David Zolesi: Design of subsystems onboard the ISS. Kayser Italia S.r.l. Via di Popogna Livorno (Italy)
|
|
|
- Zoe Warren
- 5 years ago
- Views:
Transcription
1 David Zolesi: Design of subsystems onboard the ISS Kayser Italia S.r.l. Via di Popogna Livorno (Italy)
2 Company overview Kayser Italia is a fully independent Italian system engineering company (SME), incorporated in 1986 Kayser Italia offers its products and services into the space sector Kayser Italia has a staff of around 60 engineers Kayser Italia has extensive expertise in the design and manufacturing of experiments and payloads, related Ground Support Equipment and Mission Operations and Support, both as prime-contractor, as well as sub-contractor 2
3 Company overview Kayser Italia has 28 years experience in the supply of hardware and software solutions and on-site support services for space Kayser Italia has participated to 60 space missions with 90 payloads, ranging from sounding rockets, to unmanned and manned European, Russian, Japanese, Chinese platforms, to Shuttle, and ISS. Engineering services with key focus on the following application areas: Life and Physical Science experiment hardware, for both manned and unmanned missions Equipment for spacecrafts Systems and sub-systems for exploration missions Mission support Support to on-board and ground operations 3
4 CTPU Power ON CTPU Power OFF CTPU Power ON CTPU Power OFF CTPU Power on CTPU CAN Active BT_SW_OFF CTPU CAN Active HC_END BT_SW_ON_OK Technical know-how and competencies Electrical/Electronics Power distribution Data acquisition Electronic controls Microprocessors and microcontrollers Software Instrument firmware Flight software Man-machine interface EGSE software Data acquisition, storage and presentation OFF LOW POWER CRUISE BT_SW_OFF_ERR LOW POWER SURFACE BATTERY SWITCH OFF CTPU Power OFF CTPU Power ON CTPU Power OFF CTPU Power ON CTPU Power OFF HEALTH CHECK BT_SW_OFF_OK SURFACE INIT TIMEOUT SURFACE BT_SW_ON_ERR CRUISE BT_SW_ON BATTERY SWITCH ON UPDATE TIMELINE DUMP TIMELINE TM DATA UPLOAD DATA CHECK OUT DUMP TIMELINE UPDATE TIMELINE Ground support equipment Electrical GSE Mechanical GSE Thermal GSE DATA ACQUISITION Mechanics/Structural/Thermal Mechanical design FEM Structural analysis Assembly and integration Fracture Control Thermal design and analysis System AIV 4
5 Satellites programs PAMELA (INFN) Telecommand and Telemetry interfaces TEMISAT (Telespazio) Microsatellite, EGSE and OCC MITA (CGS) - EGSE ROSETTA (OG) Breadboard of drill and carousel control for Shark subsystem COSMO-SKYMED (ALENIA) - EGSE Focal plane 5
6 Life science: biology experiments TRIPLELUX Cells and Bacteria analyser YING-B1 Yeast batch culture ROALD T-lymphocytes cell culture BIOLAB YING-B2 Yeast solid culture STROMA 2D BMSC cell culture PKINASE Monocytes cell culture KUBIK BASE-B Bacteria anaerobic culture XENOPUS Xenopus tadpoles aquaria BASE-C Bacteria aerobic culture AT-SPACE Arabidopsis germination BIOKIN-4 Bacteria aerobic culture SEN Sensor package 6
7 Life science: biology facilities BIOKON (ASI) Containers for autonomous experiments MATROSHKA (ESA/DLR) (Sub to DLR. Facility Electronics, CAN Bus, S/W, EGSE) BIOBOX (ESA) (Sub to AST. Facility control electronics, centrifuge electronics, harness, Peltier controller, F/W, EGSE) BIOPAN (ESA) (Sub to KT. Electronics, satellite electrical I/F, F/W, EGSE) KIC (ESA) Experiment Containers ECCO (ESA) Flight Thermal Transport Containers 7
