Questions tagged [orbital-maneuver]
In spaceflight, an orbital maneuver is the use of propulsion systems to change the orbit of a spacecraft.
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How would I or who/what could help me find the trajectory of an "Extended Grand Tour" spacecraft, without having to take a long course on the subject?
(As forewarning, the most integral details of this question are bolded.)
For context, I have been writing an alternate history involving the accelerated development of spaceflight technology for over ...
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Commencing atmospheric re-entry
Once a decision is taken to get back home (earth), a spacecraft, I think has two options: 1 - To reduce its speed (by firing the thrusters located in the forward or something similar), so that it is ...
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Is there any orbital launcher capable of removing the second stage from orbit after inserting the payload satellite into LEO?
The Space Shuttle was able to place a satellite into orbit and to return to Earth.
Is there any second stage that may deliver the payload satellite into LEO and do a deorbit burn after that using its ...
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How would I calculate the extra change in velocity due to residual thrust?
I'm trying to script a hover slam in a simulated environment using generic kinematic equations to calculate the correct throttle values I should be matching. I cut the throttle of my engine when my ...
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How much delta v did the space shuttle use for orbital insertion? [duplicate]
The space shuttle's OMS was used to insert the space shuttle into orbit since the external H2/LOX tank separated on a sub orbital trajectory. How much delta v did the insertion maneuver use?
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Can JWST come in for a pit stop? Is the fuel supply on JWST adequate for a transfer to an Earth Moon libration point to allow repairs?
The James Webb Space Telescope is generally considered to be in an unserviceable location at SEL2.
If servicing becomes necessary, is it possible for the JWST to use a low energy heteroclinic transfer ...
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Why did Curiosity perform TCMs?
Why did Curiosity perform TCM (Trajectory Correction Maneuver)s 1 through 5? 6 makes sense since it needed to adjust course to actually once in the SOI, but the others don't. I understand that this ...
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What maneuvers could be useful to move between two sun synchronous orbits with different times?
Consider two sun-synchronous orbits with similar orbital elements, except for their times. For example 8h and 9h orbits. Their semi-major axes (a), inclinations (i), and eccentricities (e) are the ...
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Targeted Sub-Orbital Optimization Problem
I was messing around with some orbital dynamics for a simulator I am working on, and I came across a snag that I have not been able to figure out. Specifically, I am trying to minimize the required ...
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How do satellites ensure they are orientated towards the Earth to allow of clear connections? [duplicate]
As the title says,
How do satellites ensure they are orientated towards the Earth to allow of clear connections, whilst having their solar panels face the sun?
I understand reaction wheels are ...
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Given an initial orbit calculate the necessary maneuver impulse to obtain a required final eccentricity and semi-major axis
The question is simple. Starting from an eccentric orbit I want to obtain a final orbit of which the final semi-major axis and the final eccentricity are known. You would have to determine the boost ...
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Parameters of the L2 insertion burn to be done tomorrow
What parameters control the impulse to be applied in the L2 insertion burn? What parameters control when/where it is to be performed? What velocity is the impulse applied to achieve? Is the vehicle ...
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What was the first spacecraft intentionally moved from GEO to the graveyard orbit to die? (just a bit above geosynchronous)
Why “super” for supersynchronous orbits? Why not “trans”? and discussions and answers there got me wondering:
Question: What was the first spacecraft intentionally moved from GEO or geosynchronous to ...
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James Webb orbit insertion
Webb will issue a final course correction burn to insert it into the orbit around L2. It arrives from earth so the approach velocity should be higher than the desired orbit velocity and the vector ...
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What are the benefits of supersynchronous transfer orbits?
Some satellites are injected into higher apogee than standard GTO apogee of 35 786 km. Next the satellite then has to increase its perigee ( usually 250 km ) to GEO altitude. Then the apogee has to be ...
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Are VASIMR + Arcjet engines feasible for orbital transfers on Mars?
The VASIMR engine is an electric propulsion system that has been lauded for its ability to cut down on interplanetary transfers. While it requires a high power source (in the range of 200kW), it is a ...
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What is the delta v required for insertion to sun-earth L2?
What is the delta v required to place a satellite in L2 from earth transfer orbit ( Like the James Webb Telescope )?
