equation 27.53 eq:cfs-kepler-third-exact
open in the book ·
parts/03-classical-mechanics/10-central-forces-statics.tex:1274
- part of a statement or proof
Rests on
- step_from equation 27.52 eq:cfs-orbit-integral ¶
- step_from equation 27.41 eq:cfs-relative-eom ¶
- step_from equation 27.49 eq:cfs-semi-major ¶
Supports
- depends_on example 27.36 A satellite in low Earth orbit ¶
Neighborhood
Every logical edge within two steps of this node.
- declared and complete
- partly declared
- a check failed
- not graded
- declared in the source
- inferred from structure
Edges
| type | direction | node | provenance | where |
|---|---|---|---|---|
step_from |
→ | eq:cfs-orbit-integral | declared — integrating the equal-area law over one revolution and eliminating $p$ and $L$ | parts/03-classical-mechanics/10-central-forces-statics.tex:1277 |
step_from |
→ | eq:cfs-relative-eom | declared — integrating the equal-area law over one revolution and eliminating $p$ and $L$ | parts/03-classical-mechanics/10-central-forces-statics.tex:1277 |
step_from |
→ | eq:cfs-semi-major | declared — integrating the equal-area law over one revolution and eliminating $p$ and $L$ | parts/03-classical-mechanics/10-central-forces-statics.tex:1277 |
depends_on |
← | A satellite in low Earth orbit | declared | parts/03-classical-mechanics/10-central-forces-statics.tex:1359 |