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Thu, 25 Aug 2016 23:28:00 +0100
NASA has selected United Launch Services LLC of Centennial, Colorado, to provide launch services for a mission that will address high-priority science goals for the agency's Journey to Mars. Mars 2020 is targeted for launch in July 2020 aboard an Atlas V 541 rocket from Space Launch Complex 41 at Cape Canaveral Air Force Station in Florida. The rover will conduct geological assessments of its landing site on Mars, determine the habitability of the environment, search for signs of ancient Mart...
Thu, 25 Aug 2016 22:44:00 +0100
NASA has awarded the Next Generation Land Mobile Radio contract to Motorola Solutions, Inc., of Linthicum Heights, Maryland. This is a firm-fixed-price contract with indefinite-delivery/indefinite-quantity (IDIQ) components. The contract has a one-year base period, beginning Sept. 1, and four one-year options that total approximately $1.8 million. The IDIQ portion of the contract has a maximum value of $7.3 million. The total contract value, including all options, is approximately $9.1 millio...
Thu, 25 Aug 2016 21:00:00 +0100
Boeing has delivered one of the world's most advanced satellite communications systems to Mexico, one that opens high-speed data and voice communications to the entire country including some previously unserved areas. After successfully completing its final tests, the Mexsat system was today formally accepted by the Ministry of Communications and Transportation. Mexsat provides 3G+ voice and data services to mobile terminals on land, air and sea, enhancing the country's national security, ...
Thu, 25 Aug 2016 01:00:00 +0100
An Ariane 5, operated by Arianespace, has delivered two telecom satellites, Intelsat-33e and Intelsat-36, into their planned orbits. Liftoff of flight VA232 occurred on 24 August at 22:16 GMT (19:16 local time, 00:16 CEST on 25 August) from Europe's Spaceport in Kourou, French Guiana. Intelsat-33e, with a mass at liftoff of 6600 kg and mounted in the upper position atop Ariane's Sylda dual-payload carrier inside the fairing, was the first to be released about 28 minutes into the mission. ...
Tue, 23 Aug 2016 16:00:00 +0100
When it comes to transmitting sensitive information in highly contested areas, the Advanced Extremely High Frequency (AEHF) system and Milstar satellites are proving their value, achieving 100 years of combined successful operations. Designed as a protected, global network, the first Milstar launched in 1994 aboard a Titan IV rocket. Since then, the constellation has served as a critical resource for troops and national leaders in delivering secure and reliable communications. In 2010, the fi...
Mon, 22 Aug 2016 14:00:00 +0100
Northrop Grumman Corporation (NYSE:NOC) has been awarded a contract from OHB System AG to supply the space inertial reference system for Germany's SARah satellite-based radar reconnaissance system. Northrop Grumman will supply its Scalable Space Inertial Reference Unit-L (Scalable SIRU(tm)-L) for sensor pointing/stabilization and attitude control on the SARah satellite-based radar reconnaissance system. This contract marks the first international application of the new Scalable SIRU(tm)-L con...
Mon, 22 Aug 2016 09:37:00 +0100
Every 18 months or so, scientists and sensation-seekers gather at set points on Earth's surface, to await awe-inspiring solar eclipses. The Moon briefly blocks the Sun, revealing its mysterious outer atmosphere, the corona. Though what if researchers could induce such eclipses at will? That's the scientific vision behind ESA's double-satellite Proba-3, the world's first precision formation-flying mission, planned for launch in 2019. An 'occulter' satellite will fly 150 m ahead of a second...