8 Life science: analysers MIDASS Microbial Detection in Air System for Space (ESA) (Sub to biomérieux) I-BICA Immuno-Biochemical Analyser on ISS (ESA) (Sub to Astrium) BioanalysISS (ESA) (Sub to Univ. Laval) 8
9 Life science: human physiology facilities HPA (ASI) Hand Posture Analyser ELITE-S2 (ASI) ELaboratore Immagini TElevisive - Space 2 Posture Acquisition Glove (PAG) and Wrist Electronics Box (WEB) Hand Grip Dynamometer (HGD) Target Objects ELITE-S2 camera in the USLab of ISS Pinch Force Dynamometer (PFD) HPA used : - Taxi flight TM34 (R.Vittori, 2002) - Increment 7 (Ed Lu, 2003) - Increment 8 (Mike Foale, 2004) - Soyuz 10S (R.Vittori, 2005) - STS120 (Paolo Nespoli, 2007) ELITE-S2 integrated in EXPRESS rack at KSC ELITE-S2 cameras at KSC 9
10 Physical science GABRIEL (ESA) MSL (ESA) (Sub to KT. Power Distribution Module) IFOAM (ASI) EML (ESA) (Sub to AST. Power distribution, signal/data acquisition & control electronics, GSEs 10
11 EHD (ESA) Data storage device ISS equipment PPS/KuPS (ESA) Portable Power Supply HAMVIDEO (ESA) Video Transmitter CFEU (ESA) Cabin Fan Electronics Unit ACLS (ESA) Advanced Closed Loop System Sub to Astrium. Avionics of the facility in progress.. 11
12 Technologies TSS (ESA) Tensegrity Space Structures Wired and Wireless On-board Sensor Network (ESA/ASI) EAP (ESA) Electro-Active Polymers GNSS Retroreflector Arrays for satellite laser ranging (ASI) (Sub to INFN) SMA Shape Memory Alloys Peltier controllers from 25 W up to 250 W 12
13 ICARO ICARO - Italian Centre for Advanced Research and Operations, is the Kayser Italia centre for experiments and operations support. ICARO USOC User Support Operations Centre Kayser Italia Livorno, Italy. ESC Experiment Support Centre Kayser Italia Livorno, Italy. Management of on-board facilities and experiments Science Lab Hardware Lab Clean Room 13
14 End of presentation. 14
European Lunar Lander: System Engineering Approach
human spaceflight & operations European Lunar Lander: System Engineering Approach SECESA, 17 Oct. 2012 ESA Lunar Lander Office European Lunar Lander Mission Objectives: Preparing for Future Exploration
System 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,
Pre-Launch Procedures
Pre-Launch Procedures Integration and test phase This phase of operations takes place about 3 months before launch, at the TsSKB-Progress factory in Samara, where Foton and its launch vehicle are built.
Robots to Support a Human Mars Mission
Robots to Support a Human Mars Mission 1 W. Naumann, P. Hofmann, A. v. Richter Kayser-Threde GmbH Wolfratshauser Str. 48, D-81379 München email: andreas.von.richter@kayser-threde.com 7th Workshop ASTRA
ARCHIVED REPORT. For data and forecasts on current programs please visit or call
Space Systems Forecast - Launch Vehicles & Manned Platforms ARCHIVED REPORT For data and forecasts on current programs please visit www.forecastinternational.com or call +1 203.426.0800 Outlook ATV-5,
Validation System (EVS)
Presentation of the Astrium EGSE Validation System (EVS) Compiled Clive Catley Introduction document is the property of Astrium. It shall not be communicated to third Its content shall not be disclosed.
