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9:48 pm December 30, 2009
| Luke M
| | Adelaide, Australia | |
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I have been thinking lately about how to extend our current plans for the lander frame to the complete vehicle. This involves finding somewhere to put avionics etc., an RCS solution and some means of docking the lander with the fuel module. Below is a concept diagram of one way we could perhaps put all this together – but I'm not that fond of it and I suspect somebody could come up with something better.
 So, let's see what we have:
- Instead of the lander legs meeting at pointed apex as per current renderings, they terminate a bit earlier in a square shape, which is easier to attach stuff to.
- Electronics etc. are arranged around the chair in a horseshoe shape.
- There is a cross-shaped structure underneath the chair/electronics which holds RCS units away from the seat. The RCS units in this diagram are scaled down versions of the CM's RCS, which is probably suboptimal – originally I envisioned them as being exact copies of the CM RCS but then I realised they were probably far too big. Rather than change the diagram I "scaled down", we should probably consider alternatives.
- Also at the ends of the cross-shaped structure are very strong (titanium?) vertical poles with some sort of attachment mechanism on the ends (perhaps combining magnets and some kind of simple locking structure) which allow the whole thing to attach to the end of the mission stack without blocking access to the chair.
- Two of these vertical poles have fuel lines integrated with them somehow (one for fuel, one for oxidiser). The others may have anteannas in/on them.
Note that this diagram is quite poor in a few ways: the chair is shown point 45 degrees away from the nearest legs, but of course the steps are built onto one of the legs so the chair (and the horseshoe electronics structure around it) should be rotated 45 degrees from how they are shown in this diagram. Note that the cross structure with the RCS should not be rotated as this would have the RCS units directly over the legs, and we don't want to melt our legs off during descent. This diagram, at least in the top view, shows the RCS units directly over the tanks – obviously the arms they are on should be long enough that they are a safe distance away. The problem with this is that the docking pylons may be too far apart to attach to the back of the stack without some kind of expanding adaptor – although that isn't a huge problem.
As I've said, I'm not too fond of this diagram, but it's the only thing that has been proposed so far. Feel free to tear it to shreds or offer suggestions for improvement.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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11:06 pm December 30, 2009
| Luke M
| | Adelaide, Australia | |
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| posts 1484 | |
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An obvious improvement might be to have three equally spaced circular bands encompassing and welded to the support pylons, at the top, bottom and middle. This would make the whole thing a little more structurally sound, might make docking easier (the top band could support all sorts of attachment mechanisms) and would still leave the seat fairly accessible.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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5:54 am December 31, 2009
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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This looks like a nice evolution of the current renders. I'm not sure if I will be able to change the current model to this flat topped design since all of the geometry is thoroughly entangled (i.e. one component).
As you said, one of the problems (from a general layout standpoint) is the placement of the RCS thrusters. The need to be positioned so that they don't increase the outside dimensions of the lander so that it can fit inside the launch vehicle. One option would be to place them on spring loaded poles that can telescope out (by means of small explosive bolts) once in orbit. This is likely a viable option, but I'd rather not have any more moving parts than we need (design philosophy). Mounting them on the legs is probably going to be an option but I think that may move them substantially away from the center of gravity.
I assume that we want an "RCS quadrant", that is, a cluster of four thrusters that is a modular unit. If we don't necessarily want to go with this simple design then we will give ourselves the option of symmetrically mounting individual thrusters all around the lander in places where they can be fired perpendicular to any structural members. This approach obviously complicates a lot of things from a control software standpoint, but then again software is likely to be one of our strong points.
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Main Workgroups: Propulsion & Spacecraft Engineering
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6:48 am December 31, 2009
| Luke M
| | Adelaide, Australia | |
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| posts 1484 | |
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Rocket-To-The-Moon said:
Mounting them on the legs is probably going to be an option but I think that may move them substantially away from the center of gravity.
Isn't that a good thing, from the point of view of minimising thrust needed to achieve a given rate of rotation? Torque is force multiplied by distance from centre of mass?
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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7:09 am December 31, 2009
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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Post edited 2:21 pm – December 31, 2009 by Rocket-To-The-Moon
I guess what I meant is that it will move the (thrust) line of symmetry (with respect to the diametrically opposed thruster quadrants) below the center of mass of the vehicle. To use an exaggerated example, imagine the RCS thrusters on the tips of the docking pylons.
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Main Workgroups: Propulsion & Spacecraft Engineering
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10:55 am December 31, 2009
| Luke M
| | Adelaide, Australia | |
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| posts 1484 | |
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Rocket-To-The-Moon said:
I assume that we want an "RCS quadrant", that is, a cluster of four thrusters that is a modular unit.
This seems like by far the most sensible thing to do to me.
I wonder if we would be able to get away with cold gas RCS on the lander due to its relatively low mass? If we did then building a proof-of-concept quadrant would be pretty straightforward – there's a diagram on the Copenhagen Suborbitals site for the Tycho Brahae RCS system which is cold gas, and Gary Schneider for OLF suggested to me in an email that building a simple cold gas thruster might be a good beginning project.
If we did build a few of these thrusters, and just a basic frame for the lander (not worry about pylons etc) we could suspend the frame from a low crane and spin/tilt it using the thrusters, which would be pretty awesome and let us do some software work, too.
If we built the test frame out of steel instead of aluminium (I'm assuming steel is considerably cheaper) then building one would probably be pretty cheap and could be easily done in a weekend in a backyard workshop – all it would take would be a welder and some basic powertools. The more I think about it, the more it feels like this (rough lander frame with cold gas RCS) could be an exellent way to get some physical hardware in existence to show off on the website that would be quick, cheap and actually somewhat useful.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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5:39 pm December 31, 2009
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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Building the frame would be a relatively simple construction project for a small team to tackle. I think that I am in favor of using the actual material that we plan on flying so that we can gain more experience with the stresses that it will experience along with refining construction methods. Having a computer controlled RCS demonstrator would really be an awesome step in the right direction.
