Astronomy:Explorer 2
 Launch of Explorer 2 | |
| Mission type | Earth science |
|---|---|
| Operator | Army Ballistic Missile Agency |
| Mission duration | Launch failure |
| Spacecraft properties | |
| Manufacturer | Jet Propulsion Laboratory |
| Launch mass | 14.52 kilograms (32.0 lb)[1] |
| Start of mission | |
| Launch date | March 5, 1958, 18:28 UTC |
| Rocket | Juno I RS/CC-26 |
| Launch site | Cape Canaveral Air Force Station Cape Canaveral Air Force Station Launch Complex 26 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Medium Earth |
| Epoch | Planned |
Explorer program | |
Explorer 2 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 Cape Canaveral Air Force Station Launch Complex 26 in Florida on March 5, 1958 at 18:28 UTC by a Juno-I launch vehicle.[2] The Juno-I had its origins in the United States Army's Project Orbiter in 1954. The project was canceled in 1955 when the decision was made to proceed with Project Vanguard.
Following the launch of the Soviet Sputnik 1 on October 4, 1957, the Army Ballistic Missile Agency (ABMA) was directed to proceed with the launching of a satellite using the Juno-I four-stage variant of the three-stage 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 and Jet Propulsion Laboratory (JPL) completed the job of modifying the Jupiter-C and building Explorer 1 in 84 days.
Spacecraft design
Explorer 2 was equipped with a Geiger counter for the purposes of detecting cosmic rays. After Explorer 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 the Earth'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
Explorer 2 failed to reach orbit after a malfunction in the Juno-I launch vehicle caused the fourth stage to not ignite.[3]
References
- ↑ "Data Sheet - Explorer Information". Department of Astronautics, National Air and Space Museum, Smithsonian Institution. https://history.nasa.gov/sputnik/expinfo.html. Retrieved 2008-02-02.
- ↑ "Launch Vehicle Database - Redstone". JSR. http://www.planet4589.org/space/lvdb/launch/Redstone. Retrieved 2008-02-03.
- ↑ "Mission and Spacecraft Library - Explorer Program". Jet Propulsion Laboratory. Archived from the original on 2008-01-27. https://web.archive.org/web/20080127144116/http://msl.jpl.nasa.gov/Programs/explorer.html. Retrieved 2008-02-02.
External links
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