'Reaction wheels' diaporamas de présentation

An Introduction to FORMOSAT-3/COSMIC

Speaker: Yi-Fan Chang Advisor: Prof. Jian-Jiun Ding 2012/12/07. An Introduction to FORMOSAT-3/COSMIC. Outline. Introduction System and Mission Overview GPS Radio Occultation Current Status Data Analysis Discussion Conclusion Reference. Outline. Introduction

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Orbital Analysis for Inter-Calibration Dave Mac Donnell Brooke Anderson

Orbital Analysis for Inter-Calibration Dave Mac Donnell Brooke Anderson Bruce Wielicki Don Garber NASA Langley Research Center Solar Workshop January 30, 2009. CLARREO Crossing Below Aqua 700km. Aqua MODIS, CERES, or AIRS Crosstrack Scan . D. Garber LaRC, 7/07. CLARREO 100 km nadir fov.

489 views • 26 slides

Mark Clampin (GSFC) John Stansberry (STScI)

Mark Clampin (GSFC) John Stansberry (STScI). JWST Operations. JWST Observatory Status. Image Quality. 150 nm @ NIRCam focal plane: 2 m m diffraction limit Note: performance specified to short wavelength cameras WFE budget contributors include:

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X-Ray Calorimeter Mission

295 views • 22 slides

Pruned Design Option Tree ADCS

Pruned Design Option Tree ADCS. Selected ADS concepts. Maryland Aerospace Inc . IMI-100 ADACS Sun Sensors and a Star Tracker GPS based attitude control. Sources: http://www.cubesatkit.com/docs/datasheet/DS CSK ADACS 634-00412-A.pdf

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176 views • 8 slides

ESTREMO/WXT Initiative: AAS-I Contribution

ESTREMO/WXT Initiative: AAS-I Contribution. ESTREMO/WXT: Preliminary Consideration. For preliminary ESTREMO feasibility evaluation the basic consideration are about: Launch capability (mass, firing volume, firing height) of Vega for LEO Payload Accommodation Fast pointing

181 views • 8 slides

Time to Complete 50m/s ? V & 100g Payload System Overview

Time to Complete 50m/s ? V & 100g Payload System Overview. Brittany Waletzko 100g Payload Integration Manager Translunar /OTV Phase Week 9. 50m/s ? V Maneuver (Requirement). ? V = ?T /m dt = 50 m/s. t = ? V m T T = instantaneous thrust (assumed constant over interval)

141 views • 6 slides