Thor Able II
In-activeMcDonnell Douglas (MDC)
Jan. 23, 1959
Description
American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.
Specifications
-
Stages
2 -
Length
27.3 m -
Diameter
2.44 m -
Fairing Diameter
2.44 m -
Launch Mass
52.0 T -
Thrust
668.0 kN
Family
-
Name
Thor Able II -
Family
― -
Variant
Able II -
Alias
― -
Full Name
Thor Able II
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
McDonnell Douglas
Commercial
None
MDCNone
Thor Able II | Tiros 1
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
Thor Able II | Transit 1A
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
Kinetica 2
Success
SpaceSail Polar Group #17
Launch Area 140 - Jiuquan Satellite Launch Center, People's Republic of China18 Low Earth Orbit communication satellites with Ku, Q and V band payloads for the G60 constellation operated by Shanghai Spacesail Technologies with…
Electron
Success
The Sea God Surveys (iQPS Launch 9)
Rocket Lab Launch Complex 1A - Rocket Lab Launch Complex 1, Mahia Peninsula, New ZealandSynthetic aperture radar Earth observation satellite for Japanese Earth imaging company iQPS.
Falcon 9
Success
Starlink Group 15-18
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 27 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
GSLV Mk II
Success
IRNSS-1L (NVS-03)
Satish Dhawan Space Centre Second Launch Pad - Satish Dhawan Space Centre, IndiaThis is a replacement satellite for the Indian Regional Navigation Satellite System. The constellation will provide India with an alternative to GPS …
Falcon 9
Success
Starlink Group 15-16
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 27 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
