What is the most aerodynamic Satellite?












6














From what I understand at least in the lower orbits you want the least amount of drag possible.



My brain is telling me that a long pole or submarine shape satellite orientated to the direction of travel or direction of solar wind would be best and not a ball at all?



Would adding a smooth skin to take out the contour between the parts on the ISS create less drag?



At what point does the extra weight and mass to make a satellite aerodynamic cost more fuel then saved?










share|improve this question


















  • 2




    Aerodynamics at a pressure of about 1 bar and subsonic speeds may be very different to drag in a nearly perfect vacuum and at hypersonic orbital speed.
    – Uwe
    17 hours ago






  • 1




    @Uwe If you released 2 rubber balloons with a .2psi from the bow of the ISS one shaped as a strait noodle balloon and the other round how much would "nearly" effect each balloon?
    – Muze
    17 hours ago










  • At theses speed and pressure cross section is all that matter.
    – Antzi
    4 hours ago
















6














From what I understand at least in the lower orbits you want the least amount of drag possible.



My brain is telling me that a long pole or submarine shape satellite orientated to the direction of travel or direction of solar wind would be best and not a ball at all?



Would adding a smooth skin to take out the contour between the parts on the ISS create less drag?



At what point does the extra weight and mass to make a satellite aerodynamic cost more fuel then saved?










share|improve this question


















  • 2




    Aerodynamics at a pressure of about 1 bar and subsonic speeds may be very different to drag in a nearly perfect vacuum and at hypersonic orbital speed.
    – Uwe
    17 hours ago






  • 1




    @Uwe If you released 2 rubber balloons with a .2psi from the bow of the ISS one shaped as a strait noodle balloon and the other round how much would "nearly" effect each balloon?
    – Muze
    17 hours ago










  • At theses speed and pressure cross section is all that matter.
    – Antzi
    4 hours ago














6












6








6


1





From what I understand at least in the lower orbits you want the least amount of drag possible.



My brain is telling me that a long pole or submarine shape satellite orientated to the direction of travel or direction of solar wind would be best and not a ball at all?



Would adding a smooth skin to take out the contour between the parts on the ISS create less drag?



At what point does the extra weight and mass to make a satellite aerodynamic cost more fuel then saved?










share|improve this question













From what I understand at least in the lower orbits you want the least amount of drag possible.



My brain is telling me that a long pole or submarine shape satellite orientated to the direction of travel or direction of solar wind would be best and not a ball at all?



Would adding a smooth skin to take out the contour between the parts on the ISS create less drag?



At what point does the extra weight and mass to make a satellite aerodynamic cost more fuel then saved?







artificial-satellite design aerodynamics drag






share|improve this question













share|improve this question











share|improve this question




share|improve this question










asked 17 hours ago









Muze

1,8911055




1,8911055








  • 2




    Aerodynamics at a pressure of about 1 bar and subsonic speeds may be very different to drag in a nearly perfect vacuum and at hypersonic orbital speed.
    – Uwe
    17 hours ago






  • 1




    @Uwe If you released 2 rubber balloons with a .2psi from the bow of the ISS one shaped as a strait noodle balloon and the other round how much would "nearly" effect each balloon?
    – Muze
    17 hours ago










  • At theses speed and pressure cross section is all that matter.
    – Antzi
    4 hours ago














  • 2




    Aerodynamics at a pressure of about 1 bar and subsonic speeds may be very different to drag in a nearly perfect vacuum and at hypersonic orbital speed.
    – Uwe
    17 hours ago






  • 1




    @Uwe If you released 2 rubber balloons with a .2psi from the bow of the ISS one shaped as a strait noodle balloon and the other round how much would "nearly" effect each balloon?
    – Muze
    17 hours ago










  • At theses speed and pressure cross section is all that matter.
    – Antzi
    4 hours ago








2




2




Aerodynamics at a pressure of about 1 bar and subsonic speeds may be very different to drag in a nearly perfect vacuum and at hypersonic orbital speed.
– Uwe
17 hours ago




Aerodynamics at a pressure of about 1 bar and subsonic speeds may be very different to drag in a nearly perfect vacuum and at hypersonic orbital speed.
– Uwe
17 hours ago




1




1




@Uwe If you released 2 rubber balloons with a .2psi from the bow of the ISS one shaped as a strait noodle balloon and the other round how much would "nearly" effect each balloon?
– Muze
17 hours ago




@Uwe If you released 2 rubber balloons with a .2psi from the bow of the ISS one shaped as a strait noodle balloon and the other round how much would "nearly" effect each balloon?
– Muze
17 hours ago












At theses speed and pressure cross section is all that matter.
– Antzi
4 hours ago




At theses speed and pressure cross section is all that matter.
– Antzi
4 hours ago










1 Answer
1






active

oldest

votes


















19














The only satellite I know of that was shaped to have low drag was GOCE, which orbited at 250 km.