Fri, 19 Aug 2016 16:46:00 +0100
Orbital ATK, a global leader in aerospace and defense technologies, announced today that two satellites the company designed, built and tested for the U.S. Air Force were successfully deployed following their launch aboard a United Launch Alliance (ULA) Delta IV rocket from Cape Canaveral Air Force Station, Florida, on August 19, 2016. The satellites were the third and fourth for the Geosynchronous Space Situational Awareness Program (GSSAP) and comprise Air Force Space Command Mission Number Si...
Fri, 19 Aug 2016 13:51:00 +0100
A United Launch Alliance (ULA) Delta IV rocket carrying the AFSPC-6 mission for the United States Air Force lifted off from Space Launch Complex-37 Aug. 19 at 12:52 a.m. EDT. This is ULA's seventh launch in 2016 and the 110th successful launch since the company was formed in December 2006. "Thank you to the ULA, Air Force and industry partners for the outstanding teamwork and flawless execution that made today's mission a success," said Laura Maginnis, ULA vice president of Custom Services. "...
Thu, 18 Aug 2016 10:34:00 +0100
An ESA tracking station has acquired signals from the international Cassini spacecraft orbiting Saturn, across more than 1.4 billion km of space. Following a seven-year journey to Saturn, the NASA/ESA/ASI Cassini orbiter delivered Europe's Huygens probe to the surface of Saturn's mysterious moon Titan in January 2005, just a few months after becoming the first spacecraft to enter orbit around the giant gas planet. Since then, Cassini and Huygens have returned a wealth of information on the...
Wed, 17 Aug 2016 21:06:00 +0100
NASA is preparing to launch its first mission to return a sample of an asteroid to Earth. The mission will help scientists investigate how planets formed and how life began, as well as improve our understanding of asteroids that could impact Earth. The Origins, Spectral Interpretation, Resource Identification, Security-Regolith Explorer (OSIRIS-REx) spacecraft will travel to the near-Earth asteroid Bennu and bring a sample back to Earth for intensive study. Launch is scheduled for 7:05 p.m. E...
Wed, 17 Aug 2016 11:28:00 +0100
The miniature satellites known as CubeSats already play a variety of roles in space. In future they could also serve as the building blocks of other, larger missions by being docked together in orbit. CubeSats are nanosatellites of standardised dimensions based on multiple 10-cm-sided cubes, which ESA is employing for both educational and technology-demonstration purposes. "The ability to autonomously rendezvous and dock CubeSats could enable in-orbit assembly of larger structures that sim...
Tue, 16 Aug 2016 20:00:00 +0100
Astro Aerospace, a Northrop Grumman Corporation (NYSE:NOC) company, has completed the preliminary design review (PDR) of the AstroMesh(r) radar antenna reflector for the NASA-ISRO Synthetic Aperture Radar (NISAR) satellite. The antenna reflector, furnished by Astro Aerospace, is part of the NISAR L-band synthetic aperture radar managed by NASA's Jet Propulsion Laboratory. Scheduled to launch in 2021, NISAR will be the first radar imaging satellite to use dual L-Band and S-Band frequencies, pr...
Tue, 16 Aug 2016 08:34:00 +0100
Dark matter, the mysterious substance that constitutes most of the material universe, remains as elusive as ever. Although experiments on the ground and in space have yet to find a trace of dark matter, the results are helping scientists rule out some of the many theoretical possibilities. Three studies published earlier this year, using six or more years of data from NASA's Fermi Gamma-ray Space Telescope, have broadened the mission's dark matter hunt using some novel approaches. &...