The European Lunar Lander Mission
The European Lunar Lander Mission Alain Pradier ASTRA Noordwijk, 12 th April 2011 European Space Agency Objectives Programme Objective PREPARATION FOR FUTURE HUMAN EXPLORATION Lunar Lander Mission Objective
Development and Implementation of a new Columbus Operations Setup
IAC-12.B3.4-B6.5.1 Development and Implementation of a new Columbus Operations Setup D. Sabath*, G. Söllner*, D. Schulze-Varnholt + * DLR, Oberpfaffenhofen, Germany + Astrium GmbH, Friedrichshafen, Germany
SURVEYOR-H. Technical Data. Max speed 120 km/h. Engine power 7.2 hp. Powerplant Modified Zenoah G29E. Fuel tank volume 3.6 l
rev. 28.10.14 * features & specifications are subject to change without notice. Technical Data Max speed 120 km/h Engine power 7.2 hp Powerplant Modified Zenoah G29E Fuel tank volume 3.6 l Payload with
SPARTAN. 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
Formation 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
Super Squadron technical paper for. International Aerial Robotics Competition Team Reconnaissance. C. Aasish (M.
Super Squadron technical paper for International Aerial Robotics Competition 2017 Team Reconnaissance C. Aasish (M.Tech Avionics) S. Jayadeep (B.Tech Avionics) N. Gowri (B.Tech Aerospace) ABSTRACT The
Podium Engineering complete race cars, vehicle prototypes high performance hybrid/electric powertrain
Born in the firm belief that design quality, high project commitment and absolute respect of deadlines are key competitive factors for a consulting and engineering company, Podium Engineering is a dynamic
In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led
A-Level Aerosystems In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led the company to be a leader in the micro UAV market in Russian
OLEV AN ON-ORBIT SERVICING PROGRAM FOR COMMERCIAL SPACECRAFTS IN GEO
Von der Erde ins All. Und zurück. Intelligente Lösungen für Industrie und Wissenschaft. From Earth to Space. And back. Intelligent solutions for industry and science. E a r t h S p a c e & F u t u r e
Electric Penguin s philosophy:
UNMANNED PLATFORMS AND SUBSYSTEMS Datasheet v 1.1 Penguin BE Electric Unmanned Platform Up to 110 minutes of endurance 2 with 2.8 kg payload 23 liters of payload volume Quick replaceable battery cartridge
SOYUZ TO LAUNCH GALILEO
SOYUZ TO LAUNCH GALILEO This new Starsem s flight will boost the European Space Agency s Giove-B spacecraft (Galileo In Orbit Validation Element), the second European navigation satellite. This prestigious
SSC Swedish Space Corporation
SSC Swedish Space Corporation Platforms for in-flight tests Gunnar Florin, SSC Presentation outline SSC and Esrange Space Center Mission case: Sounding rocket platform, dedicated to drop tests Satellite
Cygnus Payload Accommodations: Supporting ISS Utilization
The Space Congress Proceedings 2018 (45th) The Next Great Steps Feb 27th, 1:30 PM Cygnus Payload Accommodations: Supporting ISS Utilization Frank DeMauro Vice President and General Manager, Advanced Programs
neuron An efficient European cooperation scheme
DIRECTION GÉNÉRALE INTERNATIONALE January, 2012 neuron An efficient European cooperation scheme I - INTRODUCTION 2 II - AIM OF THE neuron PROGRAMME 3 III - PROGRAMME ORGANISATION 4 IV - AN EFFICIENT EUROPEAN
NASA Glenn Research Center Intelligent Power System Control Development for Deep Space Exploration
National Aeronautics and Space Administration NASA Glenn Research Center Intelligent Power System Control Development for Deep Space Exploration Anne M. McNelis NASA Glenn Research Center Presentation
