Thor Delta L
In-activeMcDonnell Douglas (MDC)
Aug. 27, 1969
Description
American orbital launch vehicle family with Thor first stage and a delta second stage.
Specifications
-
Stages
4 -
Length
35.0 m -
Diameter
2.44 m -
Fairing Diameter
2.44 m -
Launch Mass
89 T -
Thrust
1452 kN
Family
-
Name
Thor Delta L -
Family
― -
Variant
Delta L -
Alias
― -
Full Name
Thor Delta L
Payload Capacity
-
Launch Cost
$16540000 -
Low Earth Orbit
300 kg -
Geostationary Transfer
Orbit
300 kg -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
McDonnell Douglas
Commercial
None
MDCNone
Thor Delta L | HEOS 2
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
Jan. 31, 1972, 5:20 p.m.
Status: Launch Successful
Mission:
HEOS 2 was a spin-stabilized spacecraft with a highly eccentric orbit whose apogee occurred at high latitude. Its primary scientific mission was the investigation of interplanetary space and the high-latitude magnetosphere and its boundary in the region around the northern neutral point.
Elliptical OrbitThor Delta L | Pioneer E
McDonnell Douglas | United States of AmericaCape Canaveral, FL, USA
Aug. 27, 1969, 9:59 p.m.
Status: Launch Failure
Mission:
Pioneer A to E (Pioneer 6 to 9 after launch) were a series of five solar-orbiting, spin-stabilized, solar-cell and battery-powered satellites designed to obtain measurements of interplanetary phenomena from widely separated points in space on a continuing basis.
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