Mon, 15 Aug 2016 15:00:00 +0100
Space Systems Loral (SSL), a leading provider of innovative satellites and spacecraft systems, today announced that a satellite designed and built for SKY Perfect JSAT Corporation , a leading satellite operator based in Japan , was launched on Saturday night and is successfully performing post-launch maneuvers according to plan. The satellite, JCSAT-16, deployed its solar arrays on schedule following the SpaceX Falcon 9 launch from Cape Canaveral Air Force Station in Florida . JCSAT-16, which wi...
Fri, 12 Aug 2016 08:31:00 +0100
A pioneering Earth observation satellite for Peru has made initial contact with launcher hardware as PerúSAT-1 completes its fit-check in preparation for a September 16 liftoff from French Guiana aboard an Arianespace Vega launch vehicle. The fit-check is a regular milestone during mission preparations at Arianespace’s Spaceport launch site in French Guiana, verifying the physical matchup of a payload with the hardware that serves as its interface when integrated on the launche...
Thu, 11 Aug 2016 11:00:00 +0100
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Wed, 10 Aug 2016 22:33:00 +0100
Today global technology leader Lockheed Martin (NYSE: LMT), the UAE Space Agency and Mubadala launched a space-based workforce training program to develop emerging leaders in the UAE space industry. Generation Space: The Space Fundamentals Training Program for early career professionals across the UAE aerospace industry will run for the next four months and includes training in the UAE and the United States. The program begins in the UAE with training in "space foundations" and moves into mor...
Wed, 10 Aug 2016 13:25:00 +0100
A new micro-size cryocooler from Lockheed Martin (NYSE: LMT) is enabling quick-startup infrared (IR) sensors for missile and sensor applications. Cryocoolers are standard components in IR-sensing platforms, from space observation to weapons targeting, and this new highly-compact product enables faster activation and smaller packaging. "The Fast Cool Down Microcryocooler makes sure our military can have rapid-reaction systems, from missile to passive sensor applications," said Dr. Jeffrey Olso...
Wed, 10 Aug 2016 12:00:00 +0100
The small smattering of bright blue stars in the upper left of this vast new 615 megapixel ESO image is the perfect cosmic laboratory in which to study the life and death of stars. Known as Messier 18 this star cluster contains stars that formed together from the same massive cloud of gas and dust. This image, which also features red clouds of glowing hydrogen and dark filaments of dust, was captured by the VLT Survey Telescope (VST) located at ESO's Paranal Observatory in Chile. Messier 18 w...
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    Personal information
     Name:<withheld>
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    Contact information
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    Candidate Profile
     Date Submitted:24-03-2011
     Last Modified:09-12-2014 (01:12)
    Job information
     Current job:Aerospace Avionic Systems Engineer
     Employment Term:Permanent
     Job location:Anywhere
     Date available:immediately
     Industry:Civil Agencies/International Organizations, Satellite Manufacturers and Subcontractors, Satellite Operators, , , Launch Systems, Consulting/Engineering Services
     KeywordsProject Management (RUP, Scrum, Agile, Work Package Definition, Risk Analysis) Process Engineering (CMMI Level 3/4)) Requirements / Business Process Analysis (RDD, BPMN) System Modeling & Design (SCADE, Simulink, SysML, UML, OOA, OOD, TDD, HOOD) SW /
    CV