Thinking 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
NATIONAL SPACE PROGRAM. February 10 th, 2016 Capua, ITALY
NATIONAL SPACE PROGRAM February 10 th, 2016 Capua, ITALY The National Space Program Space Information Cycle (To go to space to see the Earth ) An opportunity for national technology development 2 The National
Palamede, more than a microsatellite. Workshop on University Micro Satellites in Italy Rome, July 27, 2005
Palamede, more than a microsatellite The Palamede Team (represented by Franco Bernelli and Roberto Armellin) Workshop on University Micro Satellites in Italy Rome, July 27, 2005 Outline Mission and educational
The 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
Exomars 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
CALL 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
OMOTENASHI. (Outstanding MOon exploration TEchnologies demonstrated by NAno Semi-Hard Impactor)
SLS EM-1 secondary payload OMOTENASHI (Outstanding MOon exploration TEchnologies demonstrated by NAno Semi-Hard Impactor) The smallest moon lander launched by the most powerful rocket in the world * Omotenashi
NASA Perspectives on the Importance of Reform in Electric Energy Systems Education
NASA Perspectives on the Importance of Reform in Electric Energy Systems Education Reforming Electric Energy Systems Curriculum With Emphasis on Renewable/Storage, Smart Delivery, and Efficient End-Use
NEXT Exploration Science and Technology Mission. Relevance for Lunar Exploration
NEXT Exploration Science and Technology Mission Relevance for Lunar Exploration Alain Pradier & the NEXT mission team ILEWG Meeting, 23 rd September 2007, Sorrento AURORA PROGRAMME Ministerial Council
CHAPTER 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,
POWER CONTROL SYSTEM FOR THE AGILE SATELLITE
POWER CONTROL SYSTEM FOR THE AGILE SATELLITE G. Ebale (1), A. Lamantia (1), M. La Bella (1) (1) Blu Electronic s.r.l. via Gallarate,150. 20151 Milano (Italy), Email: giorgio.ebale@bluelectronic.it; antonio.lamantia@bluelectronic.it;
Length Height Rotor Diameter Tail Rotor Diameter..12. Tail Boom Length Width
2.1 Air Vehicle 2.1.1 Vehicle General Description The PA-01 Vapor S-UAV is a rotary wing small unmanned aerial vehicle. The AV is powered by an outrunner 8.5hp class brushless electric motor. The airframe
FALL SEMESTER MECE 407 INNOVATIVE ENGINEERING ANALYSIS AND DESIGN PROJECT TOPICS
2016-2017 FALL SEMESTER MECE 407 INNOVATIVE ENGINEERING ANALYSIS AND DESIGN PROJECT TOPICS 1- Design, construction and control of a cart-inverted pendulum control system: - There will be a cart and an
VEGA SATELLITE LAUNCHER
VEGA SATELLITE LAUNCHER AVIO IN WITH VEGA LAUNCHER Avio strengthened its presence in the space sector through its ELV subsidiary, a company jointly owned by Avio with a 70% share and the Italian Space
Analysts/Fund Managers Visit 19 April Autonomous Systems and Future Capability Mark Kane
Analysts/Fund Managers Visit 19 April 2007 Autonomous Systems and Future Capability Mark Kane The Rationale for UAVs The Rationale for UAVs UAVs generally seen to carry out the dull, dirty, and dangerous
NanoRacks 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
Gravity Control Technologies Phase I - Unmanned Prototype
archived as http://www.stealthskater.com/documents/gct_02.pdf read more of GCT at http://www.stealthskater.com/ufo.htm#gct note: because important websites are frequently "here today but gone tomorrow",
An Overview of CSA s s Space Robotics Activities
An Overview of CSA s s Space Robotics Activities Erick Dupuis, Mo Farhat ASTRA 2011 ESTEC, Noordwijk, The Netherlands Introduction Key Priority Area for CSA Recent Reorganisation Strategy Guided by Global
