'Launch vehicle' diaporamas de présentation

Satellite System and Engineering Procedure-An Introduction

Satellite System and Engineering Procedure-An Introduction. Instructor: Roy C. Hsu Computer Science and Information Engineering Department National Chia-Yi University 10/05/2006. OUTLINE. Introduction Satellite System Engineering Procedure Cases Study. INTRODUCTION.

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Mars Exploration Rovers and Two Year Highlights

http://mars.jpl.nasa.gov/mer/gallery/artwork/rover2browse.html. Mars Exploration Rovers and Two Year Highlights. Assembly, Test and Launch. Rover . Two Earth Year Highlights of the Rovers Spirit Opportunity . Reference Information .

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PHOENICS USER CONFERENCE MOSCOW 2002

PHOENICS USER CONFERENCE MOSCOW 2002. The problem of exhaust plume radiation during the launch phase of a spacecraft. Attilio Cretella, FiatAvio, Italy and Dr. Tony Smith, S & C Thermofluids Limited United Kingdom. Contents. Introductions - F iatAvio Introductions - S & C Thermofluids

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International Cooperation: Working Together to Get to Mars

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John Carey Evan Goldstein CII Team 21 April 2011

Common Instrument Interface (CII) Environmental Guidelines DRAFT. John Carey Evan Goldstein CII Team 21 April 2011. Design Goals.

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Bretton Alexander Executive Director for Space X PRIZE Foundation

Bretton Alexander Executive Director for Space X PRIZE Foundation. X PRIZE Foundation. Not-for-profit educational foundation Offers incentive prizes to create radical breakthroughs for the benefit of all humanity Ansari X PRIZE for Suborbital Spaceflight

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REUSABLE LAUNCH VEHICLE (RLV) DEVELOPMENT WORKING GROUP EXPORTS 30 MAY 2000

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2010 Commercial GSO Demand Forecast

2010 Commercial GSO Demand Forecast. 19 May 2010. Chris Kunstadter Senior Vice President XL Insurance chris.kunstadter@xlgroup.com. Cover art by John Sloan/FAA. Agenda. Membership and Methodology Statistics Market Assessment and Trends Summary. Working Group Members.

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Team A Propulsion

Team A Propulsion. 1/16/01. Presentation Outline. Chemical Propulsion: Expansion of gases as a result of chemical interaction/combustion Thermonuclear Propulsion: Expansion of gases as a result of heating by a nuclear generator

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The mission of HSFL is to: promote innovative engineering and science research for terrestrial and planetary space missi

The mission of HSFL is to: promote innovative engineering and science research for terrestrial and planetary space missions. develop, launch, and operate small spacecraft from the Hawaiian Islands to accelerate the validation of new space technologies.

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ISS Commercial Resupply Services

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The Ariane 5 Launcher Failure

The Ariane 5 Launcher Failure. June 4th 1996 Total failure of the Ariane 5 launcher on its maiden flight. Ariane 5. A European rocket designed to launch commercial payloads (e.g.communications satellites, etc.) into Earth orbit Successor to the successful Ariane 4 launchers

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Outline

Outline. Science goals, mission name (bonus for acronym and logo!!) Define telescope and instrument Choose orbit Calculate data volume, rate and downlink Calculate pointing requirements Select spacecraft bus Determine launch mass Select launch vehicle Describe major risks

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COMSTAC Risk Management Working Group October 28, 2009

COMSTAC Risk Management Working Group October 28, 2009. Chris Kunstadter XL Insurance chris.kunstadter@xlgroup.com. Risk Management Working Group. Extension of CSLA indemnification Three-year extension passed House and sent to Senate Combined Meeting with Space Transp Ops WG

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Assessment of Alternate Methodologies for Establishing Equivalent Satisfaction of the Ec Criterion for Launch Licensing

Assessment of Alternate Methodologies for Establishing Equivalent Satisfaction of the Ec Criterion for Launch Licensing. Terry Hardy AST-300/Systems Engineering and Training Division May 19, 2004. Project Description.

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Mission data

Mission data. Launch vehicle data. Mission payloads. Delta 4 Heavy US. 2 x [3 SSME + 2 x 4-Segment SRB, Inline]. 2 x [3 SSME + 2 x 4-Segment SRB, Side-Mount]. 2 x [4 SSME + 2 x 5-Segment SRB, Inline]. 1 x [4 SSME + 2 x 5-Segment SRB, In-line]. NEO Mission (2 Crew). GEO Mission (4 Crew).

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Leyte Normal University Tacloban, City

Leyte Normal University Tacloban, City. Lunar Reconnaissance Orbiter Title Presented by: Valiant M. Fegi. Time Launch Mission: Lunar Reconnaissance Orbiter (LRO) Launch Vehicle: United Launch Alliance Atlas V Launch Site: Cape Canaveral Air Force Station, Fla.

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Tim Lorenzana 1/16/2008 Avionics Recovery/Termination

Tim Lorenzana 1/16/2008 Avionics Recovery/Termination. Rocket Recovery. Parachute Impact System Airbags Retro Rockets Rotating Wing Helicopter Action. Nylon 496.05grams/meter $12.14meter Launch Vehicle Mass 100.5kg Parachute Diameter 1.06meters Parachute Mass 2.22kg

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Engineering Team Support for the Roadmap Committee

Engineering Team Support for the Roadmap Committee. Mary DiJoseph GSFC Tim VanSant GSFC Ron Muller GFSC/QSS Pete Cline GSFC Regan Howard GSFC Gregg Marr GSFC Neil Murphy JPL Juan Ayon JPL Janine Daughters JPL. Engineering Team Support for Roadmap mission studies.

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Name that Launch Vehicle!

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