Thor Able IV
In-activeMcDonnell Douglas (MDC)
March 11, 1960
Description
American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.
Specifications
-
Stages
3 -
Length
27.2 m -
Diameter
2.44 m -
Fairing Diameter
2.44 m -
Launch Mass
52.0 T -
Thrust
668.0 kN
Family
-
Name
Thor Able IV -
Family
― -
Variant
Able IV -
Alias
― -
Full Name
Thor Able IV
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
McDonnell Douglas
Commercial
None
MDCNone
Thor Able IV | Pioneer V
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
March 11, 1960, 1 p.m.
Falcon 9
Success
Starlink Group 11-23
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 28 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Long March 2
Success
Shenzhou 21
Launch Area 4 (SLS-1 / 921) - Jiuquan Satellite Launch Center, People's Republic of ChinaTenth crewed flight to the Chinese space station.
Falcon 9
Success
Starlink Group 10-37
Space Launch Complex 40 - Cape Canaveral SFS, FL, USAA batch of 29 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Falcon 9
Success
Starlink Group 11-21
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 28 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Falcon 9
Success
Starlink Group 10-21
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.
