- Explorer 2
Infobox_Spacecraft
Name = Explorer 2
Organization =Army Ballistic Missile Agency
Major_Contractors =Jet Propulsion Laboratory
Mission_Type =Earth science
Satellite_Of =Earth
Launch =March 5 ,1958 at 18:28 UTC
Launch_Vehicle =Jupiter-C
Mission_Duration = 0 days
NSSDC_ID = EXPLR2
Webpage = [http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=EXPLR2 NASA NSSDC Master Catalog]
Mass = 14.52 kg (31.36 lb) [ cite web
url = http://history.nasa.gov/sputnik/expinfo.html
title = Data Sheet - Explorer Information
accessdate = 2008-02-02
publisher = Department of Astronautics,National Air and Space Museum ,Smithsonian Institution ]Explorer 2 (EXPLR2) was to be a repeat of the
Explorer 1 mission. However, due to a failure in the rocket during launch, the spacecraft did not reach orbit.Explorer 2 was launched from
Cape Canaveral Air Force Station (nowKennedy Space Center ) LC-26a inFlorida onMarch 5 ,1958 at 18:28 UTC, by aJupiter-C launch vehicle.cite web
url = http://www.planet4589.org/space/lvdb/launch/Redstone
title = Launch Vehicle Database - Redstone
accessdate = 2008-02-03
publisher = JSR] The Jupiter-C has its origins in the United States Army'sProject Orbiter in1954 . The project was canceled in1955 , when the decision was made to proceed withProject Vanguard .Following the launch of the Soviet
Sputnik 1 onOctober 4 ,1957 , theArmy Ballistic Missile Agency (ABMA) was directed to proceed with the launching of a satellite using the Jupiter-C, which had already been flight-tested in nose-cone re-entry tests for the Jupiter IRBM (intermediate-range ballistic missile ). Working closely together, ABMA andJet Propulsion Laboratory (JPL) completed the job of modifying the Jupiter-C and building the Explorer 1 in 84 days.Spacecraft design
Explorer 2 was equipped with a
Geiger counter for the purposes of detectingcosmic ray s. AfterExplorer 3 , it was decided that the original Geiger counter had been overwhelmed by strong radiation coming from a belt of charged particles trapped in space by theEarth's magnetic field (see:Van Allen radiation belt ). Explorer 2 was also equipped with a wire grid array and an acoustic detector for the purpose of micrometeorite detection.Mission results
Due to a malfunction in the Jupiter-C launch vehicle, the fourth stage did not ignite. [cite web
url = http://msl.jpl.nasa.gov/Programs/explorer.html
title = Mission and Spacecraft Library - Explorer Program
accessdate = 2008-02-02
publisher =Jet Propulsion Laboratory ] Subsequently Explorer 2 did not reach orbit.References
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