    Personal

    Date of Birth  9 November 1965

    Place of Birth London, England

    Marital Status Single

    Nationality  British

    Gender  Male


    Summary

    * Mission & Safety Critical Software & Hardware Systems Engineer - Aerospace, Spacecraft & Mechatronic Systems

    * Aircraft Software & Hardware Systems Development, Integration & Test Engineer:
    ° Airbus A350 XWB, A380, & A400M, Eurofighter, Merlin Anti-Submarine Helicopter, ASTOR Sentinel R1 Aircraft.

    * Spacecraft Software, Hardware & AIT & V Systems Engineer:
    ° QinetiQ STRV a & b, & TopSat Spacecraft; ESA Cluster, GOCE, ATV, GAIA, & Euclid Spacecraft.

    * Spacecraft Systems Design & Research Engineer:
    ° QinetiQ UK-10 Ion-Thruster, ESA Solar-Wind Plasma Characterisation, Galactic Astrometry, Cometary Fragmentation Analysis, Robotics & Mechatronics.

    Specialties:
    * Project Management (RUP, Scrum, Agile, Work Package Definition, Risk Analysis)
    * Process Engineering (CMMI Level 3/4))
    * Requirements / Business Process Analysis (RDD, BPMN)
    * System Modelling & Design (SCADE, Simulink, SysML, UML, OOA, OOD, TDD, HOOD) * SW / Algorithm Development (MATLAB, MISRA C, C++, Assembler, STL, Boost)
    * Safety Critical SW & HW (DO-178B, DO-254, FAA / EASA certification, FMECA)
    * Embedded SW (PLC, Microcontroller, Device Driver, BSP, RTOS, Embedded Linux)
    * Data Analysis (MATLAB, IDL, Fortran, Monte Carlo Simulation)
    * EMI, EMC (Def Stan 59-41, MIL-STD-461 / 462 / 464), TEMPEST (AMSG 720B)
    * Spacecraft Systems Development (ESA ECSS-E40, ESA PSS-05, ECSS-Q-80)

     

    Education

    PhD, Cometary Dust Particle Fragmentation with Rosetta GIADA Instrument, 2014, Planetary & Space Science Research Institute (PSSRI)

    BSc (Hons) Class 2.1 Physical Science, 2010, Open University Milton Keynes

    BSc (Hons) Class 2.1 Information Technology & Computing, 2005, Open University Milton Keynes

    MSc, Astronautics & Spacecraft Engineering, 1992, College of Aeronautics, Cranfield University

    Her Majesty’s Commission, 1989, Royal Air Force College Cranwell

    BSc (Hons) Class 2.2, 1988, Department of Physics, Leeds University

     

    Professional Experience

    Altran AG, Zurich
    November 2010 – Present

    ESA Euclid Spacecraft - Solid State Mass Memory (SSMM) Design & Development:
    * Specify & design SSMM architecture & Spacecraft Command & Data Management Unit (CDMU) Interfaces
    * Specify system development processes
    * Define SW / HW production tool chain
    * Define & verify SW / HW required input's availability & consistency
    * Define HW, SW / FPGA Interfaces (ICDs)
    * Define, develop data compression & storage algorithms
    * Develop HW, embedded SW & FPGAs
    * Define HW, SW & FPGA AIV & AIT processes
    * Specify, design & develop Ground Support Equipment (GSE).
    * Define system Modelling & Simulation methodology & trade-offs

    Robotic Laboratory Analysis Workstation: Sub-system SW Engineer:
    * Specification, design, implementation and test of mechatronic sub-systems:
    ° 3-axis motion controlled arm & gripper, Optical scanner & sample analyser, Centrifuge, Sample incubator, Liquid handling system.
    * Design, development of servo-motor and actuator control algorithms and position encoding.
    * Integration and programming of sensors:
    ° 3-axis accelerometer, Reflected & ambient optical, Touch, 1-axis gyro, Temperature,Ultrasonic. * System & Sub-system testing and test automation,
    * Preparation of Requirement-Test Analysis & Failure Modes Effect Analysis (FMEA) for FDA approval,
    * Team Foundation Server, Enterprise Architect, HP Quality Centre, Wireshark, LabVIEW, Subversion, C++, PCD XML,
    * PLC S7, AS-i, Industrial Ethernet, RT protocol for PROFINET CBA and PROFINET IO.

    ALFApump & SmartCharger SW Engineer:

    * Development, implementation of embedded firmware & boot-loader, MISRA C, Assembler, * Integration of uBlox LEON-G100 GSM/GPRS Modem,
    * Implementation of 2-wire interface for SHT1x Humidity Sensor,
    * Implementation of i2C protocol between ARM7 (SAM7X256) microcontroller, LPS331AP pressure sensor & DS2764 battery monitor,

    * Setup of development, integration, & test bench,
    * Protocol testing using Agilent MSO 6034A Oscilloscope,
    * Preparation of development & integration training materials,
    * System & Sub-system testing and test automation,
    * Preparation of Requirement-Test Analysis & Failure Modes Effect Analysis (FMEA) for FDA approval,
    * Keil uVision4 IDE, MISRA C, Surround SCM, Beyond Compare, TestTrack, Doxygen,
    * E3633A PSU, JTAG, Rohde & Schwarz Digital Radio GSM Test Set. Wavetek Protocol Analyser.

