18
$\begingroup$

We all know that the Space Shuttle Solid Rocket Boosters (SRB) were the pair of large solid rockets used by the United States' NASA Space Shuttle during the first two minutes of its powered flight. Together, they provided about 83% of liftoff thrust for the Space Shuttle.

What would have happened if the Solid Rocket Boosters didn't separate after the separation point?

$\endgroup$
  • $\begingroup$ This case happened due to modelling bugs in the Shuttle Mission Simulator at least once. The manual sep didn't work because of the particular model that was erroneous. The software didn't proceed to the next ops mode because SRB sep didn't happen; the crew could do it manually, but it was a mess. Ended up as a loss of control case. Sadly I don't remember many details. $\endgroup$ – Organic Marble Jun 15 '17 at 0:57
22
$\begingroup$

The empty SRBs would have added an additional mass to the vessel which would need to be carried into orbit until separation of the main tank. The additional fuel needed for this would mean that it would not have been possible to reach orbit.

The standard procedure for an abort between SRB separation and main-engine cut-off was the Transoceanic Abort Landing (TAL). The orbiter would have been separated from the external tank, continue on its sub-orbital trajectory and perform a landing on the designated abort runway in Europe (for every space shuttle launch, two different airports in Europe were prepared especially for this eventuality. It never happened).

Should the separation of the orbiter from the external tank also fail... well, the orbiter was unable to glide aerodynamically and land with the tank still attached, so this failure would have been catastrophic.

$\endgroup$
  • 3
    $\begingroup$ The answer assumes both SRBs fail to separate, a benign scenario. If one fails, it's a LOC event. $\endgroup$ – Deer Hunter Sep 22 '14 at 16:01
  • 3
    $\begingroup$ @DeerHunter LOC? $\endgroup$ – Everyone Sep 22 '14 at 17:53
  • 3
    $\begingroup$ Loss of Crew I think $\endgroup$ – 0x6adb015 Sep 22 '14 at 19:09
  • 3
    $\begingroup$ @DavidRicherby If the non-separated SRB is still firing at that point, the vector of thrust does not go through the shuttle's center of mass and you get the same effect you get in those spinny fireworks -- the offset thrust causes the whole to start spinning very rapidly. The Shuttle's control surfaces are not built to stabilize that kind of spin (and that's even assuming we have the space age materials we'd need to stand the kind of stresses involved)... $\endgroup$ – Shadur Sep 23 '14 at 8:12
  • 4
    $\begingroup$ @Shadur The SRBs do indeed have a self-destruct, which is operated from the ground. This was used after Challenger exploded: the SRBs continued flying after the orbiter broke up and they were deliberately destroyed to prevent them hitting the ground or ocean in one big, rocket-propelled piece. $\endgroup$ – David Richerby Sep 23 '14 at 8:32
6
$\begingroup$

The flight crew had a contingency procedure for this. On Panel C3 a switch allowed the crew to manually initiate the SRB separation sequence should the software fail to trigger it automatically. I don't believe this required a call up from the flight controllers.

enter image description here

$\endgroup$
  • $\begingroup$ I vaguely remember someone stating that this switch doesn't do anything other than trigger the automated processes in place that should've already been triggered. It won't instantly separate the stages if the SRBs are still burning or the software deems it unsafe, so if failures occurred to that part of the software, this switch wouldn't've done much. $\endgroup$ – Magic Octopus Urn Jul 27 '18 at 13:30
  • $\begingroup$ Actually according to a member of the SAIL team in 1986, the SRB sep had minimal checks before passing the command to the MEC. The ET sep on the other hand had a six second delay if conditions for ET sep were not nominal. After those 6 seconds ET sep would occur regardless of conditions. This was done at the request of the Astronaut office. It was felt that the Pilot should be in command in off nominal situations not the FSW. $\endgroup$ – Challenger Truth Jul 30 '18 at 16:52
  • $\begingroup$ If the physical element of SRB sep, the actual decoupling mechanism between the ET and the SRB, failed, then pushing the switch wouldn't be any good. It would just send another command to the flawed decoupling assembly. The thing is, in this case it's possible that only one failed. If only one fails, you're likely facing a loss of crew and vehicle scenario. $\endgroup$ – Ranga Rutiser Sundar May 16 at 15:22

Your Answer

By clicking “Post Your Answer”, you agree to our terms of service, privacy policy and cookie policy

Not the answer you're looking for? Browse other questions tagged or ask your own question.