Since it was vital to ensure that the measurements taken are of true gravity and not influenced by any movement of the satellite, this unique five-metre long arrow-shaped satellite had none of the moving parts often seen in other spacecraft. The satellite, together with its instrumentation, actually forms a single composite gravity-measuring device.



The satellite orbited Earth as low as possible to observe the strongest possible gravity-field signal – hence GOCE was designed to skim the edge of Earth's atmosphere at a height of about 250 km. Low fuel consumption meant that its altitude could be lowered to 235 km in 2012.



An electric ion thruster at the back of the satellite continuously generated tiny forces to compensate for any drag that GOCE experienced along its orbit.



The need to fly low and be ultra-stable led to a novel satellite design that minimised air drag and torque and excludes mechanical disturbances. The result was a slim 5 metre-long satellite with a cross sectional area of about 1m2, weighing in at about 1050 kg. The satellite was symmetrical about its horizontal plane and had two winglets that provided additional aerodynamic stability.




GOCE



You can see this places constraints on the satellite's shape: you can't have protruding solar panels, antennas etc. This means it's only done when really necessary; for most purposes it's much cheaper to go to a slightly higher orbit instead.






share|improve this answer





















  • That's very cool and new to me.
    – Organic Marble
    15 hours ago










  • The solar panels are built into it as shown and an antenna follows the wings. The space craft is on a lean performing a turn the belly facing towards the camera.
    – Muze
    14 hours ago













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1 Answer
1






active

oldest

votes








1 Answer
1






active

oldest

votes









active

oldest

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active

oldest

votes









19














The only satellite I know of that was shaped to have low drag was GOCE, which orbited at 250 km.




Since it was vital to ensure that the measurements taken are of true gravity and not influenced by any movement of the satellite, this unique five-metre long arrow-shaped satellite had none of the moving parts often seen in other spacecraft. The satellite, together with its instrumentation, actually forms a single composite gravity-measuring device.



The satellite orbited Earth as low as possible to observe the strongest possible gravity-field signal – hence GOCE was designed to skim the edge of Earth's atmosphere at a height of about 250 km. Low fuel consumption meant that its altitude could be lowered to 235 km in 2012.



An electric ion thruster at the back of the satellite continuously generated tiny forces to compensate for any drag that GOCE experienced along its orbit.



The need to fly low and be ultra-stable led to a novel satellite design that minimised air drag and torque and excludes mechanical disturbances. The result was a slim 5 metre-long satellite with a cross sectional area of about 1m2, weighing in at about 1050 kg. The satellite was symmetrical about its horizontal plane and had two winglets that provided additional aerodynamic stability.




GOCE



You can see this places constraints on the satellite's shape: you can't have protruding solar panels, antennas etc. This means it's only done when really necessary; for most purposes it's much cheaper to go to a slightly higher orbit instead.






share|improve this answer





















  • That's very cool and new to me.
    – Organic Marble
    15 hours ago










  • The solar panels are built into it as shown and an antenna follows the wings. The space craft is on a lean performing a turn the belly facing towards the camera.
    – Muze
    14 hours ago


















19














The only satellite I know of that was shaped to have low drag was GOCE, which orbited at 250 km.




Since it was vital to ensure that the measurements taken are of true gravity and not influenced by any movement of the satellite, this unique five-metre long arrow-shaped satellite had none of the moving parts often seen in other spacecraft. The satellite, together with its instrumentation, actually forms a single composite gravity-measuring device.



The satellite orbited Earth as low as possible to observe the strongest possible gravity-field signal – hence GOCE was designed to skim the edge of Earth's atmosphere at a height of about 250 km. Low fuel consumption meant that its altitude could be lowered to 235 km in 2012.



An electric ion thruster at the back of the satellite continuously generated tiny forces to compensate for any drag that GOCE experienced along its orbit.



