5
$\begingroup$

In Musk is testing x-wing style fins, spaceport drone ship there is mention of two Musk tweets:

Testing operation of hypersonic grid fins (x-wing config) going on next flight.

and

Grid fins are stowed on ascent and then deploy on reentry for 'x-wing' style control. Each fin moves independently for pitch/yaw/roll.

What is the function of these fins?

Improve this question
$\endgroup$
5
$\begingroup$

Actually, they are deliberately draggy.
During descent, they would produce significant drag given the waffle pattern producing vortices in the air around them (the hairs on a bee's wings have the same effect). In addition to attitude control, they could serve to reduce retrorocket burn and save a bit of fuel. They would definitely serve to keep the top of the rocket from heeling over when the thrusters ignite, acting like small drogue chutes.

Improve this answer
$\endgroup$
  • 3
    $\begingroup$ Do you have a citation for the dragginess? $\endgroup$ – Nathan Tuggy Jan 14 '15 at 4:36
8
$\begingroup$

Grid fins can be lighter, lower drag, and improve maneuverability at supersonic speeds relative to conventional planar fins. Russian designers seem to like them.

Improve this answer
$\endgroup$
  • $\begingroup$ In this video, are they being used for landing? I can't imagine how they should prove to be useful at that low speed. $\endgroup$ – Daniel F Dec 9 '14 at 21:25
  • $\begingroup$ In that video, they don't need to impart a lot of control authority because the maneuvering is very gentle. The main thing they're doing in that scenario is adding drag, moving the center of pressure/center of drag toward the top of the rocket, helping keep the rocket stable. $\endgroup$ – Russell Borogove Dec 9 '14 at 23:17
  • $\begingroup$ Didn't you mean to write that they increase drag (as they can have bigger surface area and remain stable compared to planar fins at supersonic speeds)? $\endgroup$ – TildalWave Dec 19 '14 at 20:13
  • 1
    $\begingroup$ According to the wikipedia article, they have less drag in the supersonic regime, but F9 is using them at lower speeds for drag as well as control. $\endgroup$ – Russell Borogove Dec 19 '14 at 21:58
3
$\begingroup$

They are aerodynamic control surfaces.

Improve this answer
$\endgroup$
1
$\begingroup$

Also since the rocket is only using one engine it has no control over rotation about the long axis of the rocket the fins provide that.

Improve this answer
$\endgroup$
  • $\begingroup$ During powered descent, when the grid fins are used, only one of the Merlins is running - the stage is very light on fuel at that point, and they want it to come down rather than to keep going up. :) $\endgroup$ – Russell Borogove Dec 19 '14 at 21:59
0
$\begingroup$

I am not an aerospace engineer, but it seems to me that because each grid fin can be independently controlled, then each can be rotated at extremely high speeds to create small vortexes which would allow discrete control of aerodynamic forces on the overall moment of the inherently unstable vertical proportion of the Falcon booster. A really eureka solution to creating means to achieve a soft landing in atmosphere...gyroscopically controlled rockets might require more fuel and weight than these fins. Very very impressed with what SpaceX and Musk are accomplishing...just hope that they partner up with Sierra Nevada and Dream Chaser to provide a more complete U.S. space capacity...after reading another article it seems the grid fins do not rotate at high speeds...rather they operate to assist in stabilizing and steering the booster as it descends at hypersonic then transonic velocities...sorry for the confusion but am not a rocket scientist...

Improve this answer
$\endgroup$
  • 3
    $\begingroup$ Welcome to Space Exploration SE! Please note that good answers are characterized by references to primary sources. Would be nice if you could substantiate your claim to "rotation at extremely high speeds" as the mode of operation of the fins. $\endgroup$ – Deer Hunter Jan 13 '15 at 15:03
  • 1
    $\begingroup$ Possibilus, with your last edit you're kinda disqualifying your own answer. Could you please edit it again to include a link to the article that you mentioned, and perhaps extract from it some useful information that's relevant to the questions and hasn't yet been discussed? Assuming its a credible source, of course. Thanks! $\endgroup$ – TildalWave Jan 14 '15 at 3:33

Your Answer

By clicking “Post Your Answer”, you agree to our terms of service, privacy policy and cookie policy

Not the answer you're looking for? Browse other questions tagged or ask your own question.