A small repair drone of mass 6.0kg drifts near a disabled satellite. Two identical cold-gas thrusters mounted orthogonally on the drone can fire in the +x and +y directions, respectively. A sequence of computer-controlled pulses is executed while on-board sensors record data.
Piecewise description of the net external force components on the drone (SI units):
Interval I: 0≤t<1.5s
• Fx=+9.0N
• Fy=+12.0N
Interval II: 1.5s≤t<3.0s
• Fx=0N
• Fy=+12.0N
Interval III: 3.0s≤t<4.0s
• Fx=−9.0N (opposite the +x direction)
• Fy=0N
Interval IV: t≥4.0s
• Fx=0N
• Fy=0N
At t=0 the drone is momentarily at rest at the origin of an inertial coordinate system: r0=0 and v0=0. Neglect gravitational and other external influences.
(a) For each interval, calculate the drone’s acceleration components ax and ay.
(b) Determine the drone’s velocity components immediately after the end of each interval (at t=1.5s, t=3.0s, and t=4.0s).
(c) Compute the drone’s position vector at t=4.0s.
(d) Describe the drone’s motion for t>4.0s, and explain how your answer illustrates Newton’s first law and the concept of dimensional independence.
(e) Suppose an unexpected micro-meteorite strike at t=5.0s delivers an impulse purely in the +y direction. Without performing additional calculations, predict qualitatively how the x and y components of the drone’s velocity will be affected and justify your reasoning.