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.
Long March 2D
Success
4 x SatNet test satellites
Launch Area 4 (SLS-2 / 603) - Jiuquan Satellite Launch Center, People's Republic of ChinaOfficially described as "Satellite-Internet Technology Demonstration Satellites". Probable 4 test satellites for the Chinese state-owned LEO communic…
Falcon 9
Success
Fram2
Launch Complex 39A - Kennedy Space Center, FL, USAFram2 is the world’s first astronaut mission to polar orbit. Named after the Norwegian polar research ship Fram, the Crew Dragon spacecraft will laun…
Falcon 9
Success
Starlink Group 6-80
Space Launch Complex 40 - Cape Canaveral SFS, FL, USAA batch of 28 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Spectrum
Failure
Maiden Flight
Orbital Launch Pad - Andøya SpaceportFirst flight of the Isar Spectrum launch vehicle.
Long March 7A
Success
TJSW-16
201 - Wenchang Space Launch Site, People's Republic of ChinaChinese classified satellite claimed to be for communication technology test purposes. Actual mission not known.