Does orbits closer to L2 different delta v from orbits far from L2?
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What is the largest single burn plane change maneuver executed in LEO?
Below 2000 km in low Earth orbit (or close to it), what is the largest propulsive plane change from a single burn?
Expecting an answer in degrees, a named mission and vehicle executing the burn itself....
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What is the equation that relates delta v of a rocket to time taken to complete an orbit?
I wanted to see how the delta-v produced by a rocket affects the time it takes to complete a certain orbit. So what is the equation that relates these two quantities?
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How much delta-v could be saved with a Hohmann-like transfer orbit to the aphelion of Mercury 's orbit instead of its perihelion?
I wrote "Hohmann-like" of course because Mercury's orbit is rather eccentric and has an inclination of 7 ⁰.
From this factsheet I've learned that perihelion is at 46 million km and aphelion ...
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How to calculate an initial impulse for escape from planet's sphere of influence and lay on a specific orbit around the Sun?
I have a spacecraft parked on orbit around the planet. I want to make interplanetary transfer to another planet. I can find the orbit around the Sun that I can use to move from the end of departure ...
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Do operational Starlink satellites run their ion engines at night on batteries? And if so, do they have hi/low settings?
Discussion below What is the maximum thrust of the Starlink satellites? raise the question of the Starlink communications satellites' power budget and use of their ion thruster in daylight when the ...
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What types of propulsion are used to adjust an orbit?
What types of propulsion are used to adjust the orbit of an object such as a satellite, space station, supply vehicle?
I'm curious if they all use the same method to adjust their trajectory, or if ...
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During orbital rendezvous, at what distance and approach velocity does the transition from orbital mechanics to “boating around” occur?
During the intercept (terminal) phase of orbital rendezvous, the intercepting spacecraft must use Proportional Navigation or Orbital Mechanics to develop an intercept course: all that counterintuative ...
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Pure orbit inclination changing, why delta v differs between vector and numerical approach?
as said in the title I have different results between numerical en vector approach during inclination changing maneuver.
The initial orbit :
Perigee radius : 6700 km
Eccentricity : 0.7
Inclination : ...
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Does other orbital parameters change on plane alignment impulsive maneuver?
I work on small application to apply impulsive maneuver on an orbit.
I want to align two orbits in the same plane.
After the execution of the function, original orbit has the same inclination and ...
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Is an orbital insertion burn part of any launch from earth
As I understand it once a spacecraft reaches low earth orbit it may have to do another burn to reach a different orbit. Would that change in orbit be considered an orbital insertion burn? Do any ...
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How to correct my real orbit and turn it into predicted ideal orbit?
I want to launch my ship to the purple ellipse orbit. But because of non-ideal world I have non-ideal ship orientation and non-ideal thrust impulse. So, my initial speed is a bit bigger and it's ...
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How to keep the phase angle with an Hohmann transfer?
I am studying the drag make up maneuver. In this maneuver, I need to go from point A to point B keeping the same phase angle as shown schematically in this picture
When I've approached this problem, ...
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Can ISS trash be used as reaction mass for orbital maintenance
There have been a number of videos posted about trash being hand-pitched out the back of the ISS. This seems like a waste of potential reaction mass, especially since it cost $20,000/kg to get it up ...
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How to correct orbit in case of perturbations? [duplicate]
I predicted the future position of orbital body and sent my spacecraft to that position. But the trajectory of body and spacecraft are changing because of perturbations. So, I need to correct this ...
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How to correctly change velocity in space?
The solver of the Lambert's problem gives me a hyperbolic velocity to move to some position on orbit. But the spacecraft is moving on orbit and changing the velocity takes some time. So, when I ...
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Calculating the projectile of rocket using RCS to tilt the flight path
If I have main solid rocket with 800 N Thrust, 9 kg in total and has RCS thrusters 0.5 m from the center mass. Mid flight the RCS with 1 N force is activated for 2 sec. How does it affect the flight ...
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How do RAAN steering increase the launch window?
In the recent ULA video by Tory Bruno Tory Talk // Atlas V Lucy: RAAN Steering (linked below) he gave some short hints about RAAN steering.
What is RAAN (Right Ascension of Ascending Node) steering?
