard Company 5400/8200 zl Switch Series Module Name: HP Networking 5400 zl [1,2] and 8200 zl [3,4] Switch Series Hardware Versions: 5406 zl [1] 5412 zl [2], 8206 zl [3], 8212 zl [4] [A]; Switches:
More informationFirst results and next steps in Kazakhstan Earth Observation missions in cooperation with SSTL
First results and next steps in Kazakhstan Earth Observation missions in cooperation with SSTL M.Moldabekov (1), M.Nurguzhin (2), V.Ten (3), S.Murushkin (3), H.Lambert (3), A.da Silva Curiel (4), D.King
More informationCATERPILLAR 3516B DP2 System
CATERPILLAR 3516B DP2 System CONTENTS System Overview 3 Offshore Rig or Ship DP2 Package 3 Main Generator Diesel Skid 3 Main Generator Diesel Engines 3 Instrument, Alarms and Automatic Start/Stop System
More informationMIMO Zen Series. Dual Band 3x3 MIMO ac/b/g/n High Bandwidth Indoor Access Point 700MHz CPU / 2.4GHz at 450Mbps / 5GHz at 1300Mbps
MIMO Zen Series Dual Band 3x3 MIMO 802.11ac/b/g/n High Bandwidth Indoor Access Point 700MHz CPU / at 450Mbps / at 1300Mbps Model: MMZ558 KEY FEATURES Qualcomm Atheros 700MHz Processor QCA9558 IEEE 802.11ac/a/b/g/n
More informationExomars Orbiter Module Bus OMB
Exomars Orbiter Module Bus OMB TAS-F 23rd Sept 2010 Exomars Industrial day- Turin 1 Exomars OMB definition Exomars OMB will: serve as a carrier to deliver the EDM at the right landing latitude in the 2016
More informationTurret Systems SOLUTIONS TM. and Accessories Catalog
23 CONTROL SOLUTIONS TM Turret Systems and Accessories Catalog 2016 978 Control Solutions has been providing military systems for over 20 years. We are one of the first companies to provide heavy turret
More informationMIMO Zen Series. Dual Band 3x3 MIMO ac/b/g/n High Bandwidth Indoor Access Point 775MHz CPU / 2.4GHz at 450Mbps / 5GHz at 1300Mbps (Wave-2)
MIMO Zen Series Dual Band 3x3 MIMO 802.11ac/b/g/n High Bandwidth Indoor Access Point 775MHz CPU / at 450Mbps / at 1300Mbps (Wave-2) Model: 3x3 MMZ563 KEY FEATURES Qualcomm Atheros 775MHz Processor QCA9563
More informationDEFENSE AND AEROSPACE GUIDE
DEFENSE AND AEROSPACE GUIDE WWW.THERMISTOR.COM ABOUT QTI QTI is a privately-held manufacturer of temperature sensors and assemblies. Founded in 977, we have grown to be the trusted supplier of temperature
More informationDESIGN AND TEST OF THE PAYLOAD ELECTRONICS & IN FLIGHT SEQUENCE DEVELOPMENT FOR THE CSUN CUBESAT1 LOW TEMPERATURE BATERY EXPERIMENT
DESIGN AND TEST OF THE PAYLOAD ELECTRONICS & IN FLIGHT SEQUENCE DEVELOPMENT FOR THE CSUN CUBESAT1 LOW TEMPERATURE BATERY EXPERIMENT G.S. Bolo>n* K.B. Chin, M.C. Smart, E.J. Brandon, N.K. Palmer Jet Propulsion
More informationNanoPower P31u / P31uX Datasheet Electric Power System for mission critical space applications with limited resources
NanoPower P31u / P31uX Datasheet Electric Power System for mission critical space applications with limited resources 1 Table of Contents 1 TABLE OF CONTENTS... 2 2 OVERVIEW... 3 2.1 HIGHLIGHTED FEATURES...
More informationELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS
MIL-STD-1539 (USAF) 1 AUGUST 1973 MILITARY STANDARD ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS FSC 1810 Electrical Power, Direct Current, Space Vehicle Design Requirements MIL-STD-1539
More informationInvestigation of timing constraints violation as a fault injection means. ZUSSA Loïc, DUTERTRE Jean-Max, CLEDIERE Jessy, ROBISSON Bruno, TRIA Assia
Investigation of timing constraints violation as a fault injection means ZUSSA Loïc, DUTERTRE Jean-Max, CLEDIERE Jessy, ROBISSON Bruno, TRIA Assia Context Timing constraints of synchronous digital IC Timing
More informationAN OPTIMIZED PROPULSION SYSTEM FOR Soyuz/ST
1 RD-0124 AN OPTIMIZED PROPULSION SYSTEM FOR Soyuz/ST Versailles, May 14,2002 Starsem Organization 2 35% 25% 15% 25% 50-50 European-Russian joint venture providing Soyuz launch services for the commercial
More informationPhilae : A made to measure battery. Richard Hague ESTEC AIM Workshop 22/23 Feb 2016
Philae : A made to measure battery Richard Hague ESTEC AIM Workshop 22/23 Feb 2016 Agenda 1 SAFT s Space Heritage 2 Philae 3 ExoMars Rover AIM 2 presnetation 1 SAFT S SPACE HERITAGE 3 Space Satellites
More informationDeployment and Flight Test of Inflatable Membrane Aeroshell using Large Scientific Balloon
1 Deployment and Flight Test of Inflatable Membrane Aeroshell using Large Scientific Balloon Kazuhiko Yamada, Takashi Abe (JAXA/ISAS) Kojiro Suzuki, Naohiko Honma, Yasunori Nagata, Masashi Koyama (The
More informationThe ATV Programme "Jules Verne"
Nicholas Camussy The ATV Programme "Jules Verne" Ein Vortrag organisiert vom VDI in Kooperation mit DGLR und RAeS 16.02.2009 Hochschule für Angewandte Wissenschaften Hamburg Download: http://hamburg.dglr.de
More informationSilvertel. Ag Features. 2. Description. Power-Over-Ethernet Module for CCTV. IEEE802.3af compliant
Silvertel V2.4 August 202 Datasheet Pb. Features IEEE802.3af compliant Standard CCTV package sizes - 38mm x 38mm x 6mm (H) or 42mm x 42mm x 6mm (H) Low cost Input voltage range 36V to 57V Input diode bridges
More information