Palos Verdes High School 1
Abstract: The Palos Verdes High School Institute of Technology (PVIT) Unmanned Aerial Vehicle team is proud to present Condor. Condor is a hexacopter weighing in at 1664g including the 4 cell 11.1 volt,
Modular 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 *,
Analysis of Power Storage Media for the Exploration of the Moon
Analysis of Power Storage Media for the Exploration of the Moon Michael Loweth, Rachel Buckle ICEUM 9 22-26 th October 2007 ABSL Space Products 2005 2007 Servicing USA and the ROW UNITED KINGDOM Culham
MASCOT Marco Polo Surface Scout. Progress Report on Lander Package Study for Marco Polo
MASCOT Marco Polo Surface Scout Progress Report on Lander Package Study for Marco Polo Lutz Richter 1, Lars Witte 1, Tra-Mi Ho 1, Stephan Ulamec 2, Jean-Pierre Bibring 3 1 DLR Bremen, 2 DLR Cologne, 3
A Private Commercial Space Company EA02P046V5
A Private Commercial Space Company Outline Who We Are The Technology The Next Step Excalibur Almaz was formed to revolutionize the spaceflight industry through regular manned and unmanned flights to orbit
Over 100 Years of History
IT1903 Over 100 Years of History AND AEROSPACE TECHNOLOGY www.secondomona.com 1903 We started together Over 100 years OF SUCCESSFUL HISTORY 1903 Founded by Mr. Secondo Mona in Somma Lombardo, Italy 1913
Upper 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
Autonomous Quadrotor for the 2014 International Aerial Robotics Competition
Autonomous Quadrotor for the 2014 International Aerial Robotics Competition Yongseng Ng, Keekiat Chua, Chengkhoon Tan, Weixiong Shi, Chautiong Yeo, Yunfa Hon Temasek Polytechnic, Singapore ABSTRACT This
Jay Gundlach AIAA EDUCATION SERIES. Manassas, Virginia. Joseph A. Schetz, Editor-in-Chief. Blacksburg, Virginia. Aurora Flight Sciences
Jay Gundlach Aurora Flight Sciences Manassas, Virginia AIAA EDUCATION SERIES Joseph A. Schetz, Editor-in-Chief Virginia Polytechnic Institute and State University Blacksburg, Virginia Published by the
NASA s Choice to Resupply the Space Station
RELIABILITY SpaceX is based on the philosophy that through simplicity, reliability and low-cost can go hand-in-hand. By eliminating the traditional layers of management internally, and sub-contractors
Light-Lift Rocket II
Light-Lift Rocket I Light-Lift Rocket II Medium-Lift Rocket A 0 7 00 4 MASS 90 MASS MASS This rocket can lift a mission that has up to 4 mass units. This rocket can lift a mission that has up to 90 mass
r 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
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
Instruction Manual: Space Launch System Payload Transfer Module (PTM)
Instruction Manual: Space Launch System Payload Transfer Module (PTM) Designer s comments: This model has been designed without the benefit of engineering blueprints. Only publically available conceptual
The Mars Express Mission A Continuing Challenge. Erhard Rabenau, NOVA Space Associates Ltd Mars Express Senior Mission Planner
The Mars Express Mission A Continuing Challenge Erhard Rabenau, NOVA Space Associates Ltd Mars Express Senior Mission Planner Mars Society, Munich, 13 October, 2012 The Mars Express Mission - a First in
Table of Contents. Abstract... Pg. (2) Project Description... Pg. (2) Design and Performance... Pg. (3) OOM Block Diagram Figure 1... Pg.
March 5, 2015 0 P a g e Table of Contents Abstract... Pg. (2) Project Description... Pg. (2) Design and Performance... Pg. (3) OOM Block Diagram Figure 1... Pg. (4) OOM Payload Concept Model Figure 2...
