Function | Expendable launch system |
---|---|
Country of origin | United States |
Capacity | |
Payload to LEO | |
Altitude | 350 nautical miles (650 km; 400 mi) |
Mass | 800 pounds (360 kg)[1] |
Payload to Earth escape trajectory | |
Mass | 130 pounds (59 kg)[1] |
Launch history | |
Status | Retired[2] |
Launch sites | Cape Canaveral LC-17[3] |
Total launches | 9 |
Success(es) | 8 |
Failure(s) | 1 |
First flight | 13 December 1962 |
Last flight | 19 March 1964 |
The Delta B, or Thor-Delta B was an American expendable launch system used for nine orbital launches between 1962 and 1964.[3] A derivative of the Thor-Delta, it was a member of the Delta family of rockets.[4]
The first stage was a Thor missile in the DM-21 configuration, and the second stage was the AJ10-118,[1] which was derived from the earlier Delta-A.[4] An Altair solid rocket motor was used as a third stage.[1]
All nine launches occurred from Cape Canaveral Air Force Station Launch Complex 17.[3] Most of the launches carried communications satellites, including Syncom-1[2] and Syncom-2.[2] Syncom-1 was intended to be the first satellite to be placed into a geosynchronous orbit, however the spacecraft malfunctioned prior to reaching this orbit.[5] Syncom-2 subsequently became the first geosynchronous satellite,[5] and was placed at 55° west of the Greenwich Meridian. The final launch failed due to third stage underperformance,[6] all other launches were successful.[3]