'Thermal control' diaporamas de présentation

Design of Thermal Control Sub-System(TCS) Picosat course May 18, 2006

Design of Thermal Control Sub-System(TCS) Picosat course May 18, 2006 IAA,National Cheng Kung University, Tainan J. H. Chou Department of Engineering Science National Cheng Kung University. Outline I. Review of TCS key concepts II. Design considerations III. YamSat thermal design

788 views • 47 slides

The Giant Magellan Telescope

The Giant Magellan Telescope. AAS San Diego January 11, 2005. Matt Johns. The GMT Institutions. Carnegie Observatories Harvard University Smithsonian Astrophysical Observatory Massachusetts Institute of Technology University of Arizona University of Michigan University of Texas, Austin

835 views • 32 slides

Thermal Control for Improved Productivity in Die Casting Review of Recent Reports

Thermal Control for Improved Productivity in Die Casting Review of Recent Reports NADCA DMC-Oak Ridge June 13, 2007. Advantages of high thermal conductivity inserts: Lower surface temperature leading to Longer die life Finer microstructure with improved mechanical properties

372 views • 30 slides

HELLO

HELLO. SIAMOIS in Dome-C. Overall Description. Divided in four sub-systems : A dedicated Telescope with its Bonnette (telescope guiding and fiber coupling). An Interferometer and a Camera. A structure for thermal and mechanical control. A command/control software system.

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M1 Thermal Control

M1 Thermal Control. 25 August 2003 ATST CoDR. Dr. Nathan Dalrymple Air Force Research Laboratory Space Vehicles Directorate. -0.69x10 -6 K -1. 0.28x10 -6 mbar -1. Primary Mirror (M1) Thermal Control. Function: Mitigate mirror seeing. seeing. Requirements. Minimize mirror seeing

381 views • 26 slides

354 views • 22 slides

Solar Orbiter - Remote Sensing Payload Working Group

Solar Orbiter - Remote Sensing Payload Working Group Mid-term meeting - 25-26 November 2002, ESTEC. Monday 25 November & Tuesday 26 November (Room: Einstein) Start: 11:00 PWG Plenary #1 - Welcome and introduction (Marsden) - Aims of meeting (Marsden and Rando)

453 views • 21 slides

WWW.CORBETTLIFESCIENCE.COM

Combining robust engineering , advanced performance and a palmtop PC interface for supreme user-friendly flexibility. WWW.CORBETTLIFESCIENCE.COM. Why a Palmtop PC Interface?. Familiar Windows operating system Allows total flexibility in cycle programming

524 views • 15 slides

Communications Conceptual Design Review

Communications Conceptual Design Review. Karim Barakat. Presentation Outline. Derived Requirements Subsystem Overview Antenna Selection LP-1 Resting Geometry Coverage Tx Data Rate Requirement Link Budget Dielectric Loss of Regolith Schedule. Derived Requirements. Subsystem Overview.

236 views • 12 slides

Universe of SERB-Approved Payloads

MidSTAR II United States Naval Academy Small Satellite Program Prof. Billy R. Smith, Jr., PhD Director. Universe of SERB-Approved Payloads.

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SNAP Electrical Design Estimates

Super Nova/Acceleration Probe. SNAP Electrical Design Estimates. November 16 , 2001 C. Paul Earle. SNAP Functional Block Diagram. Thermal Control & Monitoring. Bright Object Detector. Shutter Control. FPA. S/C C&DH. FPE. ICE. 1553 I/F. Scene. Readout Control Logic.

264 views • 12 slides

Peter Hansen 734-763-6241 pehansen@umich

PROJECT OVERVIEW. Peter Hansen 734-763-6241 pehansen@umich.edu. System Requirements. L-band NEDT: < 0.1 K desired, < 0.5 K required Absolute calibration: < 2 K desired, < 3 K required Linear dynamic range: 5 K < Tb < 300 K Ambient operating temperature range: -30 o C < To < +40 o C

199 views • 11 slides

Nikhef Activities on CO 2 Cooling

Picture: LHCb-VELO evaporator. Nikhef Activities on CO 2 Cooling. Bart Verlaat, Nikhef Introduction meeting with FOM director W. van Saarloos. 1. CO 2 cooling @ Nikhef (1). Evaporative CO 2 cooling is very promising for detectors:

239 views • 11 slides

Development of Cryogenic mounting system

Development of Cryogenic mounting system. Ke Ma and Dae-Sik Moon. Introduction. IR spectroscopy. IR spectrometer. Some basics on IR spectrometer. Process of Detector Mount Design. Outline the requirements Researching of design concepts from similar instruments

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Final Presentation Back-up Slides Orbital Transfer Vehicle (OTV) Power and Thermal Control

Final Presentation Back-up Slides Orbital Transfer Vehicle (OTV) Power and Thermal Control. Ian Meginnis. OTV Power Subsystems. Solar Array. <200V. Solar Array. Acronym Definitions: PCDU - Power Conditioning and Distribution Unit PPU - Power Processing Unit LL - Lunar Lander

222 views • 8 slides

Thermal Management

213 views • 7 slides

Orbital Transfer Vehicle (OTV) Thermal Control

Orbital Transfer Vehicle (OTV) Thermal Control. Ian Meginnis February 26, 2009 Group Leader - Power Systems Phase Leader - Translunar Injection OTV Power Systems OTV Thermal Control. Electronics Board Thermal Control. Hall Thruster Thermal Control. Acronym Definitions:

291 views • 7 slides

Intermittent Kangaroo Mother Care

Intermittent Kangaroo Mother Care. Intermittent KMC. Intermittent KMC is practiced with infants: Where incubators or warm rooms are available Who are not yet clinically stable Who are receiving oxygen therapy

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LBT Q4 2008 Engineering and Software Review

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The Corot Space instrument

The Corot Space instrument. Description of the Corot mission. Corot is a small mission of the CNES integrated on the PROTEUS spacecraft, launched by a Soyuz in mid-2006. Mass : 300kg / Power : 300W / Polar Orbit : 896km / Life Time : 2.5 years

153 views • 4 slides