Names | Vanguard Space Launch Vehicle-Six |
---|---|
Mission type | Solar heating of Earth |
Operator | Naval Research Laboratory |
Mission duration | Failed to orbit |
Spacecraft properties | |
Spacecraft | Vanguard 3B |
Spacecraft type | Vanguard |
Manufacturer | Naval Research Laboratory |
Launch mass | 10.8 kg (24 lb) |
Dimensions | 50.8 cm (20.0 in) of diameter |
Start of mission | |
Launch date | 22 June 1959, 20:16:09 GMT |
Rocket | Vanguard SLV-6 |
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 | 3840 km |
Inclination | 34.20° |
Period | 134.0 minutes |
Vanguard SLV-6, also called Vanguard Satellite Launch Vehicle-Six, hoped to be the third successful flight of the American Vanguard rocket following the successful Vanguard 2 satellite on rocket Vanguard SLV-4. Vanguard Satellite Launch Vehicle-6 (SLV-6) was designed to carry a small spherical satellite into Earth orbit to study solar heating of Earth and the heat balance. A faulty second stage pressure valve caused a mission failure.