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What's wrong with my bielliptic transfer calculation?
I'm trying to calculate the delta-v needed to get from a 200 km circular orbit to a geostationary orbit. GSO is at an altitude of 42164140.1029448 m and at a speed of 3074.6611762 m/s. Because $\frac{...
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Is there a known solution for optimal impulsive transfer between two arbitrary elliptical orbits?
If not, what optimization methods or tools do people use? (Code libraries?)
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How to find eccentric anomaly by mean anomaly?
Wikipedia gives me the equation
M = E - e*sinE
I have M and need to find E.
How to do it?
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How can we avoid collisions when moving from one orbit to another?
Imagine that my ship is parked in LEO and needs to transfer to a higher orbit. It makes a Hohmann transfer and flies to the needed orbit by an elliptical trajectory. But this trajectory is crossing a ...
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How to fly from Earth to Mars if the differences between phase angles is too big for Hohmann transfer but we have fuel for other transfers?
Hohmann transfer is possible when Earth and Mars positions are appropriate for this https://ai-solutions.com/_freeflyeruniversityguide/interplanetary_hohmann_transfe.htm
This happens one time in two ...
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Find the Orbital Inclination given all other Elements and a Position on the Ellipse
I'm in a situation where I need to determine an orbit's inclination. At my disposal I have all of the orbit's other Keplerian elements, and I have the vector of a single point on the ellipse. Is ...
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When burns are made during inefficient parts of the orbit, where does the lost energy go?
Any Kerbal Space Program player will know that burns prograde and retrograde to the velocity vector are most efficient closest to the body being orbited, while burns normal and anti-normal are most ...
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Right Ascension of the Ascending Node (RAAN) Drift and Correction
This one can be a very short and easy question, but I wanna know the proper answer of them..
Few days ago I got a questions like:
"What kind of perturbation(s) can cause drift on RAAN value of a ...
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Does going to Mars take the same energy as making a rendezvous with something going to Mars?
I think I found a mathematical error in the 2015 movie The Martian1. Warning, there will be spoilers.
The final plan they settle on to rescue Mark Watney is to have the Tiayang Shen rendezvous with ...
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Did the ISS just turn upside-down? Nauka docking attitude maneuvers; did the cupola near pointing zenith and therefore show only black sky w/ stars?
This answer to Is the ISS going to yaw and assume the XPOP attitude for Nauka docking? contains lots of information on the attitude trajectory in yaw-pitch-roll space, but from those I can't envision ...
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References for constant low-thrust spiral up-coast-spiral down phasing maneuvers for circular and non-circular orbits?
I am trying to find papers that describe constant low-thrust spiral up-coast-spiral down phasing maneuvers for circular and non-circular orbits. The thrust is assumed to be fixed at $T_{const}$ when ...
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Using GMAT to simulate phasing orbits with finite burns
I'm working on a project which requires me to use GMAT but I'm new to the program (and to asking questions on this website).
I'm supposed to send a spacecraft from a known GTO to the Moon.
A direct ...
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Rotation matrix / coordinate transformation of maneuver parameters from Prograde, Normal, Radial to Cartesian XYZ?
Say I have a state vector and Keplerian elements of an orbiting spacecraft:
Position = [x, y, z]
Velocity = [vx, vy, vz]
Elements = [a, e, i, $\omega$, $\Omega$, $\nu$]
And I have the maneuver I ...
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Is it possible for the exhaust plume of a rocket engine burning retrograde to accelerate an object into an even higher orbit?
A couple weeks back, a debris object was catalogued in a 210x540km orbit following the deorbit burn of the Falcon 9 second stage that launched CRS-22:
Hmm... possible that CRS-22's stage 2 made ...
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How many existing satellites have a continuously varying orbit because of human design decisions?
In the space community, there is an assumption that changes to an Earth satellite's orbit are infrequent (other than those due to atmospheric drag). Are there any known satellites designed to ...
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Could this three-thruster spherical spacecraft de-tumble itself with zero final velocity?
@Joshua's answer to What is the minimum number of RCS thrusters capable of stabilizing a satellite against an arbitrary rotation? begins:
I know this question is old, but I randomly discovered a ...
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