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How does a spacecraft's speed change when the engine burns versus coasts?

Research question: When a spacecraft's engine burns for only a few minutes and then coasts for days, how does its speed relative to Earth change during the burn compared with the coast?

The records show that a burn adds speed: the Oberth Effect says a burn accelerates a vehicle most effectively at periapse, where it moves fastest 2, and it gives more kinetic energy when executed at higher speeds 10. As one example, the Vanguard second-stage engine was designed to burn for only 2 minutes, boosting the rocket to about 19,000 miles per hour 22. After the burn, the vehicle moves ballistically with no further propulsion 618, but the facts do not state how its speed relative to Earth changes during the coast. The ZK spiral source describes burn-then-free-flight patterns yet explicitly does not state how speed changes in each phase 17.

Checked 2026-10-21. Only documented and supported facts are used.
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Sources

[1] supported
The Oberth manoeuvre is a burn performed close to the Sun, where a sustained high-thrust burst is used to add kinetic energy to the probe.
"The VASIMR ® performs a slingshot pass or Oberth manoeuvre close to the Sun.With solar electric propulsion, the effect of the Oberth manoeuvre is boosted by using the high level of available solar energy to produce a sustained burst of high thrust."
Solar and Hybrid Electric Propulsion to the Kuiper Belt and Beyond (2021)
[2] supported
The Oberth Effect says a burn accelerates a vehicle most effectively when it is performed at periapse, the point of the orbit closest to the central body where the vehicle moves fastest.
"In fact the principle known as the Oberth Effect describes how a burn is most effective in accelerating a vehicle when it is conducted at the periapse of the spacecraft’s orbit."
Using the Two-Burn Escape Maneuver for Fast Transfers in the Solar System and Beyond (2010)
[3] supported
The burn near the Sun gives the probe enough kinetic energy within one AU to reach Jupiter's orbit or beyond.
"This trajectory provides enough kinetic energy to the probe within one AU to reach Jupiter orbit or beyond."
Solar and Hybrid Electric Propulsion to the Kuiper Belt and Beyond (2021)
[4] supported
The VASIMR-powered solar Oberth manoeuvre reaches a speed above 60 km/s at its maximum velocity.
"The VASIMR ® powered solar Oberth manoeuvre reaches a speed > 60 kps at maximum velocity."
Solar and Hybrid Electric Propulsion to the Kuiper Belt and Beyond (2021)
[5] documented
In the two-burn maneuver, the first burn slows the spacecraft so that it drops further into the central body's gravity well.
"the first burn decelerates the spacecraft resulting in a trajectory that takes it further into the gravity well of the central mass"
Using the Two-Burn Escape Maneuver for Fast Transfers in the Solar System and Beyond (2010)
[6] supported
After the near-perihelion SEP-SOM thrust arc, the spacecraft coasts ballistically on its outbound trajectory with no further propulsion.
"after which the spacecraft coasts ballistically"
High-temperature photovoltaics for solar-electric Oberth maneuvers: ton-class payload feasibility for interstellar-precursor missions (2026)
[7] supported
The second burn is timed for periapse of the new elliptical orbit, where it accelerates the spacecraft out of the central body's gravity well.
"The second burn is performed at the periapse of the new elliptical orbit and accelerates the spacecraft out of the gravity well of the central mass."
Using the Two-Burn Escape Maneuver for Fast Transfers in the Solar System and Beyond (2010)
[8] supported
An Oberth maneuver happens when a spacecraft falls into the Sun's gravitational well and fires its engine as it reaches its maximum speed, so the burn occurs at the point of highest orbital speed.
"Also known as an Oberth maneuver, it occurs when a spacecraft falls into the Sun’s gravitational well and performs an impulsive burn as it reaches its maximum speed."
Combined Heat Shield and Solar Thermal Propulsion System for an Oberth Maneuver (2023)
[9] supported
The Crew-12 Dragon capsule's deorbit burn, which used its Draco thrusters, was expected to last 9.5 minutes.
"The deorbit burn, which involves Freedom's Draco thrusters, started at 10:46 a.m. EDT (1446 GMT) and is expected to last 9.5 minutes."
NASA SpaceX Crew-12 flight latest news: Landing day nears for Dragon astronauts
[10] supported
The Oberth effect means a spacecraft gains more kinetic energy from a manoeuvre when the burn is executed at higher speeds, typically near the closest approach to the body it orbits.
