IMPRS June 2003. Space Research, in praxis, illustrated by a ground-based example The „Ozonometer“ as a student project.

Slides:



Advertisements
Similar presentations
AMSAT-NA FOX Satellite Program Review, Status, and Future JERRY BUXTON, NØJY AMSAT VP-ENGINEERING.
Advertisements

Advanced Energy Vehicle
Basic Overview of Project Management and Life Cycle ACES Presentation T. Gregory Guzik January 21, 2003.
Innovation You Can Count On™ 1 Payload Integration Wendi Otto Systems Engineer, Pegasus and Taurus Launch Vehicles October 4, 2007 All Information Approved.
Charles Nola Lisa Blue June 21, 2006 Charles Nola Lisa Blue June 21, 2006 Crew Launch Vehicle (CLV) Upper Stage Avionics & Software Acquisition Planning.
Chapter 14 Network Design and Implementation. 2 Network Analysis and Design Aspects of network analysis and design Understanding the requirements for.
Cory Fulkerson (Project Manager) - Mechanical Engineer John Graham - Computer Engineer Clayton Hooks - Electrical Engineer O’Raphael Okoro - Electrical.
Questions from the European colleagues & Answers (only) from the Chinese engineers present for Y.-W. Zhang and S.-G. Yuan Chinese Academy of Space Technology.
Global Magnet Systems including Field Mapping MICE Project Board 28 th June 2011 M Courthold – RAL R Preece - RAL.
GLAST LAT ProjectISOC CDR, 4 August 2004 Document: LAT-PR-04500Section 4.11 GLAST Large Area Telescope: Instrument Science Operations Center CDR Section.
GLAST LAT ProjectSLAC Pre - Baseline Review, April 16, 2002 ` 1 GLAST Large Area Telescope: I&T Overview WBS: Elliott D. Bloom Stanford Linear Accelerator.
Conceptual Design Review Metro State College of Denver Daniel Bass, Matt Hanley
LSU 01/18/2005Project Life Cycle1 The Project Life Cycle Project Management Unit, Lecture 2.
Library Automation: Planning and Implementation
LSU 07/07/2004Communication1 Communication & Documentation Project Management Unit – Lecture 8.
1 Engineering the James Webb Space Telescope Paul Geithner JWST Deputy Project Manager - Technical March 26, 2011.
DC Chp 1 Jeopardy Review Section 1Section 2Section 3Section 4Section
A Finmeccanica Company 04/2000/1 EUSO Development Philosophy EUSO General Meeting Max Planck Institute for Physics Munich, November the 20th 2003.
The Pursuit for Efficient S/C Design The Stanford Small Sat Challenge: –Learn system engineering processes –Design, build, test, and fly a CubeSat project.
New Mexico Space Grant Consortium Student Launch Program Provide annual access to space for student experiments from Spaceport America.
October 2005ALMA Cost Review1 Atacama Large Millimeter Array Science IPT Review Bilateral Project Scientists: Al Wootten, (Lead) Tom Wilson, (Deputy) Ryohei.
Andrea Santangelo, Kepler Center-Tü Toulouse, February 2, 2012 “The Organization of the EUSO- Balloon mission” Andrea Santangelo * Kepler Center for Astro.
IMPRS June Organigram of ESA, in the late 1980s
Hunt for Molecules, Paris, 2005-Sep-20 Software Development for ALMA Robert LUCAS IRAM Grenoble France.
NASA’s Goddard Space Flight Center LRO Integration and Test Joanne Baker GSFC Code 568 August 16-17, 2005.
High Altitude Balloon Data Logger for Scientific Payloads Presented by: Dallas Hodge Spring Space Grant Symposium 1.
Common PDR Problems ACES Presentation T. Gregory Guzik March 6, 2003.
What does a Computer Do?. What is a Computer? A computer is an electronic device, operating under the control of instructions stored in its own memory,
MASSACHUSETTS INSTITUTE OF TECHNOLOGY NASA GODDARD SPACE FLIGHT CENTER ORBITAL SCIENCES CORPORATION NASA AMES RESEARCH CENTER SPACE TELESCOPE SCIENCE INSTITUTE.
VST: dome THE LIFE CYCLE OF MODERN TECHNOLOGICAL PROJECTS Ing. Davide Fierro THE LIFE CYCLE OF MODERN TECHNOLOGICAL PROJECTS.