     

    Airbus, Germany
    January 2009 – October 2010
    Airbus A350 XWB, A380, & A400M Integrated Modular Avionics (IMA) System Engineer
    :

    * Design, development of IMA system:

    ° Arinc 600 MCU, Common Remote Data Concentrator (CRDC), Core Processing & Input / Output Module (CPIOM), & Input / Output Module (IOM)
    * Design, development of avionics communications network system:

    ° Arinc 429, AFDX.
    * Design, development of Switching Table configuration software & process:

    ° Data base data extraction, Network Configuration Description generation, Configuration Check, Configuration load for switches.
    * Integration, configuration of CPIOM SW:

    ° Boot SW, Drivers, Arinc 653 Operating System. * Development of Test Bench:

    ° Data translation tools, automated test suite, test harnesses.
    * Software integration & test on Host (HBOSS), & on Representative Target (TBOSS), * Author / Technical Editor of IMA system Reference Manuals & User Manuals,
    * Subcontractor/supplier management and coordination.

    AFDX DO-178-B Linux Software Engineer:

    * Development, maintainance of Embedded Linux BSPs, & Boot Loader Firmware,
    ° Scheduling, interrupt subsystem, concurrency, logical and physical memory management.
    * Development of (2.6 series device driver model) Device Drivers:
    ° Optimisation, bug fixing & adding new functionality.
    * Implementation & integration of interfaces & protocols:
    ° I2C, SPI, UART, USB, AFDX, PCI Express.
    * Documentation control for hardware schematics, & datasheets,
    * Protocol testing using oscilloscope, logic analyser, and bus protocol analysers,
    * Porting of third party software libraries,
    * Development, customisation of software tools & utilities (from free/open source and scratch), * Writing shell scripts for source code patching under Clearcase
    * C, Clearcase, ARM7
    * ARM Development Studio 5:
    ° Eclipse IDE, GNU cross-compiler, DS-5 debugger, Streamline performance analyser.

     

    Astrium, Stevenage UK
    January 2008 – December 2008
    GAIA Spacecraft Video Processing Unit (VPU) Hardware / Software Integration & Test Engineer:

    * Integration and configuration of focal plane control computer board and software.
    * Configuration of BSP and focal plane control computer boot software.
    * Integration and configuration of communications protocols and VPU start-up software.
    * Design and development of Ground Support Equipment (GSE).
    * Design and implementation of test and test automation software.
    * Focal plane array integration & test @ Astrium, Toulouse.
    * Spacewire (ECSS-E-ST-50-12C), Maxwell SCS750, IBM 750FX, cPCI v2.2, RS422, MIL-STD 1553
    * C, VxWorks 5.5 BSP, C++, XML, Tornado, Eclipse

    GAIA is an ESA mission to:
    * Measure positions of ~1 billion galactic and local-group stars with accuracy ~20 μas,
    * Perform spectral and photometric measurements of all objects,
    * Derive space velocities of Galaxy's constituent stars using stellar distances and motions, * Create a 3D structural map of the Galaxy.

     

    Airbus, Germany
    April 2002 - December 2007
    Airbus A400 Aircraft Mission Management System (MMS) Software Engineer:
    * Design, development of Mission Data Management Subsystem (DO-178B, DO-254) DAL C,
    * Design, development of Navigation Subsystem (DO-178B, DO-254) DAL C,
    * Design, implementation of Navigational Data Model,
    * Integration of Flight Management Computer Display Unit & Embedded GPS/INS,
    * Design, implementation of Tactical Navigation Data Retrieval Subsystem,
    * Design, development of Pilot Assistance System 4D flight control subsystem,
    • Design, implementation of EGI Navigational Data 1553 Controller for Tactical Display,
    * Design, implementation of Missile Warning System Passive Element (MWS-PE) (DO-178B, DO-254) DAL C,
    * DOORS. Rhapsody, UML, SCADE, C++, MISRA C, GCC, Greenhills Integrity. eXtreme dB,
    * PVCS, Eclipse IDE, ADS2 Simulation, VxWorks, MIL-STD 1553B & Arinc 429, Arinc 653.

