Flight system
Built to move mass beyond the atmosphere.
American orbital launch vehicle family with Thor first stage and a delta second stage.
Thor · Delta E
American orbital launch vehicle family with Thor first stage and a delta second stage.
Height
31 m
Diameter
2.44 m
LEO capacity
540 kg
Manufacturer
McDonnell Douglas
Total launches
6
Successful
6
Pending
0
Successful landings
0
Flight system
American orbital launch vehicle family with Thor first stage and a delta second stage.
Mission record
Apr 20, 1967
Vandenberg SFB, CA, USA
Jan 26, 1967
Vandenberg SFB, CA, USA
Oct 2, 1966
Vandenberg SFB, CA, USA
Feb 28, 1966
Cape Canaveral SFS, FL, USA
Dec 16, 1965
Cape Canaveral SFS, FL, USA
Nov 6, 1965
Cape Canaveral SFS, FL, USA