Names | Vanguard Space Launch Vehicle-3 |
---|---|
Mission type | International Geophysical Year |
Operator | Naval Research Laboratory |
Mission duration | Failed to orbit |
Spacecraft properties | |
Spacecraft | Vanguard 2D |
Spacecraft type | Vanguard |
Manufacturer | Naval Research Laboratory |
Launch mass | 10.6 kg (23 lb) |
Dimensions | 50.8 cm (20.0 in) of diameter |
Start of mission | |
Launch date | 26 September 1958, 15:38 GMT |
Rocket | Vanguard SLV-3 |
Launch site | Cape Canaveral, LC-18A |
Contractor | Glenn L. Martin Company |
End of mission | |
Decay date | Failed to orbit |
Orbital parameters | |
Reference system | Geocentric orbit (planned) |
Regime | Medium Earth orbit |
Perigee altitude | 655 km |
Apogee altitude | 3970 km |
Inclination | 34.20° |
Period | 134.0 minutes |
Vanguard SLV-3, also called Vanguard Satellite Launch Vehicle-3 hoped to be the second successful flight of the American Vanguard rocket following successful Vanguard 1 satellite on rocket Vanguard TV-4.