Engineering:Delta B

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Short description: Retired American expendable rocket
Delta B
Thor Delta B with TIROS 8 (Dec. 21 1963).gif
Delta B prior to the launch of TIROS-8
FunctionExpendable launch system
Country of originUnited States
Capacity
Payload to LEO800 pounds (360 kg)[1]
Payload to Earth escape trajectory130 pounds (59 kg)[1]
Launch history
StatusRetired[2]
Launch sitesCape Canaveral Air Force Station LC-17[3]
Total launches9
Successes8
Failures1
First flight13 December 1962
Last flight19 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]

References