Thor Able I

In-active

McDonnell Douglas (MDC)

April 24, 1958

Description

American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.

Specifications
  • Stages
    2
  • Length
    30.0 m
  • Diameter
    2.44 m
  • Fairing Diameter
    2.44 m
  • Launch Mass
    51.0 T
  • Thrust
    667.0 kN
Family
  • Name
    Thor Able I
  • Family
    ―
  • Variant
    Able I
  • Alias
    ―
  • Full Name
    Thor Able I
Payload Capacity
  • Launch Cost
    $8900000
  • Low Earth Orbit
    120.0 kg
  • Geostationary Transfer Orbit
    ―
  • Direct Geostationary
    ―
  • Sun-Synchronous Capacity
    ―

McDonnell Douglas

Commercial
None
MDC

None

Previous Flights

flew on three previous launch(es).

Thor Able I | Pioneer 2

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

The third pioneer orbiter, pioneer 2 intended to enter lunar orbit but failed to make orbit when the third stage failed to ignite.

Lunar Orbit
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Thor Able I | Pioneer 1

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

The second pioneer orbiter, pioneer 1 intended to enter lunar orbit but missed the Moon after a third stage partial failure.

Lunar Orbit
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Thor Able I | Able I (Pioneer)

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

The first pioneer orbiter, pioneer 0 was a lunar orbiter intended to enter a lunar orbit for observation. However, the mission failed 77 seconds into launch.

Lunar Orbit
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