Aerodynamic stabilization of satellites

  • Thread starter Thread starter giber
  • Start date Start date
  • Tags Tags
    Satellites
AI Thread Summary
Aerodynamic stabilization of satellites is a complex topic, particularly because traditional aerodynamic control surfaces are ineffective in space due to the lack of air. The discussion highlights the importance of understanding specific forms of stability, such as spin or orbit stability, when researching this area. Participants mention that atmospheric drag still affects satellites in low Earth orbit, necessitating strategies like torque equilibrium attitude and minimum drag attitude to manage forces acting on the vehicle. Resources for further reading are suggested, including free academic papers that could provide more insights. Overall, the conversation emphasizes the nuanced relationship between atmospheric effects and satellite stability.
giber
Messages
15
Reaction score
0
i need to do a work about aerodynamic stabilization on satelites.. can anyone help

thanks
 
Engineering news on Phys.org
Try googling "torque equilibrium attitude".
 
i don´t find anything about it... all papers to pay, not even examples of satellites... the only information was that URSS send one (cosmos 149) with gravitational and aerodynamic control.. nothing much...
 
giber,
giber said:
i don´t find anything about it... all papers to pay, not even examples of satellites... the only information was that URSS send one (cosmos 149) with gravitational and aerodynamic control.. nothing much...

What, precisely, do you mean by aerodynamic stabilization of satellites? I would presume you know that there is no air in space, and as such any form of aerodynamic control surfaces (such as used on aircraft) are ineffective. And I think you should also define what specific form of stability you are researching: Spin stability or Orbit stability? Suffice it to say that use of the word "aerodynamic" whenever it comes to space (or anything above about 200,000 feet in altitude) is odd.

Rainman
 
giber said:
i don´t find anything about it... all papers to pay, not even examples of satellites... the only information was that URSS send one (cosmos 149) with gravitational and aerodynamic control.. nothing much...


So bypass the pay sites. This one, for example, is free.
http://www.lerc.nasa.gov/WWW/MMAP/PIMS/MEIT/MEIT_pdfs/meit2002/Section19.pdf"


RainmanAero said:
Suffice it to say that use of the word "aerodynamic" whenever it comes to space (or anything above about 200,000 feet in altitude) is odd.

It is not odd at all. The exoatmosphere extends well beyond low Earth orbit. The Space Station's orbit, for example, decays by a few hundred meters per day due to atmospheric drag.

Approaches used by vehicles in low Earth orbit to address atmospheric drag include
  • Torque equilibrium attitude. Atmospheric drag imparts force and torque on the vehicle. The torque depends on attitude. If the vehicle has a non-spherical mass distribution, the gradient in the gravitation field also exerts a torque on the vehicle. Torque equilibrium attitude is the attitude that results in the smallest net torque on the vehicle from the combined effects of atmospheric drag torque and gravity gradient torque.
  • Minimum drag attitude. This is the attitude that minimizes the drag force on the vehicle.
  • Ah f*** it attitude. The vehicle has some science to perform. It pays the penalty and expends fuel to maintain the altitude and attitude needed to carry out its primary mission.
 
Last edited by a moderator:
Posted June 2024 - 15 years after starting this class. I have learned a whole lot. To get to the short course on making your stock car, late model, hobby stock E-mod handle, look at the index below. Read all posts on Roll Center, Jacking effect and Why does car drive straight to the wall when I gas it? Also read You really have two race cars. This will cover 90% of problems you have. Simply put, the car pushes going in and is loose coming out. You do not have enuff downforce on the right...
I'm trying to decide what size and type of galvanized steel I need for 2 cantilever extensions. The cantilever is 5 ft. The space between the two cantilever arms is a 17 ft Gap the center 7 ft of the 17 ft Gap we'll need to Bear approximately 17,000 lb spread evenly from the front of the cantilever to the back of the cantilever over 5 ft. I will put support beams across these cantilever arms to support the load evenly
Thread 'What's the most likely cause for this carbon seal crack?'
We have a molded carbon graphite seal that is used in an inline axial piston, variable displacement hydraulic pump. One of our customers reported that, when using the “A” parts in the past, they only needed to replace them due to normal wear. However, after switching to our parts, the replacement cycle seems to be much shorter due to “broken” or “cracked” failures. This issue was identified after hydraulic fluid leakage was observed. According to their records, the same problem has occurred...
Back
Top