"a spacecraft can gain more kinetic energy from a manoeuvre when it is executed at higher speeds, typically at its closest to the centre of a celestial body it is orbiting"
Development of a Kick Stage and Trajectory Optimisation for Large Interplanetary Scientific Missions (2024)
[11] supported
After the burns, Ship 41 was planned to coast for about eight hours in orbit before a deorbit burn, rather than burning its engines during the coast.
"Ship will enter an approximately eight-hour coast phase. At the end of a nominal coast phase, the spacecraft will complete a deorbit burn to target a soft splashdown off the coast of Chile."
SpaceX Starship Flight 14 live updates: Mission success!
[12] supported
The deorbit burn finished as planned after about 9.5 minutes, and the capsule jettisoned its trunk shortly after engine shutdown.
"The Freedom capsule's deorbit burn went as planned, wrapping up at 10:56 a.m. EDT (1456 GMT) after about 9.5 minutes."
NASA SpaceX Crew-12 flight latest news: Landing day nears for Dragon astronauts
[13] supported
For cryogenic stages with boil-off, the Oberth effect's benefit is outweighed by fuel losses, so immediate engine firing is needed for optimal fuel use rather than waiting to burn at higher speed.
"outweighing the losses due to the Oberth effect and necessitating immediate engine firing for the optimal fuel usage"
Development of a Kick Stage and Trajectory Optimisation for Large Interplanetary Scientific Missions (2024)
[14] supported
Ship 41 completed its first-ever orbital insertion burn at about 170 miles altitude, shortly before its payload deployment began.
"Ship 41 has completed its first-ever orbital insertion burn an altitude of approximately 170 miles (275 kilometers)."
SpaceX Starship Flight 14 live updates: Mission success!
[15] supported
After undocking from the International Space Station, the Crew-12 Dragon capsule had a roughly 27-hour coast back to Earth.
"Freedom undocked from the station on Wednesday morning (Oct. 7), kicking off a roughly 27-hour trip home to Earth."
NASA SpaceX Crew-12 flight latest news: Landing day nears for Dragon astronauts
[16] supported
After its launch-day deployment, the Dragon capsule coasted on a 2-day trip to the International Space Station.
"The Dragon capsule then floated free to begin a 2-day trip to the International Space Station."
NASA SpaceX Crew-12 flight latest news: Landing day nears for Dragon astronauts
[17] supported
The document says that for small k, the ZK spiral trajectory closely resembles a series of patched conic orbits produced by impulsive burns separated by long ballistic free-flight periods, which is the burn-then-coast pattern the question describes. It does not state how speed relative to Earth changes during each phase.
"For small k, the ZK spiral is very similar to the trajectory obtained using a series of “patched conic orbits” produced by a series of impulsive burns, separated by long periods of ballistic free-flight paths"
The ZK Spiral Family of Trajectories and Forces (2024)
[18] supported
After its second stage burns out, the missile nose continues onward without propulsion, moving ballistically like a thrown rock along a long arc.
"like a rock hurled into a long arc through the sky."
Image 3 of Evening star (Washington, D.C.), April 24, 1958
[19] supported
After the powered burnout at about 140 miles altitude, the second and third stage combination coasts upward without thrust until it reaches the satellite's orbit about 300 miles above Earth.
"After its burnout, at about i 140 miles altitude, the second and third stage combination will coast upward until it reaches the satellite’s orbit 300 miles above the earth"
Image 7 of Evening star (Washington, D.C.), March 21, 1956
[20] supported
The spacecraft accelerates only in short thrusting bursts, with about an hour of thrust before it must coast for several hours to recharge its batteries.
"After approximately an hour of accelerating it is expected to need to coast for several hours to recharge its batteries, resulting in a relatively high frequency stop-go-stop thrust profile."
Trajectory design for a very-low-thrust lunar mission. (2013)
[21] supported
The Thor-Vanguard nose cone, after the powered phase, needed only about 30 minutes to cover the roughly 5,500 miles to the Ascension Island area, far faster than the jet-powered Snark's 8 or 9 hours.
"required only about 30 minutes to travel to the Ascension Is Island"
Image 3 of Evening star (Washington, D.C.), April 24, 1958
[22] documented
The Vanguard second-stage engine was designed to burn for only 2 minutes, boosting the rocket's speed to about 19,000 miles per hour.
"The second-stage engine was designed to burn for 2 minutes. ' boosting the rocket speed to 1 9,000 miles an hour, and would 1 sputter out at an altitude of about 130 miles."
Image 6 of Evening star (Washington, D.C.), March 17, 1958