Key relationship
vesc=√(2GM/r); ε=½v²−GM/r; bound radial turning point rmax=−GM/ε.
Physics · Class 11
Escape occurs when the launch kinetic energy cancels or exceeds the negative gravitational potential energy. The escape speed depends on the central body and launch radius but not the probe mass.
Open the interactive experiment →விடுபடு வேகம் பொருளின் நிறையைப் பொறுத்ததல்ல. இயக்க ஆற்றல் ஈர்ப்பு நிலை ஆற்றலின் அளவை ஈடுகட்ட வேண்டும்.
vesc=√(2GM/r); ε=½v²−GM/r; bound radial turning point rmax=−GM/ε.
Escape occurs when the launch kinetic energy cancels or exceeds the negative gravitational potential energy. The escape speed depends on the central body and launch radius but not the probe mass.
Escape speed is not a continuously required cruising speed.
Radial launch outside Earth; no air resistance, rotation or thrust after launch. Exact zero total energy gives marginal escape with zero speed at infinity.
Use total energy to distinguish bound launch, marginal escape and unbound launch.
Try both scenarios, change one control, and predict the result before checking the graph and readouts.
Change one input while keeping the others fixed, as you would in a controlled experiment.
At Earth radius, vesc≈11.19 km/s. At four times that radius, escape speed halves to about 5.59 km/s.
The model connects test the escape-energy threshold with an observable reading. Check the equation and assumptions before applying it.
SI units · algebra · graph reading
What happens when launch speed equals escape speed?
At escape threshold ε=0, so no energy remains as kinetic energy at infinite radius.
Course connection: Class XI Chapter 7. Consult the roadmap for CBSE, NEET, JEE Main and Advanced scope.