A 1.2×103kg spacecraft already experiences a 1.8kN force directed along +x due to the solar wind. Its main engine can provide thrusts up to 20kN in any direction. Mission control requires the craft to accelerate at 15m/s2 in a direction 30∘ above the +x axis (in the xy-plane).
Which of the following best states the additional engine thrust magnitude needed and whether the requirement is within the engine’s capability?
a) 20kN; requirement is just at the limit
b) 17kN; requirement is achievable
c) 16kN; requirement is achievable
d) 18kN; requirement is achievable