Rocket engines are most effective when exhaust gases escape from their nozzles at the same pressure as the surrounding atmosphere.
Conclusion (Thus)
To work most effectively throughout their ascents, all rockets must have both short nozzles and long nozzles on their engines.
Evidence
To work most effectively, rocket engines need their exhaust gases to be the same pressure as the surrounding atmosphere.
A short nozzle matches the pressure of low altitudes, whereas a long nozzle matches the pressure in the thin upper atmosphere.
Evaluate
Because the conclusion is conditional "to do X, it must be that Y", we might be wise to guess that LSAT is testing a missing link. Is there any new term in the conclusion?
Throughout their ascents / all rockets is new. The evidence talked about short/long nozzles and defined what it means for a rocket to work most effectively.
You need a short nozzle for low altitudes and a long nozzle for the thin upper atmosphere. So I guess the author is assuming that
If we were trying to use an Objection mindset, we'd be thinking,
Maybe some rockets only ascend to low altitudes, so they could get away with just having short nozzles. Maybe some rockets only "turn on" once they reach the thin upper atmosphere, so they could get by with just long nozzles.
Goal
Look for an answer dealing with the new Conclusion language (throughout their ascents, all rockets) establishing that we will be dealing with both low altitudes and the thin upper atmosphere, or look for an answer ruling out an objection like the ones we made.