TDRS-B was launched in the payload bay of Challenger, attached to an Inertial Upper Stage (IUS). It was to have been deployed from the Shuttle in low Earth orbit. The IUS would have then performed two burns to raise the satellite into a geosynchronous orbit. On the previous TDRS launch, TDRS-1, the IUS second-stage motor malfunctioned following the first-stage burn, resulting in a loss of control, and delivery of the satellite into an incorrect orbit.
Launch failed
TDRS-B was originally scheduled for launch on STS-12 in March 1984; however, it was delayed and the flight cancelled following the IUS failure on TDRS-1.[2] It was later re-manifested on STS-51-E; however, this too was cancelled due to concerns over the reliability of the IUS. It was eventually assigned to STS-51-L, which was also to carry the SPARTAN-Halley astronomy satellite.[3]
Once it reached orbit, TDRS-B was to have been given the operational designation TDRS-2. Although normal practice was to reassign operational designations in the event of launch failures, the TDRS-2 designation was not reassigned, and when TDRS-C was launched, it became TDRS-3. Debris from TDRS-B was recovered along with the wreckage of Challenger.
The TDRS-G satellite was ordered to replace TDRS-B.[6] It was launched from Space ShuttleDiscovery in 1995, on mission STS-70. It became TDRS-7 after reaching geosynchronous orbit.[4]
^ abMcDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 24 June 2009.
^The O-ring failed in the first seconds of liftoff, causing progressive malfunction that culminated in the structural failure of the liquid hydrogen tank, explosion of the hydrogen fuel, and breakup of the vehicle stack.
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).