    Digital Electronic Control and Monitoring Unit (DECMU) Software Engineer:

    * Safety critical software design, implementation to DO-178B DAL A,
    * Hardware & Software Integration testing for DECMU to DO-254,
    * Writing utilities to communicate with target hardware for HSI test scripts,
    * Ensuring tool chain compliance with European Aviation Safety Agency (EASA) regulations, * Leading end of software life-cycle certification activities,
    * Requirements analysis for tool chain certification,

    * MatLab, Simulink, SCADE, DOORS 6.0, TI Code Composer cross compiler, C.

    Eurofighter - Radar Test & Ground Support Equipment Engineer:

    * Development, implementation of Radar Data Generator & Scenario Replay Facility
    ° Simulates IQ returns of various targets, differing operational conditions, weather effects.
    ° Scenarios definition, Range profile extraction, Doppler processing, Sensor coverage analysis, Multiple simultaneous target injections.
    * Measurement the radar performance for different scenarios,
    * Characterization of radar receiver designs.

     

    Astrium
    July 1999 – April 2002
    Automated Transfer Vehicle (ATV) Propulsion & Reboost System Engineer:

    * Design, development of Propulsion & Reboost Test System hardware:

    ° Control PC, Comms unit, Reboost System interface.
    * Design, development of Propulsion & Reboost Test System software:

    ° MS-DOS Scripting, LabVIEW, C.
    * Design, development of ATV Propulsion & Reboost System telemetry test interface:

    ° Ka-Band, S-band, ATV Control Centre & Ground Control Simulator (ATV-CC & AGCS) protocols. * Development & operation ATV propulsion and refuelling systems simulator,
    * Design, development of ATV Attitude and Orbital Control System (AOCS) test system,
    * Maintenance, upgrade of HP VEE 5.0 Test System,
    * Assembly, integration, & test of Propulsion & Reboost System.

     

    Lockheed Martin, Portsmouth, England
    June 1996 - July 1999
    Merlin (Anti-Submarine Helicopter) Avionics Test System (MATS) Engineer:

    * Requirements management and analysis (RDD, Doors).
    * Creation, maintenance and control of:

    ° Software Requirement Specification (SRS), ° Software Design Document (SDD),
    ° Software Quality Control Plan.

    * Design, implementation of Avionics subsystems Test & Verification processes: ° Digital, Analogue, RF, Video, & Manometric.

    * Sub-contractor management:
    ° Westland Helicopter, Logica, SERCO, Marconi, British Aerospace.

    * Creation, maintenance & control of:
    ° Requests for Proposals (RFPs),
    ° Contractual Statements of Work (SOWs),
    ° Service Level Agreements (SLAs),
    ° Post Design Services (PDS) Task Management System, ° HW & SW Design & Specification Documents,
    ° Task Management Process documentation.

    Airborne Stand Off Radar (ASTOR) Reconnaissance / Surveillance Aircraft

    * RF, EMC & TEMPEST Design and Test
    * Requirements Management & analysis (RDD, DOORS). * RF analysis & design for radar components.
    * Creation, maintenance and control of:

    ° EMC & TEMPEST Control Plan,
    ° Hardware Design Specification (HDS),
    ° Interface Control Specification Document (ICD).

     

    Mullard Space Science Laboratory (MSSL), University College London June 1993 - June 1996

    Plasma Electron And Current Experiment (PEACE) Assembly Integration, Test, and Calibration Engineer:
    * Assembly, integration & test of High & Low Energy Electron Analyser (HEEA & LEEA) sensors,
    * Assembly, integration & test of Data Processing Unit (DPU),

    * Development of Electrical Ground Support Equipment (EGSE) software,
    * Development of Cluster Spacecraft Interface Simulator,
    * Development & operation of HEEA & LEEA electron optics calibration and test using:

    ° Thermal vacuum chamber, Electron gun,
    ° 3-axis rotating sensor mount,
    ° Automated calibration sequencing software.

