Thor Able I
In-activeMcDonnell Douglas (MDC)
April 24, 1958
Description
American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.
Specifications
-
Stages
2 -
Length
30.0 m -
Diameter
2.44 m -
Fairing Diameter
2.44 m -
Launch Mass
51 T -
Thrust
667 kN
Family
-
Name
Thor Able I -
Family
― -
Variant
Able I -
Alias
― -
Full Name
Thor Able I
Payload Capacity
-
Launch Cost
$8900000 -
Low Earth Orbit
120 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
McDonnell Douglas
Commercial
None
MDCNone
Thor Able I | Pioneer 2
McDonnell Douglas | United States of AmericaCape Canaveral, FL, USA
Nov. 8, 1958, 7:30 a.m.
Thor Able I | Pioneer 1
McDonnell Douglas | United States of AmericaCape Canaveral, FL, USA
Oct. 11, 1958, 8:42 a.m.
Thor Able I | Able I (Pioneer)
McDonnell Douglas | United States of AmericaCape Canaveral, FL, USA
Aug. 17, 1958, 12:18 p.m.
Falcon 9
Success
Starlink Group 6-59
Space Launch Complex 40 - Cape Canaveral, FL, USAA batch of 23 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Soyuz 2.1b/Fregat-M
Success
Kosmos 2576
43/4 (43R) - Plesetsk Cosmodrome, Russian FederationRussian military payload of unknown purposes. Hitchhiking Payloads: SITRO-AIS 53-56; Zorkiy-2M-4 & 6
Falcon 9
Success
Starlink Group 8-7
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 20 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Falcon 9
Success
Starlink Group 6-58
Space Launch Complex 40 - Cape Canaveral, FL, USAA batch of 23 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Long March 4C
Success
Shiyan 23
Launch Area 4 (SLS-2 / 603) - Jiuquan Satellite Launch Center, People's Republic of ChinaSatellite officially named for "space environment detection" purposes, exact details unknown.
