Thor Delta C1
In-activeMcDonnell Douglas (MDC)
May 25, 1966
Description
American orbital launch vehicle family with Thor first stage and a delta second stage.
Specifications
-
Stages
3 -
Length
27.5 m -
Diameter
2.44 m -
Fairing Diameter
2.44 m -
Launch Mass
52.0 T -
Thrust
756.0 kN
Family
-
Name
Thor Delta C1 -
Family
― -
Variant
Delta C1 -
Alias
― -
Full Name
Thor Delta C1
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
81.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
McDonnell Douglas
Commercial
None
MDCNone
Thor Delta C1 | OSO 5
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
Jan. 22, 1969, 4:48 p.m.
Thor Delta C1 | OSO 4
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
Oct. 18, 1967, 3:58 p.m.
Thor Delta C1 | Explorer 32
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
May 25, 1966, 2 p.m.
Soyuz 2.1b/Fregat-M
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