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- W2187817998 abstract "Anexperimental micro-satellite project acceptsobservation dataandinformation. Thequality ofinformation a numberof characteristics typically denouncedin derived fromearthobservation dataandusedforthese commercialspacecraft development. Theseincludeapplications ishighly dependent on dataspecifications, acceptance ofhighrisk, little component redundancy ofthe including spatial, spectral, andtemporal resolution. Asthese experiments, low-precision control, non-optimal designs, specifications improve, thetechnology advanceswill andlimited mission duration. Itisproposed touseamicro-encourage greater interest inanduseofearth observation data satellite asaplatform fortheresearch anddevelopment of andtechniques. Thegeneral application topics served byearth microsystemtechnology to enhancetheknowledgeobservation technology arepublic services administration, infrastructure of microsystemtechnology and itsnatural resource management, environmental assessment and applications inspace. Thepresent research isfocused on management, disaster management, and otherunique microsystems withemphasis onlowermass, lowervolume,applications (1). lower powerandenhanced flexibility/reco nfigurability. The Fromtheearly 1980's advances inmicroelectronics andtheir experimental microsatellite provides anopportunity for massproduction, as wellas improvements in COTS commercial oftheshelf component andsystem (sensors and components reliability, haveenable microandsmall satellites actuators) qualification, monitoring itsbehavior inaspacetobemanufactured andlaunched within short time-scale and environment andautonomous system experiments. tight budgets. Surrey Satellite Technology Ltd.(SSTL) inthe EgyptIris-1 micro-satellite isanexperimental remoteUK haspioneered theuseofmicro-satellites weighing less than sensing satellite ofsmallphysical sizeandmass,will100Kg(2). Also, there aremanyUniversities, Institutes, and operate inaNearEarthOrbitandhaveagroundsamplingSpaceCenters intheworldundergoing MicroandSmall distance intherange(10-15)m, whichwillallowmany Satellite projects inrecent years (3-1 1). civilian services. EgyptIris-1 project aimsatenhancementEgyptshowed aninterest inusing micro-satellite inEarth ofscientific capabilities andexperience inthefield of observation applications. TheNational Authority forRemote satellite technologies andspace-born Earthobservation for Sensing andSpaceScience (NARSS), whichbelongs to thebenefit ofscience andtechnology toserveinpeaceful Egyptian Ministry ofHighEducation andScientific Research, useofsuchproject. Also, within thepartnership frameworkannounced in2001thestart ofanambitious program for we aim tomanagetheproject as a geographically developing amicro-satellite Egyptsat-1 (12) tooperate inalow distributed teamsbuilding different subsystems of Earth Orbit (670 km)forremotesensing applications launched EgyptIris-1 andcombining aswellexisting knowledge and inMarch2007. experience ofpartners andenhancement ifenthusiasm and Asanational collaborative program (NARSS) space section, talent ofyoungstudents. Inaddition, animportant goalis withtheArabInternational Optronics (AIO) in1999(13) have todevelop arobust platform structure capable toservein built anddeveloped twoEarth Observation optical mechanical manylaunchvehicles anddifferent mission applications. units oneof310mm,andsecond of620mm focal lengths tobe Preliminary calculations willbecarried outtoinvestigate mounted asapayload onapeach airplane forEarth imaging. thesuitable orbittoachieve mission requirements and Oneofthese payloads shall bemodified tobetheEgyptIris-1 define theworstspaceenvironment parameters affecting satellite primary payload. thesatellite mission performance. The concept ofuse EgyptIris- 1shall carry apush-broom typesmall size aperture Commercial Of-The-Shelf (COTS)whilebuilding the cameratoprovide 10-15 m ofground sampling distance ina satellite subsystems isapproved toimprove thesatellite costpanchromatic bandatorbit altitude 300-450 km.A micro- effective mission life measure. Infuture asanambitious satellite busshall bedesigned tosupport payload operation plan,andafter validation ofthesystemoperation and requirements. Theattitude determination andcontrol subsystem evaluation ofthemission objectives comewithpositive shall bebased on3-axis stabilization method andshall benadir results, itishopedtoinvite otherinternational partners to pointed. Thesatellite shall bebaseline foraone-year mission. participate inbuilding aconstellation forthis issue." @default.
- W2187817998 created "2016-06-24" @default.
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- W2187817998 date "2007-01-01" @default.
- W2187817998 modified "2023-09-27" @default.
- W2187817998 title "Conceptual Mission Analysis forRSMicro-Satellite: EgyptIris- 1" @default.
- W2187817998 hasPublicationYear "2007" @default.
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