High Performance Engineering, Unleashed
High Performance Engineering, Unleashed Statement of Capabilities Award Winning Range of Advantages Private SME venture headquartered in Portugal, The Netherlands, UK, and Germany A proven history of delivering
SMall Innovative Launcher for Europe: results of the H2020 project SMILE. Leo Timmermans, NLR І 2 October 2018
SMall Innovative Launcher for Europe: results of the H2020 project SMILE Leo Timmermans, NLR І 2 October 2018 Problem (and opportunity) 2 Problem (and opportunity) SmallSat Launch Market to Soar Past $62
System Level Design Review
System Level Design Review HABIP High Altitude Balloon Instrumentation Platform P17104 & P17105 October 6, 2016 Team Members Team Communications Data Acquisition and Control Systems Team Member Major Team
The validation of HUMS engine data
Fourth DTSO International Conference on Health and Usage Monitoring The validation of HUMS engine data Joanna Kappas Air Vehicles Division, Platforms Sciences Laboratory, Defence Science and Technology
Solar Electric Propulsion Benefits for NASA and On-Orbit Satellite Servicing
Solar Electric Propulsion Benefits for NASA and On-Orbit Satellite Servicing Therese Griebel NASA Glenn Research Center 1 Overview Current developments in technology that could meet NASA, DOD and commercial
Mars 2018 Mission Status and Sample Acquisition Issues
Mars 2018 Mission Status and Sample Acquisition Issues Presentation to the Planetary Protection Subcommittee Charles Whetsel Manager, Advanced Studies and Program Architecture Office Christopher G. Salvo
Mercury VTOL suas Testing and Measurement Plan
Mercury VTOL suas Testing and Measurement Plan Introduction Mercury is a small VTOL (Vertical Take-Off and Landing) aircraft that is building off of a quadrotor design. The end goal of the project is for
Hybrid Renewable Energy Solutions for Telecommunication: Case Studies in Kazakhstan
Session 4 - Cross-sectoral systems - Off-Grid Solutions for Industries, Telecommunications and Infrastructure WINDKINETIC OFF-GRID POWER SYSTEMS AND MICROGRIDS Headquarters in Florence WindKinetic designs
UNDERWATER SOLUTIONS WORLDWIDE
UNDERWATER SOLUTIONS WORLDWIDE Payload Autonomy on the Phoenix International Artemis AUV MOOS-DAWG 2015 July 22-23 Peter McKibbin IRAD/Special Projects Manager pmckibbin@phnx-international.com Brief Company
SMARTSat. 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
IRENE PROGRAM. European Sounding Rocket Experiment on Hypersonic Deployable Re-entry Demonstrator
IRENE PROGRAM European Sounding Rocket Experiment on Hypersonic Deployable Re-entry Demonstrator R. Savino, R. Aurigemma, Dr. Pasquale Dell Aversana, L. Gramiccia, F. Punzo, J. Longo, L. Scolamiero, L.
Results of the Airbus DS led e.deorbit Phase B1 ESA study. Dr.-Ing. Stéphane Estable ESA Clean Space Industrial Days, October 2017
Results of the Airbus DS led e.deorbit Phase B1 ESA study Dr.-Ing. Stéphane Estable ESA Clean Space Industrial Days, 24-26 October 2017 2 e.deorbit Mission Final rendezvous and capture phase Phase B1 Team
The 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
Lunar Science and Infrastructure with the Future Lunar Lander
ICEUM9 Sorrento Lunar Science and Infrastructure with the Future Lunar Lander Session 9: Next steps for Robotic Landers, Rovers and Outposts ICEUM9 Sorrento, Oct. 26, 2007 Hansjürgen Günther 26/10/2007
UNCLASSIFIED R-1 ITEM NOMENCLATURE
COST ($ in Millions) All Prior Years FY 2012 FY 2013 # Base OCO ## Total FY 2015 FY 2016 FY 2017 FY 2018 Air Force Page 1 of 5 R-1 Line #106 Complete Total Program Element - 44.308 10.051 13.000-13.000
Sandwich nozzle hot test on Vulcain 2 engine.
Sandwich nozzle hot test on Vulcain 2 engine. Vulcain 2 Vulcain 2 + Vulcain 1 The information contained in this document is Volvo Aero Corporation Proprietary Information and it shall not either in its
Electric propulsion as game changer for CubeSat: mission analysis with LOTOS
Electric propulsion as game changer for CubeSat: mission analysis with LOTOS Space Tech Expo Europe 24 October 2017, Bremen (DE) Francesco Cremaschi, Sven Schäff Astos Solutions GmbH, Stuttgart service@astos.de
Rover development status
EXOMARS PROJECT 2018 Mission Rover development status ASTRA Workshop 15-17 May 2013 P. Baglioni & the EXM Rover Team Progress on the 2018 Mission Following EXM Program approvals from the Council and IPC
From MARS To MOON. V. Giorgio Director of Italian Programs. Sorrento, October, All rights reserved, 2007, Thales Alenia Space
From MARS To MOON Sorrento, October, 2007 V. Giorgio Director of Italian Programs Page 2 Objectives of this presentation is to provide the Lunar Exploration Community with some information and status of
Fire Power Forum. DISTRIBUTION A: Approved for Public Release.
