Explorer 2

Explorer 2
Launch of Explorer 2 satellite
NamesExplorer II
Mission typeEarth science
OperatorJPL / Army Ballistic Missile Agency
Mission durationFailed to orbit
120 days (planned)
Spacecraft properties
SpacecraftExplorer II
Spacecraft typeScience Explorer
BusExplorer 1
ManufacturerJet Propulsion Laboratory
Launch mass14.22 kg (31.3 lb)
Dimensions203 cm (80 in) length
15.2 cm (6.0 in) diameter
Power60 watts
Start of mission
Launch date5 March 1958, 18:27:57 GMT[1]
RocketJuno I (RS-26)
Launch siteAtlantic Missile Range, LC-26A
ContractorArmy Ballistic Missile Agency
End of mission
DestroyedFailed to orbit
Orbital parameters
Reference systemGeocentric orbit (planned) [2]
RegimeMedium Earth orbit
Perigee altitude358 km (222 mi)
Apogee altitude2,550 km (1,580 mi)
Inclination32.24°
Period114.80 minutes
Instruments
Geiger counter
Micrometeorite Detector
Satellite Drag Atmospheric Density
Resistance Thermometers
Thermometers
Explorer program

Explorer 2 was an American unmanned space mission within the Explorer program. Intended to be a repetition of the previous Explorer 1 mission, which placed a satellite into medium Earth orbit, the spacecraft was unable to reach orbit due to a failure in the launch vehicle during launch.

Explorer 2 was launched from Cape Canaveral Missile Test Center of the Atlantic Missile Range (AMR), LC-26A in Florida on 5 March 1958 at 18:27:57 GMT by a Juno I launch vehicle.[3] 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.

  1. ^ Cite error: The named reference JSR1 was invoked but never defined (see the help page).
  2. ^ "Trajectory: Explorer-1 1958-001A". NASA. 14 May 2020. Retrieved 13 February 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  3. ^ "Launch Vehicle Database - Redstone". Jonathan's Space Report. Archived from the original on 10 October 2007. Retrieved 13 February 2021.