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Thinking big picture / long term again

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5:45 am
February 7, 2010


Luke Maurits

Adelaide, Australia

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In some ways, this post is a result of continuing the line of thinking in this one I made earlier today.

Basically, I have been thinking about our current list of projects and also our long term goal of being a proper open sourece space agency, not just one particular space project (c.f. Copenhagen Suborbitals, Open Luna, etc).

The fact is that we in fact started as one particular space project (put a Redditor on the moon) and then kind of evolved into an agency, tacking on projects as they seemed like an appropriate idea.

I've come to think that this has taken us somewhere quite different to where we would be if we'd initially began thinking of planning a space agency from scratch.

As mentioned in my other post, I think our situation with regards to launch vehicles is a bit incoherrent.  We have one project, OHKLA, which is about building a one-stage sounding rocket which, while a huge achievement and motivator for us, is of itself not particularly useful.  Our other project, CLLARE, has as a part of it, the construction of a hybrid booster cluster.  I think one project, a launch vehicle project, with the goal of building a modular hybrid system capable of scaling from minimal sounding rockets like OHKLA up to CLLARE-status LVs, and also things inbetween, such as for launching minimalist satellites, makes a lot, lot more sense than either of these.  This doesn't make the current OHKLA work useless or leave CLLARE without a non-commercial LV, so it's no kind of step backward, just a more coherrent, general approach.  Supposing we kept the name "Selene" for our booster system (although bear in mind (1) that the name Selene has previously been used by a JAXA project and (2) that a general purpose modular LV would have no inherrent link to the moon, we may want to reconsider), basically the current OHKLA plans would become Selene-1, and a full CLLARE stack launch would be left up to Selene-9, or whatever.  A critical factor of this project would be the requirement that it involved as few separate rockets as possible while covering as wide a range of payload types as possible.  This could help us put some much tighter restrictions on the requirements for OHKLA, which are currently quite open ended.

Also, I am wondering if it would be better to represent CLLARE not so much as a lunar landing project as "our first manned spaceflight project", a project whose requirements included scalability from suborbital through LEO to lunar landing.  This better explains the highly modular nature of the hardware stack and also slightly insulates us from the "crazy factor" associated with going to the moon.  It also opens us up to some other possibilities (e.g. we could have a module which attaches to the back of the OSM which had a rearward-facing ISS-compatible docking port on it.  Obviously, due to the CM's heat shield you couldn't actually enter through the docking port, but entry to the ISS or a Soyuz via EVA would be possible.  Whether or not the ISS is still up by the time we have a CM-OSM stack flying is debatable, but I am willing to bet that the ISS common berthing mechanism remains an international standard on future vehicles/stations.  This proposal is more about a change in how we present/market CLLARE than an actual change in any of our current plans.  CLLARE would become a "simple as possible, cheap as possible manned spaceflight project which is scalable from suborbital flight to lunar landing".  This just gives us a little bit more flexibility in direction.  Who knows, it might be that by the time we have CLLARE up to the stage that we have done circumlunar flights, CSTART may be in a position to do something a little less minimalist.

Finally, as a general purpose space agency, having an LV project and a manned spacecraft project, but not an unmanned project seems a little bit silly.  I know we are, as a group, highly averse to project bloat, but given that (1) CLLARE has now evolved to the point where there's not much for us 5 to do until some experts show up and (2) we can expect a large influx of interest after SpaceUp, I don't think it is too dangerous to consider a third project, especially since it fills a very natural gap in the line up of starter projects for a space agency.  My idea for this would be to design a sort of satellite "frame".  Basically it would be a satellite that consists of the basics – a propulsion system adequate for orientation control and station keeping, a basic navigation system (just GPS and horizon sensors could be adequate), a communications system adequate for telemetry and telecommand, and a power system for the above plus some spare – and then a physical frame of some kind with room for attaching a number of standardised independent modules (about the size of cube sats, maybe larger), which communicate data to the comms system via a standardised interface.  Basically there would be a standardised shape and size for these modules, with a standard power input and a standard data channel (maybe an ethernet port, or maybe a 9/25 pin serial/parallel cable, whatever), and the module itself could then contain whatever we wanted that could work within that system – cameras, sensors, absolutely whatever.  The frame could fit say 10 or so of these modules on it at once, we could sell slots on frames individually, or sell entire frames.  The idea is that we design one, standard system and that would be good enough to do all the basic stuff one might want to do with a satellite, so that this standardised frame is the backbone of our unmanned space operations for the next 5 or 10 years.

