Thor Delta C1

In-active

McDonnell 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
MDC

None

Previous Flights

flew on three previous launch(es).

Thor Delta C1 | OSO 5

McDonnell Douglas | United States of America
Cape Canaveral SFS, FL, USA
Status: Launch Successful
Mission:

OSO (Orbital Solar Observatory) satellite. Its purpose was to return data on the ultraviolet, X-ray and gamma ray emissions of the sun and galaxy.

Low Earth Orbit
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Thor Delta C1 | OSO 4

McDonnell Douglas | United States of America
Cape Canaveral SFS, FL, USA
Status: Launch Successful
Mission:

OSO (Orbital Solar Observatory) satellite. Its purpose was to return data on the ultraviolet, X-ray and gamma ray emissions of the sun and galaxy.

Low Earth Orbit
Explore Share

Thor Delta C1 | Explorer 32

McDonnell Douglas | United States of America
Cape Canaveral SFS, FL, USA
Status: Launch Successful
Mission:

AE B (Aeronomy Explorer B) was an aeronomy satellite which was designed to directly measure temperatures, composition, densities, and pressures in the upper atmosphere on a global basis.

Low Earth Orbit
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