The need to fly low and be ultra-stable led to a novel satellite design that minimised air drag and torque and excludes mechanical disturbances. The result was a slim 5 metre-long satellite with a cross sectional area of about 1m2, weighing in at about 1050 kg. The satellite was symmetrical about its horizontal plane and had two winglets that provided additional aerodynamic stability.




GOCE



You can see this places constraints on the satellite's shape: you can't have protruding solar panels, antennas etc. This means it's only done when really necessary; for most purposes it's much cheaper to go to a slightly higher orbit instead.






share|improve this answer





















  • That's very cool and new to me.
    – Organic Marble
    15 hours ago










  • The solar panels are built into it as shown and an antenna follows the wings. The space craft is on a lean performing a turn the belly facing towards the camera.
    – Muze
    14 hours ago
















19












19








19






The only satellite I know of that was shaped to have low drag was GOCE, which orbited at 250 km.




Since it was vital to ensure that the measurements taken are of true gravity and not influenced by any movement of the satellite, this unique five-metre long arrow-shaped satellite had none of the moving parts often seen in other spacecraft. The satellite, together with its instrumentation, actually forms a single composite gravity-measuring device.



The satellite orbited Earth as low as possible to observe the strongest possible gravity-field signal – hence GOCE was designed to skim the edge of Earth's atmosphere at a height of about 250 km. Low fuel consumption meant that its altitude could be lowered to 235 km in 2012.



An electric ion thruster at the back of the satellite continuously generated tiny forces to compensate for any drag that GOCE experienced along its orbit.



The need to fly low and be ultra-stable led to a novel satellite design that minimised air drag and torque and excludes mechanical disturbances. The result was a slim 5 metre-long satellite with a cross sectional area of about 1m2, weighing in at about 1050 kg. The satellite was symmetrical about its horizontal plane and had two winglets that provided additional aerodynamic stability.




GOCE



You can see this places constraints on the satellite's shape: you can't have protruding solar panels, antennas etc. This means it's only done when really necessary; for most purposes it's much cheaper to go to a slightly higher orbit instead.






share|improve this answer












The only satellite I know of that was shaped to have low drag was GOCE, which orbited at 250 km.




Since it was vital to ensure that the measurements taken are of true gravity and not influenced by any movement of the satellite, this unique five-metre long arrow-shaped satellite had none of the moving parts often seen in other spacecraft. The satellite, together with its instrumentation, actually forms a single composite gravity-measuring device.



The satellite orbited Earth as low as possible to observe the strongest possible gravity-field signal – hence GOCE was designed to skim the edge of Earth's atmosphere at a height of about 250 km. Low fuel consumption meant that its altitude could be lowered to 235 km in 2012.



An electric ion thruster at the back of the satellite continuously generated tiny forces to compensate for any drag that GOCE experienced along its orbit.



The need to fly low and be ultra-stable led to a novel satellite design that minimised air drag and torque and excludes mechanical disturbances. The result was a slim 5 metre-long satellite with a cross sectional area of about 1m2, weighing in at about 1050 kg. The satellite was symmetrical about its horizontal plane and had two winglets that provided additional aerodynamic stability.




GOCE



You can see this places constraints on the satellite's shape: you can't have protruding solar panels, antennas etc. This means it's only done when really necessary; for most purposes it's much cheaper to go to a slightly higher orbit instead.







share|improve this answer












share|improve this answer



share|improve this answer










answered 16 hours ago









Hobbes

86.1k2244390




86.1k2244390












  • That's very cool and new to me.
    – Organic Marble
    15 hours ago










  • The solar panels are built into it as shown and an antenna follows the wings. The space craft is on a lean performing a turn the belly facing towards the camera.
    – Muze
    14 hours ago




















  • That's very cool and new to me.
    – Organic Marble
    15 hours ago










  • The solar panels are built into it as shown and an antenna follows the wings. The space craft is on a lean performing a turn the belly facing towards the camera.
    – Muze
    14 hours ago


















That's very cool and new to me.
– Organic Marble
15 hours ago




That's very cool and new to me.
– Organic Marble
15 hours ago












The solar panels are built into it as shown and an antenna follows the wings. The space craft is on a lean performing a turn the belly facing towards the camera.
– Muze
14 hours ago






The solar panels are built into it as shown and an antenna follows the wings. The space craft is on a lean performing a turn the belly facing towards the camera.
– Muze
14 hours ago




















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