'Flight model' diaporamas de présentation

The Cosmic R A y Telescope for the Effects of Radiation

420 views • 27 slides

Overview of a Space Qualification Process - Radiation characterization and beyond

Overview of a Space Qualification Process - Radiation characterization and beyond. L. BONORA, ESA/ESTEC-Component Division Xanthi - Oct 2006. SUMMARY. Radiation: effects on EEE components Radiation: tests & requirements

385 views • 24 slides

GLAST Large Area Telescope Calorimeter Subsystem

368 views • 24 slides

Mig-29 A Flight Model data

Mig-29 A Flight Model data. Section A : Mig-29 A (9.12) data. Dimensions. Lenght: 17,32m Height: 4,73m Wingspan: 11,36m Wing area: 38,056m^2 Overall lift area: 60,890m^2 Wing incidence: 0deg. Anhedral: 3deg. Wing aspect ratio: 3,339:1 Tailplane span: 7,78m Tailplane area: N/A

625 views • 22 slides

Orbiter: A Free Spacecraft Simulation Tool

Orbiter: A Free Spacecraft Simulation Tool. Orbiter: A Free Spacecraft Simulation Tool. Martin Schweiger Department of Computer Science University College London www.orbitersim.com. Martin Schweiger Department of Computer Science University College London www.orbitersim.com.

306 views • 22 slides

Fuel Tank Inerting Modeling

Fuel Tank Inerting Modeling. Ivor Thomas Consultant to FAA 1 425 455 1807 fuelsguy@msn.com. Background. Following TWA 800 the FAA undertook to examine fuel tank inerting to determine if a system could be made practical. Two ARAC studies FAA lab, ground and flight test programs

223 views • 21 slides

NOAA's Joint Polar Satellite System Climate Sensors

NOAA's Joint Polar Satellite System Climate Sensors. 92nd American Meteorological Society Annual Meeting Stephen Walters NOAA Climate Sensors Program Manager Mitch Goldberg, John Furgerson & Jim Gleason JPSS January 25, 2012 Stephen.Walters@noaa.gov. Climate Sensors Overview.

370 views • 18 slides

NPOESS Preparatory Project (NPP) Status

NPOESS Preparatory Project (NPP) Status . Jim Gleason NPP Project Scientist. Nunn-McCurdy Certification of NPOESS. NPOESS Program was certified by DoD Number of spacecraft reduced from 6 to 2+2 EUMETSAT will provide mid-morning coverage Operational Data Continuity was Primary Requirement

362 views • 15 slides

Company & Product Capabilities

405 views • 15 slides

HTAP model (inter) comparisons

249 views • 14 slides

Roberta Sparvoli for the PAMELA Collaboration

Uuuuuu Uuuu uuuuuuu. Roberta Sparvoli for the PAMELA Collaboration University of Rome Tor Vergata and INFN Roma II, Italy. PAMELA scientific program.

246 views • 12 slides

Schedule & Budget

Schedule & Budget. Gunther Haller Stanford Linear Accelerator Center. Organization (1). Includes T&DF, Power System, Flight Software Overall Organization for Modules System Architecture Boards Enclosures Assembly & Qualification Install & Test Components organized in

186 views • 11 slides

COROT

COROT. Main events from the last CW (Granada). INSTRUMENT The Baffle The problem (eigen frequencies) is understood, thanks to a very strong involvement of ESA, CNES and CSL technical teams. New design of the feet Qualification is successful

353 views • 10 slides

Space Magnetometers

358 views • 9 slides