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Main Workgroups: Propulsion & Spacecraft Engineering
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11:48 pm December 31, 2009
| Luke M
| | Adelaide, Australia | |
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| posts 1484 | |
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Okay, I'm fairly excited about this idea. What do we need to make it work? A few people in the one place who have:
- The facilities to cut and weld aluminium, to build the frame.
- The facilities to machine nozzles for the RCS out of…steel? If we're using cold gas there's no temperature problem, the nozzles will not be subject to any real stress, might as well use the cheapest, most readily available material out there?
- Anything else?
How should we go about finding such a group?
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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7:15 am January 1, 2010
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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Luke Maurits said:
How should we go about finding such a group?
A professional machinist group is probably a good place to start looking. I guess the idea is to hand them our drawings and SketchUp renders so they have the basic idea and then let them do the engineering to make it work in real life. I will try to find a metal workers' forum this afternoon and see if we can stir up any interest. Maybe we can set up a second PayPal fund to collect money for materials; or should we let the group building it find the funds (distributed fundraising)?
I don't have the time now, but I am thinking about beginning welding/fabrication night classes. My Dad is a skilled welder/fabricator so I have a pretty strong background but not too much hands on experience.
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Main Workgroups: Propulsion & Spacecraft Engineering
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3:14 pm January 1, 2010
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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Main Workgroups: Propulsion & Spacecraft Engineering
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5:39 pm January 1, 2010
| Luke M
| | Adelaide, Australia | |
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Good work in seeking out an appropriate forum and making a request – unfortunately it looks like we've received a disappointing response from a group of fairly dim individuals who obviously made no effort to read any of the material you linked them to. There seems to be an idea on there that the fuel tanks are actually balloons, which means either that poster has no idea how balloons float (and hence doesn't realise that this won't work in space) or that they think we have no idea how balloons float.
I suppose this is raises an important issue, though, which is that we are going to have to learn how to manage the all important concept of take-serious-ability for our first introductions to people/groups. I think there are two facets to this: making ourselves look serious and respectable, and also combatting the public perception that our sorts of endeavours are impossible. I have read John Carmack quoted somewhere as saying "Rocket science has been mythologised out of all proportion to its actual difficulty", and I think this is true of space travel in general. There is a public perception that things need to be almost magical to work in space – you can't just take mundane metals and weld them together, you need secret NASA pixie dust! I've suffered a little from this issue myself, not in thinking that our task was impossible but in being constantly surprised while working on it at how not-impossible it is. To be sure, space travel is hard, but it's not magic. We need to think of a way to break through the misconception that this can't possibly work and make people realise that building a simple spaceship in a home workshop is only a medium step further than building a simple airplane or a simple submarine in a home workshop – and people do those all the time.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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5:52 pm January 1, 2010
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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I think that the major roadblock with just openly soliciting to a group like this is that only one in a hundred might be truly interested.
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Main Workgroups: Propulsion & Spacecraft Engineering
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6:18 pm January 1, 2010
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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This is an encouraging quote from one of the guys:
And it looks like home garage, one week, after hours job…
An off the cuff estimation, but at least they don't think we are over ambitious in that respect.
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Main Workgroups: Propulsion & Spacecraft Engineering
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7:26 pm January 1, 2010
| Luke M
| | Adelaide, Australia | |
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| posts 1484 | |
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Actually, when I said that the response was disappointing, it was fairly early on in the discussion and I didn't realise that it was continuing at that time. Some of the group seem to be warming to us, or at least listening to ideas. This might not turn out too badly.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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9:50 pm January 1, 2010
| Luke M
| | Adelaide, Australia | |
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| posts 1484 | |
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I wonder if we should give the effort to build a lander frame and put a simple cold gas RCS on it should be given some sort of official "subproject" status, with its own Wiki page, to assist in soliciting interest? There we could explain exactly what we are trying to do and why we are trying to do it. We could have a separate ChipIn (or similar) campaign running to raise money purely for this subproject.
The goals of the subproject would be:
- To get better estimates of lander frame mass and cost.
- To test strength/stability of the lander frame by loading it with something of roughly the same size and mass of our intended use and dropping it onto a roughly lunar surface from various heights and at various angles.
- To see what sort of rotational / stabilisation performance we can achieve with nitrogen or CO2 cold gas thrusters by actually putting some on a lander that is approximately the correct size/shape/mass. I would really love to use this sort of system instead of actual chemical rockets for our RCS (aside: RCS stands for reaction control system, not rocket control system) if it is feasible, and this seems like the easiest way to test.
- To generate awesome propaganda photos/videos by putting the lander somewhere remote and roughly lunar-looking.
Can anybody think of any other potential goals?
The subproject description page should emphasise that this is not the lander that will go to the moon – nor is it even a test model of the exact design of lander that will go to the moon. It is something cheap and simple that is roughly what will go to the moon – our actual design will probably be refined considerably based on the 100 little things we will learn from building this mockup, trying to spin it around with cold gas RCS and getting someone in a mock moonsuit to climb up and down it a few times in the desert. When it comes to things like designing seat suspension later on, this frame will provide a decent test bed to bolt prototypes onto for testing.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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10:49 pm January 1, 2010
| Rocket-To-The-Moon
| | Altus, Oklahoma, USA | |
| Member | posts 686 | |
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Luke Maurits said:RCS stands for reaction control system, not rocket control system
Woah there; crazy talk on my part.
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Main Workgroups: Propulsion & Spacecraft Engineering
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