Armaments Technology Fire Power Forum Mr. Michael George Weapon Systems and Technology Small and Medium Caliber Armaments, Remote Weapons Branch US Army - ARDEC - WSEC 9-10 APR 2009 DISTRIBUTION A: Approved
Notes: GENERAL DYNAMICS EARLY LUNAR ACCESS [1993]
![Notes: GENERAL DYNAMICS EARLY LUNAR ACCESS [1993]](/thumbs/88/115730710.jpg "Notes: GENERAL DYNAMICS EARLY LUNAR ACCESS [1993]")
Notes: file:///f /SPACE Misc/Lunar Explore/Lunar Do...NERAL DYNAMICS EARLY LUNAR ACCESS [1993].htm (1 of 8) [17/03/2005 9:35:03 p.m.] 1.INTRODUCTION EARLY LUNAR ACCESS (ELA) was a "cheaperfasterbetter"
GRC Aircraft Operations Office
GRC Aircraft Operations Office Glenn Research Center Aircraft Operations 1 Mission Provide safety, operational, and engineering oversight to all GRC research experiments involving flight, including non-nasa
ORBITAL EXPRESS Space Operations Architecture Program 17 th Annual AIAA/USU Conference on Small Satellites August 12, 2003
ORBITAL EXPRESS Space Operations Architecture Program 17 th Annual AIAA/USU Conference on Small Satellites August 12, 2003 Major James Shoemaker, USAF, Ph.D. DARPA Orbital Express Space Operations Program
GEO 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
DRONE & UAV.
www.erapkorea.co.kr DRONE & UAV Extended flight time Proven to be reliable, safe and easy to use Various fields of operation Completely autonomous, and manually controlled ERAP DRONE & UAV WHY ERAP s MAPPING
Adrestia. 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
Electric Propulsion Electronics Activities in Astrium Germany
Electric Propulsion Electronics Activities in Astrium Germany IEPC-2007-20 Presented at the 30 th International Electric Propulsion Conference, Florence, Italy Matthias Gollor *), Michael Boss Astrium
EHD Pump. Preliminary Design Review University of Nebraska Lincoln NASA Goddard Space Flight Center
EHD Pump Preliminary Design Review University of Nebraska Lincoln NASA Goddard Space Flight Center Mission Overview Mission Overview Mission Overview Theory and Concepts Concept of Operations Expected
RIMRES: A project summary
RIMRES: A project summary at ICRA 2013 -- Planetary Rovers Workshop presented by Thomas M Roehr, thomas.roehr@dfki.de DFKI Robotics Innovation Center Bremen Robert-Hooke Straße 5 28359 Bremen 1 Acknowledgements
UHABS-5 Mission Zeppelin
UHABS-5 Mission Zeppelin Team Members: Likeke Aipa, Drex Arine, Andrew Bui, Karen Calaro, Kanekahekilinuinanaueikalani Clark, Ka Chon Liu, Cyrus Noveloso, Reagan Paz, Yun Feng Tan, Jake Torigoe, Emanuel
Atlas V Launches the Orbital Test Vehicle-1 Mission Overview. Atlas V 501 Cape Canaveral Air Force Station, FL Space Launch Complex 41
Atlas V Launches the Orbital Test Vehicle-1 Mission Overview Atlas V 501 Cape Canaveral Air Force Station, FL Space Launch Complex 41 Atlas V/OTV-1 United Launch (ULA) Alliance is proud to support the
CENTAUR OPTIONALLY-PILOTED AIRCRAFT ULTIMATE FLEXIBILITY FOR AIRBORNE SENSING
CENTAUR OPTIONALLY-PILOTED AIRCRAFT ULTIMATE FLEXIBILITY FOR AIRBORNE SENSING CENTAUR A NEW LEVEL OF OPERATIONAL FLEXIBILITY Aurora Flight Sciences Centaur combines the best of manned and unmanned surveillance
