Oberth effect

E1000696

The Oberth effect is a principle in astrodynamics where a rocket produces more useful kinetic energy from the same amount of propellant when it performs a burn at higher speeds, typically near a gravitational body.

All labels observed (1)

Label Occurrences
Oberth effect canonical 1

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf astrodynamics concept ⓘ
physical effect ⓘ
appliesTo chemical rockets ⓘ
electric propulsion systems ⓘ
rockets ⓘ
spacecraft propulsion ⓘ
basedOn classical mechanics ⓘ
conservation of energy ⓘ
kinetic energy equation ⓘ
category orbital maneuvers ⓘ
rocket propulsion phenomena ⓘ
spaceflight mechanics ⓘ
consequenceOf kinetic energy scaling with the square of velocity ⓘ
nonlinear relationship between velocity and energy ⓘ
contrastsWith naive delta-v-only mission optimization ⓘ
describedByFormula ΔE = 1/2 m[(v+Δv)^2 − v^2] = m v Δv + 1/2 m (Δv)^2 ⓘ
field astrodynamics ⓘ
orbital mechanics ⓘ
spaceflight dynamics ⓘ
hasKeyIdea a rocket produces more useful kinetic energy when burning propellant at higher speed ⓘ
burns deep in a gravity well can be more energetically efficient ⓘ
energy gain from a burn depends on current velocity as well as delta-v ⓘ
kinetic energy change is proportional to velocity times delta-v ⓘ
performing a burn near periapsis maximizes kinetic energy gain ⓘ
historicallyAttributedTo Hermann Oberth ⓘ
implies deep-space burns at low speed are less energy-efficient than periapsis burns ⓘ
for the same delta-v, more energy is gained at higher initial speed ⓘ
namedAfter Hermann Oberth ⓘ
occursNear gravitational bodies ⓘ
periapsis of an orbit ⓘ
optimizationGoal maximize energy gain per unit propellant ⓘ
practicalImplication combine gravity assists with high-speed burns for large energy changes ⓘ
perform major burns at the lowest possible orbital altitude ⓘ
time burns to coincide with periapsis passage ⓘ
relatedTo Hohmann transfer orbit ⓘ
Tsiolkovsky rocket equation ⓘ
bi-elliptic transfer ⓘ
delta-v budget ⓘ
gravity assist ⓘ
specific orbital energy ⓘ
timePeriod early 20th century ⓘ
typicalLocation low Earth orbit ⓘ
periapsis of interplanetary transfer orbits ⓘ
usedIn bi-elliptic transfer planning ⓘ
capture maneuvers at planets ⓘ
escape trajectory design ⓘ
gravity assist maneuvers ⓘ
interplanetary mission design ⓘ

How these facts were elicited

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

Tsiolkovsky rocket equation → relatedTo → Oberth effect ⓘ