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Explorer 2

Explorer II
Explorer 1
Organization: Army Ballistic Missile Agency
Major Contractors: Jet Propulsion Laboratory
Mission Type: Earth Science
Satellite of: Earth
Launch: March 5, 1958 - Failed to orbit
Launch Vehicle: Jupiter-C 4th stage did not ignite
Decay: March 5, 1958
Mission Duration: 0 days
Mass: 14.52 kg (8.5 kg instruments)
NSSDC ID: none
Webpage: NASA NSSDC Master Catalog
Orbital elements
Semimajor Axis: 0 km
Eccentricity: .0
Inclination:
Orbital Period: 0 minutes
Apogee: 0 km
Perigee: 0 km
Orbits: 0
Instruments
Geiger-Mueller detector : Detection of cosmic rays
Wire grid array : Micrometeorite detection
Acoustic detector : Micrometeorite detection
Contents

Mission Description

Explorer-II was to be a repeat of the Explorer I mission. However, there was a launch failure in the Jupiter-C rocket and Explorer II did not reach orbit.

The satellite was launched from Cape Canaveral (now Kennedy Space Center) in Florida on March 5, 1958, by a Jupiter-C launch vehicle.

The Jupiter-C has its origins in the United States Army's Project Orbiter in 1954. The project was canceled in 1955, however, when the decision was made to proceed with Project Vanguard.

Following the launch of the Soviet Sputnik I on October 4, 1957, 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 and JPL completed the job of modifying the Jupiter-C and building the Explorer-I in 84 days.

Spacecraft Design

Explorer II was equipped with a geiger counter for the purposes of detecting cosmic rays. After Explorer III, 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)

Mission Results

Explorer II failed to reach orbit due to Jupiter-C launch vehicle malfunction. Attempted orbit of Explorer-II (14.52 kg with 8.5 kg of instruments) failed because fourth stage did not ignite.

See Also

Reference

Previous Mission:
Explorer I
Explorer program Next Mission:
Explorer 3
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