Thor Delta G

In-active

McDonnell Douglas (MDC)

Dec. 14, 1966

Description

American orbital launch vehicle family with Thor first stage and a delta second stage.

Specifications
  • Stages
    3
  • Length
    30.0 m
  • Diameter
    2.44 m
  • Fairing Diameter
    2.44 m
  • Launch Mass
    55.0 T
  • Thrust
    765.0 kN
Family
  • Name
    Thor Delta G
  • Family
  • Variant
    Delta G
  • Alias
  • Full Name
    Thor Delta G
Payload Capacity
  • Launch Cost
    $10150000
  • Low Earth Orbit
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

McDonnell Douglas

Commercial
None
MDC

None

Thor Delta G | Biosat 2

McDonnell Douglas | United States of America
Cape Canaveral SFS, FL, USA
Sept. 7, 1967, 10:04 p.m.
Status: Launch Successful
Mission:

The objectives of the Biosatellite, a.k.a. Biosat, Bios (Biological Satellite), were to determine the biological effects of the space environment upon daily rhythms of living organisms and to obtain and analyze available data on the performance in orbit of life support, altitude control, and other spacecraft systems, including instrumentation for recording biological data.

Low Earth Orbit
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Thor Delta G | Biosat 1

McDonnell Douglas | United States of America
Cape Canaveral SFS, FL, USA
Dec. 14, 1966, 7:20 p.m.
Status: Launch Successful
Mission:

The objectives of the Biosatellite, a.k.a. Biosat, Bios (Biological Satellite), were to determine the biological effects of the space environment upon daily rhythms of living organisms and to obtain and analyze available data on the performance in orbit of life support, altitude control, and other spacecraft systems, including instrumentation for recording biological data.

Low Earth Orbit
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