Thor Burner 2A
In-activeMcDonnell Douglas (MDC)
Oct. 14, 1971
Description
The Thor-Burner was an American expendable launch system, a member of the Thor rocket family. It consisted of a Thor missile, with one or two Burner upper stages.
Specifications
-
Stages
3 -
Length
23.0 m -
Diameter
2.44 m -
Fairing Diameter
2.44 m -
Launch Mass
50.0 T -
Thrust
750.0 kN
Family
-
Name
Thor Burner 2A -
Family
― -
Variant
Burner 2A -
Alias
― -
Full Name
Thor Burner 2A
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
McDonnell Douglas
Commercial
None
MDCNone
Thor Burner 2A | DMSP-5C F3
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
Feb. 19, 1976, 7:52 a.m.
Thor Burner 2A | DMSP-5C F2
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
May 24, 1975, 3:22 a.m.
Thor Burner 2A | DMSP-5C F1
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
Aug. 9, 1974, 3:22 a.m.
Thor Burner 2A | DMSP-5B F5
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
March 16, 1974, 8 a.m.
Thor Burner 2A | DMSP-5B F4
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
Aug. 17, 1973, 4:49 a.m.
Thor Burner 2A | DSAP-5B F3
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
Nov. 9, 1972, 3:23 a.m.
Thor Burner 2A | DMSP-5B F2
McDonnell Douglas | United States of AmericaVandenberg SFB, CA, USA
March 24, 1972, 8:46 a.m.
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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.
