Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
scientific equation
|
| gptkbp:alsoKnownAs |
ideal rocket equation
|
| gptkbp:appliesTo |
gptkb:satellite
rockets |
| gptkbp:assumes |
constant exhaust velocity
no external forces except thrust |
| gptkbp:describes |
motion of vehicles that follow the principle of conservation of momentum
|
| gptkbp:field |
astronautics
physics |
| gptkbp:form |
Δv = ve * ln(m0 / mf)
|
| gptkbp:formedBy |
gptkb:Konstantin_Tsiolkovsky
1903 |
| https://www.w3.org/2000/01/rdf-schema#label |
Tsiolkovsky rocket equation
|
| gptkbp:influenced |
rocket science
space exploration |
| gptkbp:m0 |
initial mass
|
| gptkbp:mf |
final mass
|
| gptkbp:usedFor |
calculating required propellant mass
mission planning in spaceflight |
| gptkbp:variant |
ve
m0 mf Δv |
| gptkbp:ve |
effective exhaust velocity
|
| gptkbp:Δv |
change in velocity
|
| gptkbp:bfsParent |
gptkb:Rocketry
|
| gptkbp:bfsLayer |
4
|