AN 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
TABLE OF CONTENTS. Thank you for your interest in CUAir
SPONSORSHIP INFORMATION 2018-2019 TABLE OF CONTENTS The Team Subteams The Competition Theia II Accomplishments 2019 Air System Outreach Why Contribute Sponsorship Levels 2017-2018 Sponsors Contact Us 3
w w w. o n e r a. f r
www. onera. fr Pioneering concepts for Personal Air Transport Systems PPlane Project AMPERE Project Hybrid electrical propulsion study PPlane : a pioneering concept for Personal Air Transport Systems The
De-orbiting technology developments at Surrey
De-orbiting technology developments at Surrey Prof G. S. Aglietti & Dr A. Viquerat University of Surrey Mar 2015 Content Background Deorbiting technology demonstrators InflateSail Active Debris Removal
KEEP TRACK OF WHAT MATTERS
KEEP TRACK OF WHAT MATTERS AUTOMATIC PASSENGER COUNTING SOLUTIONS For subways, trains, trams and train stations Automatic Passenger Counting For Subways, Trains, Trams and Train Stations INFODEV offers
AMSAT-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
Boeing CST-100. Commercial Crew Transportation System. Keith Reiley, The Boeing Company. February, 2011
Boeing CST-100 Commercial Crew Transportation System Keith Reiley, The Boeing Company February, 2011 BOEING is a trademark of Boeing Management Company. Commercial Crew Transportation System (CCTS) Design
LlSA Pathfinder PROPULSION MODULE MECHANICAL INTERFACE CONTROL DOCUMENT. UK EXPORT CONTROL RATING : 9E001 Rated By : K. Tomkins.
~. ~~~ EADS+ ASTRIUM LlSA Pathfinder Page 1 of 24 PROPULSION MODULE MECHANICAL INTERFACE CONTROL DOCUMENT CI CODE: 1241000 UK EXPORT CONTROL RATING : 9E001 Rated By : K. Tomkins Prepared by:... ~~~ ~ ~...
Development Status of H3 Launch Vehicle -To compete and survive in the global commercial market-
32 Development Status of H3 Launch Vehicle -To compete and survive in the global commercial market- TOKIO NARA *1 TADAOKI ONGA *2 MAYUKI NIITSU *3 JUNYA TAKIDA *2 AKIHIRO SATO *3 NOBUKI NEGORO *4 The H3
CIPHERING & DECIPHERING UNITS
CIPHERING & DECIPHERING UNITS High throughput Ciphering / Deciphering Unit Telecommand Deciphering Unit HIGH THROUGHPUT CIPHERING / DECIPHERING UNIT Satellite Telecommand / Telemeasure Protection, Spreading
Smart cities & effective mobility management solutions - 25 th March, San Paulo ViajeoPLUS Latin American Innovation week.
Smart cities & effective mobility management solutions - 25 th March, San Paulo ViajeoPLUS Latin American Innovation week. SWARCO AG Content Global changes & Challenges Smart City Effective Mobility solutions
BY HOEYCOMB AEROSPACE TECHNOLOGIES. HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV
BY HOEYCOMB AEROSPACE TECHNOLOGIES HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV Content SYSTEM SPECIFICATI- ON TYPICAL USING PROCESS OVERVIEW SUBSYSTEM SPECIFICATI- ON 1 OVERVIEW System
Dual Spacecraft System
Dual Spacecraft System Brent Viar 1, Benjamin Colvin 2 and Catherine Andrulis 3 United Launch Alliance, Littleton, CO 80127 At the AIAA Space 2008 Conference & Exposition, we presented a paper on the development