Close the torque and work boundary of an orbital change
Conservation applies to a defined system. An orbiting body subject to an external torque can gain orbital angular momentum; that does not violate conservation when the driver is included. Similarly, orbital energy can increase through work. A mechanism such as interaction with another body or a disk needs a complete exchange ledger rather than the assertion that every orbit must conserve its own quantities while being driven.
Learning outcome: Vary final radius at fixed mass, then mass at fixed endpoints. Close ΔE and ΔL, compare their ratio with endpoint angular rates and identify the driver that a complete physical conservation argument would need to include.
Starting recap
Retain relative versus barycentric geometry, time versus angle, fitted versus instantaneous velocity and complete energy/angular-momentum boundaries.
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For m=2 and R=4, L changes from 2 to 4, so ΔL=2. E changes from −1 to −0.25, so ΔE=0.75. The mean work/torque-transfer ratio is 0.375 per time, between endpoint rates 1 and 0.125. Multiplying the final rate by ΔL would give only 0.25 energy units and miss the changing rate.
Open the experimentPredict
Can a body move outward to a slower circular orbit while gaining total orbital energy?
Experiment
Vary final radius at fixed mass, then mass at fixed endpoints. Close ΔE and ΔL, compare their ratio with endpoint angular rates and identify the driver that a complete physical conservation argument would need to include.
Account for external torque and work between circular states
Worked teaching model · synthetic values · Original quasi-static sequence of circular states around fixed μ=1, initial radius 1. L=m√r and E=−m/(2r); external torque/work changes orbital L and E. Along this ideal sequence dE/dL=Ω=r^(−3/2). The driver belongs in a complete conservation boundary; no physical migration mechanism is assumed.
Reset keeps your prediction, captures and practice history.
An outward circular-state change requires both angular-momentum gain and less-negative orbital energy.
The orbit alone is not an isolated system while a driver exerts torque and work. Along the ideal circular sequence, integrate Ω dL rather than multiplying the entire transfer by the final angular rate. A real tidal, disk or spacecraft mechanism requires its own energy and angular-momentum ledger.
| Quantity | Value | Unit |
|---|---|---|
| Initial orbital angular momentum | 2 | mass length²/time |
| Final orbital angular momentum | 4 | mass length²/time |
| Required angular-momentum gain | 2 | mass length²/time |
| Initial orbital energy | -1 | energy |
| Final orbital energy | -0.2500000 | energy |
| Required orbital energy gain | 0.7500000 | energy |
| Mean work per angular-momentum transfer | 0.3750000 | per time |
| Initial circular angular rate | 1 | per time |
| Final circular angular rate | 0.1250000 | per time |
| Mistaken final-rate times angular-momentum gain | 0.2500000 | energy |
These original models are not measured orbit records or operational mission instructions. Retain the frame, assumptions and missing evidence before interpreting a real system.
An outward circular-state change requires both angular-momentum gain and less-negative orbital energy.
The orbit alone is not an isolated system while a driver exerts torque and work. Along the ideal circular sequence, integrate Ω dL rather than multiplying the entire transfer by the final angular rate. A real tidal, disk or spacecraft mechanism requires its own energy and angular-momentum ledger.
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Use m=1 and R=4. Find ΔL, ΔE and their ratio; explain which results scale with mass.
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