Development programs and model philosophy1 Preliminary design review Prototype program Critical design review Qualification program Qualification review.
COROTWEEK n°8 Toulouse May the 24th, 2005 Program Status (Th. Lam-Trong) 1 COROT.
1 Instructions Run this Powerpoint in slide show mode, and answers are revealed one at a time on your mouseclick. Set rules to fit your audinece / situation.
Space Engineering 2 © Dr. X Wu, Space Engineering 2 Lecture 1.
Ocean Observatories Initiative OOI Cyberinfrastructure Architecture Overview Michael Meisinger September 29, 2009.
Solar B Mission Operations Working Group - 3 February Page 1 SS Instrument Operations for TIMED, Cluster, & Stereo C. P. Holmes Sun-Earth Connection.
CRISP & SKA WP19 Status. Overview Staffing SKA Preconstruction phase Tiered Data Delivery Infrastructure Prototype deployment.
THE PROJECT LIFE CYCLE PROJECT MANAGEMENT LIFE CYCLE LSU 01/18/2005 PROJECT LIFE CYCLE 1.
CubeSat for Ions, Neutrals, Electrons and Magnetic Fields PI Robert Lin, SSL Project Manager Thomas Immel, SSL Systems Engineer Jerry Kim, SSL Mechanical.
GERB 4 Instrument Status GIST 25 23rd October 2006 Presenter: N Morris.
RBSP Radiation Belt Storm Probes RBSP Radiation Belt Storm Probes RBSP/EFW I-PER 21 January EFW Overview and Status Keith Goetz University of Minnesota.
High Performance Computing (HPC) Data Center Proposal Imran Latif, Facility Project Manager Scientific & Enterprise Computing Data Centers at BNL 10/14/2015.
Solar Probe Plus A NASA Mission to Touch the Sun March 2015 Instrument Suite Name Presenter's Name.
Solar Probe Plus Fluxgate Magnetometer QSR – Oct SPF MAG Quarterly Report – Oct 2014 The MAG EM1 (EQM) (board and frame at right) was successfully.
KEY PERSONNEL Dr. Bob Schutz, GLAS Science Team Leader Dr. Jay Zwally, ICESat Project Scientist, GLAS Team Member Mr. David Hancock, Science Software Development.
Reliability Applied to KM3NET
Prox-0.3 Georgia Institute of Technology Kiichiro DeLuca Richard Zappulla Ian Chen Matt Uhlman 1.
June 16, 2015SPP/FIELDS SOC CDR: Integration & Test SPP/FIELDS Integration and Test SOC Critical Design Review Keith Goetz University of Minnesota
SRR and PDR Charter & Review Team Linda Pacini (GSFC) Review Chair.
THEMIS MRRI&T − 1GSFC, January 5, 2007 Integration and Test.
Proton-Driven Plasma Wakefield Acceleration CERN Project Structure Edda Gschwendtner, CERN Lisbon Meeting, 22 June 2012Edda Gschwendtner, CERN2.
ESA UNCLASSIFIED – For Official Use Experiment Development and Integration Process Philippe Schoonejans, Head of Robotics and Future Projects Office ESA.
Dr.F. Arteche EMC DEPFET Project: A general overview.
Status of EPS Battery configuration finalized Solar panel layout –finalized Solar panel Substrate is ready for bonding EM – fabricated and Completed the.
The Principles of Space Instrument Design Lauren Shea Based on research completed at MSSL Alton Convent School.
THEMIS-SCM SCM – OVERALL RESSOURCES – STATUS versus REQUIREMENTS ItemSpecificationStatus Sensor Bandwith Sensor Sensitivity Up to 4 kHz 1 pT/√Hz at 10.
Power Philip Luers NASA/GSFC Code 561 August 16-17, 2005.
I&T&C Organization Chart
Agenda. Solar Probe Plus FIELDS Main Electronics Package iPER Agenda Feb 2, 2017.
GLAST Large Area Telescope:
PHI Status Report SO Cleanliness Working Group #24
Space Proximity Atmospheric Research above Tropospheric Altitudes
GLAST Large Area Telescope:
SDO Flight Dynamics Subsystem
Launch and On-orbit Checkout
Observatory Control System
Integration and Test Organization Chart
PSS verification and validation
Integration & Test Instrument Operations Coordination
ESHAC #8 Safety Readiness Review Thomas Hansson, ESH
Presentation transcript:

IMPRS June 2003

Space Research, in praxis, illustrated by a ground-based example The „Ozonometer“ as a student project

IMPRS June 2003 The instrument needs supplies from the laboratory: electrical power, cooling water, control by the experimenter, clock pulses, air condition. The instrument returns to the laboratory: measured scientific data, engineering data, waste, In space research, the terms „experiment“ and „instrument“ are often confused. Note the difference, though: an instrument is a measurement device, usually a piece of hardware. It is built by a clever scientist to allow him to perform experiments. The heart of the Ozonometer is the proper measuring device („instrument“)

IMPRS June 2003 Space Research, in praxis, illustrated by a ground-based example The „Ozonometer“ as a student project The ozonometer on board the „ozonomobil“

IMPRS June 2003 The ozonombile has to perform the same services as the laboratoy had done before. That requires several provisions: An engine for driving plus sufficient fuel, a dynamo (or solar cells) for generating electric power, a data storage for saving scientific and engineering data, a command antenna for receiving instructions on where to go and what to do, a data antenna for transmitting data to the experimenter, a dump for collecting waste. The ozonomobil can carry other instruments sharing the same resources, provided they do not interfere with each other. In order to survive rides on bad streets, the instruments have to be built with a certain robustness. The mission is expensive. Thus, risk has to be minimized by proper testing. The student now plans to move his instrument through town, on a mobile platform, the „Ozonomobile“

IMPRS June 2003 An idea is created in a researcher‘s brain, leading to calculations, discussions. Institute gets interested. Functional models of instrument are designed, built and tested in laboratory. Search for PI, CoIs, proposal written, application for funding. Development phase. Testing of critical items. Proposal accepted by agency, find funding, find contractors. Interface definitions. Detailed design. Electrical layouts. Preliminary design review (PDR). Build SM and EM, deliver to agency. Mechanical SM tests and EM system tests. Critical design review (CDR). Experiments in space: from ideas to scientific results. 1.

IMPRS June 2003 Experiments in space: from ideas to scientific results. 2. Build prototype (PM). Instrument performance tests. Qualification tests with enhanced levels. Final design review (FDR). Build flight units (FM and FS). Acceptance tests. Final calibrations. Delivery to agency. Integration into S/C, adjustments, fits, connections Electrical system tests: functional, EMC, software. Environmental tests: vibration, TV, solar simulation.... Tranport to launch pad. Final tests. Flight readiness review (FRR). Preparations for launch. Launch. Launchparty...

IMPRS June 2003 Experiments in space: from ideas to scientific results. 3. Mission operation phase Commissioning: switch on of all subsystems, EMC tests, calibrations, software patches and uploads etc., data distribution to PIs, networks, Internet. Routine operations: daily /weekly/monthly planning, preparing of joint operation programs (JOPS), observatory mode, guest investigator programs. Distribution of NRT data to PIs at mission control center. Data distribution of NRT and final data to CoIs (CD, Internet). Data archiving on tapes, CD, DVD. Routine processing to Level 2 (calibrated). Scientific evaluations. Thinking, discussing, writing, presenting... New ideas in researchers‘ brains...