'Heat shield' diaporamas de présentation

Fleece

791 views • 56 slides

The FIELDS Experiment

The FIELDS Experiment. Prof. Stuart D. Bale University of California, Berkeley. Agenda. Investigation team Overview Driving requirements Primary measurement requirements Design description Interface definition Heritage Changes since Proposal Technology development plan

568 views • 49 slides

Disassemble, Assemble and Perform a Function Check on the M249

Disassemble, Assemble and Perform a Function Check on the M249. Terminal Learning Objective. Action: Disassemble, Assemble and Perform a Function Check on the M249 Squad Automatic Weapon (SAW)

1.19k views • 31 slides

DHE Chassis and Cooling

DHE Chassis and Cooling. DES Mechanical Workshop at FNAL November 2, 2005 Vaidas Simaitis High Energy Physics Group University of Illinois at Urbana-Champaign. 6-SLOT + 4-SLOT CHASSIS. FAN MANIFOLDS ADDED. FANS ADDED. COOLING MANIFOLDS ADDED. HEAD EXCHANGERS ADDED.

494 views • 30 slides

IRENE PROGRAM

IRENE PROGRAM. I talian R e- E ntry N acell E Preliminary Study. 1 0th INTERNATIONAL Planetary Probe WORKSHOP June 17-21, 2013. BACKGROUND OF THE ACTIVITY (1/2).

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Mars and Titan

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Progress and Paper report

Progress and Paper report. Sept 23, 2009. Progress. SPP Manuscript was accepted Evaporation of a multilayer coating with low transmission in the Infrared region A. K. Ang1, P.V. Ramos, M. L. Jamero and I. B. Culaba. Introduction.

324 views • 23 slides

APOLLO SPACECRAFT

APOLLO SPACECRAFT. Daniel McCaffery Jeff Robinson Kyle Smith Jason Tang Brad Thompson. Project Apollo. The national effort that enabled Astronaut Neil Armstrong to speak those words as he stepped onto the lunar surface, fulfilled a dream as old as humanity.

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276 views • 18 slides

Production Solenoid Environment

Production Solenoid Environment. RSVP Simulation Review New York University January 12 2005. Vladimir Tumakov University of California, Irvine. Proton beam simulation PS and TS coil hitting in beam normal and fail conditions Validation of energy load simulation. The MECO Apparatus.

272 views • 16 slides

IPPW-9

333 views • 15 slides

IPPW-9

347 views • 15 slides

Aerodynamics

313 views • 12 slides

Preliminary Heat Shield Design for nEDM

Preliminary Heat Shield Design for nEDM. Ernie Ihloff 21 May 08. Heat Shield Design Choices. Meets Physics requirement for experiment Limits heat load to inner volumes Reliable design; no leaks or failures Manufacturability, Serviceability and Cost Support scheme that addresses movement

258 views • 11 slides

Wave-Ty Application

Wave-Ty Application. Wave-Ty on Heat Shield. Wave-Ty Application. Automotive - apply heat shield to an exhaust. Wave-Ty Application. Wave-Ty on truck engine. Wave-Ty Application. Dura-Ty Application. Dura-Ty Application. Dura-Ty Application. Pipeline Protection. Dura-Ty Application.

282 views • 10 slides

Conceptual design and prototype testing of the water-cooled production target. Fabrication of the target and support systems is contained in WBS 1.4.4

212 views • 9 slides

Mars Surveyors

Mars Surveyors. Spacecraft Dimensions 1.06 meters (3.5 feet) tall by 3.6 meters (12 feet) wide. Spacecraft Weight Total: 576 kg (1,270 pounds) Lander: 290 kg (639 pounds) Propellant: 64 kg (141 pounds) Cruise Stage: 82 kg (181 pounds) Aeroshell & Heat Shield: 140 kg (309 pounds)

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HOT DOG Roasters

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AEROFAST : THERMAL/ABLATION ANALYSIS OF THE FRONT HEAT SHIELD FOR A MARTIAN AEROCAPTURE MISSION

Cork based TPS. Silicon based glue. CFRP. Aluminum honeycomb. CFRP. S/D=0.482. S/D=0.561. AEROFAST : THERMAL/ABLATION ANALYSIS OF THE FRONT HEAT SHIELD FOR A MARTIAN AEROCAPTURE MISSION A.J. van Eekelen, G. Pinaud, J.-M. Bouilly. Problem description.

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X-Ray Computed Tomography Inspection

186 views • 1 slides