    * Development of data capture, reduction and analysis software, * Assembly, Integration Test and Verification @:

    ° Clean room laboratory at MSSL,
    ° On spacecraft at the Astrium Spacecraft Assembly Clean Room, Friedrichshafen ° Industrie Anlagen Betriebs Gesellschaft (IABG) Munich.

    * Support for Ariane 501 launch phase activities at Kourou, French Guiana. * C, Fortran, IDL, Lab Windows, LabVIEW.

    * Cluster is an ESA mission to study how the solar wind affects the Earth,
    * 4 Identical spacecraft travel in tetrahedral formation to provide 4D data,
    * Each spacecraft carries 11 identical instruments to investigate charged particles, electrical, & magnetic fields,
    * PEACE instrument obtains continuous plasma electrons' velocity moments distribution function,
    * Detector counts collected in energy, polar-angle, & azimuth-angle bins to form a 3D matrix,
    * Two sensors are used:

    ° LEEA (low-energy electron analyser)
    ° HEEA (high-energy electron analyser).
    ° Energy coverage is from 0.67 eV to 30 KeV in 92 levels.

     

    QinetiQ, Farnborough, England
    December 1990 - June 1993
    STRV Development & Assembly, Integration Test & Verification (AIT/AIV) Engineer:
    * Design, development, & application of environmental testing strategies (vibration, thermal vacuum, EMC)

    * Test of radiation-hardened & non-radiation-hardened components using Gamma ray radiation sources, (60Co, 137Cs) at AWRE Aldermaston,
    * Sub-system Radiated & Conducted Susceptibility & Emissions (EMC/EMI) Testing in RF Anechoic Chamber using HP Signal Analyser,
    * Antenna test using LabVIEW & HP VXI Arbitrary Waveform Generator (AM/FM/PM, PSK/FSK/MSK, QAM, 250kHz-2.7GHz),
    * Development of Pulse Height Analysis Sub-system for Cosmic Ray Effects & DOsimetry (CREDO) experiment,
    * Test Atomic Oxygen Erosion experiment.
    * Evaluation & calibration of attitude control magnetorquers using torsion bench.
    * Development of Neutralizer Xe propellant system,
    * Development & operation of Ground Support Equipment (GSE).
    * Assembly, Integration Test and Verification in DRA clean room.
    * Support for Ariane V64 launch phase activities at Kourou, French Guiana.

    UK-10 Ion Thruster Development & Assembly, Integration Test & Verification (AIT/AIV) Engineer

    * Research and development of UK-10 Ion Thruster & Neutralizer. * Assembly, integration, & test of UK-10 Ion Thruster:

    ° Xenon Flow Control Units (FCU), Power Processing Unit (PPU), Neutraliser.
    * Design, development, & operation of portable RF transparent vacuum chamber rig for UK-10 Ion thruster EMC / EMI testing within RF anechoic chamber.
    * Design, development of future spacecraft utilizing Ion Thrusters:

    ° SpaceCraft Orbital Reconnaissance Platform using Ion-thrusters for Orbit keeping (SCORPIO), ° ESA GOCE spacecraft

    ° QinetiQ TopSat spacecraft.

     

    Royal Air Force, United Kingdom
    September 1985 - September 1989
    Flying Officer. General Duties (Pilot) Branch:
    * Management, Leadership and Officer Training @ RAF College Cranwell.

    * Ab-Initio Flying Training 62 Hours
    ° General handling, Instrument flying, Spin Aerobatics, Formation, Pilot-navigation

    * Basic Fast Jet Training 124 Hours (40 Hours Simulator)
    ° General handling, Instrument flying, Spin Aerobatics, Formation, Pilot-navigation

    * RAF Cranwell, RAF Church Fenton, RAF Finningley, RNAS Turnhouse, RMCS Cranfield, RAE Farnborough


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    Individual exceptions can be made on a case by case basis by emailing sales@space-careers.com. Accounts found not to be in compliance will be deleted in the absence of an email.
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