Names | Explorer II |
---|---|
Mission type | Earth science |
Operator | JPL / Army Ballistic Missile Agency |
Mission duration | Failed to orbit 120 days (planned) |
Spacecraft properties | |
Spacecraft | Explorer II |
Spacecraft type | Science Explorer |
Bus | Explorer 1 |
Manufacturer | Jet Propulsion Laboratory |
Launch mass | 14.22 kg (31.3 lb) |
Dimensions | 203 cm (80 in) length 15.2 cm (6.0 in) diameter |
Power | 60 watts |
Start of mission | |
Launch date | 5 March 1958, 18:27:57 GMT[1] |
Rocket | Juno I (RS-26) |
Launch site | Atlantic Missile Range, LC-26A |
Contractor | Army Ballistic Missile Agency |
End of mission | |
Destroyed | Failed to orbit |
Orbital parameters | |
Reference system | Geocentric orbit (planned) [2] |
Regime | Medium Earth orbit |
Perigee altitude | 358 km (222 mi) |
Apogee altitude | 2,550 km (1,580 mi) |
Inclination | 32.24° |
Period | 114.80 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.
JSR1
was invoked but never defined (see the help page).