This resturcturing of CSTART would leave us with 3 projects, which I don't feel is too much, and it would leave us with all the obvious bases covered – an expandable launch vehicle family, a basic, extendable unmanned craft, and a basic, extendable manned craft.  This gives us a complete framework for an basic, flexible space agency.  We could probably do good, exciting science and exploration using the hardware from these 3 projects for a decade before we had to think about completely new hardware to go further.  Unlike most other space agencies, all three projects are designed so as to be highly modular, flexible and extendable.  This is different and cheap and exciting and gives the entire agency a uniform "flavour".

As a final small note, most of these proposals involve renaming projects.  If we do do this, I'd like to voice the opinion that maybe we should try to steer away from acronyms as names (you'll notice no other manned spaceflight project has ever done this) and go with something a little catchier/more exciting.  We could even have competitions.

As always, these are just thoughts, put up for discussion by the group.  I'm not married to any of them, I've just been thinking about how we could perhaps optimally reinvent ourselves for SpaceUp to look more coherrent, organised and well-planned for the long term.

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

8:15 am
February 7, 2010


Luke Maurits

Adelaide, Australia

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If we do go with this approach, it may be worth while defining very early on a list of "milestones" for each project.  Ensuring the LV project has a "single stage suborbital flight" milestone will ensure that OHKLA fully survives the reorg in spirit.

The manned spaceflight project milestones would be obvious: suborbital / orbital / circumlunar / lunar landing.

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

8:50 am
February 7, 2010


Rocket-To-The-Moon

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To be completely honest, I think that if anything we should be trimming down our scope prior to SpaceUp. The organization can grow in time as we gain members, but to bite off more than we can chew will do nothing but slow our progress on the projects that we can tackle at this time.

My opinion is that SpaceUp should mention CLLARE (and emphasize that this is where the organization is headed), but focus on OHKLA since it is a 100% attainable goal.

With the new NASA budget (which allocates money for commercial space flight) we may be able to secure some funding for these large projects though.

Completely offline from 8-14 March. Main Workgroups: Propulsion & Spacecraft Engineering

9:22 am
February 7, 2010


Luke Maurits

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As always, I understand the concern about biting off more than we can chew.  I am just worried about first impressions and I feel like right now CSTART looks a little like it doesn't have a sensible "big picture" organisation, it's just two projects, with some degree of overlap (hybrid rocketry in both).  The proposal above was intended as a trade off between not adding too much work (really all it adds is the unmanned satellite frame system, and arguably there's not a lot of new work in that – we could make an explicit effort to make as much hardware reusable between the satellite frame and CLLARE as possible, in terms of comms etc.) and presenting a coherent big picture.

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

3:04 pm
February 7, 2010


brmj

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I'm a bit conflicted about this idea, but I think I am slightly in favor of it over all.

I agree that having a larger strategy and all that would be nice. As for the exact details of the unmanned project, my thoughts are that it ought to essentially be the guts of a CLLARE CM, plus some solar panels and batteries. It doesn't sound so very horrible in terms of new work, but it would hardly be trivial. If we designed the manned stuff first, it wouldn't be too bad to design an unmanned satellite frame derivative, or even an unmanned probe derivative that keeps the PM. If we designed it correctly, a derivative of our lander could be added to put cargo, a rover or a static instrument platform on the moon.

If, on the other hand, we designed the unmanned stuff first, it might be a little more difficult to add some of that flexibility, though there is no fundamental reason why we couldn't.

On the suggestion about OHKLA: Do we even still want to do a big, clustered hybrid rocket? I thought we were planing on using SpaceX launch vehicles? My concerns here are twofold. First, developing a launch vehicle is likely to be expensive, difficult and dangerous. Second, and perhaps more important, such a design would cause extreme ITAR trouble if any work on it was done in the US or Canada. With the other stuff ITAR might apply to, I figure we could successfully argue that it isn't a weapon and could never be useful for one, and that for any given subsystem, something better is probably commercially available. With a launch vehicle, however, that tech is fundamentally applicable to ballistic missiles, and nothing we could do could change that. If we still want our own launch vehicle, I suggest that we develop it entirely outside of the US and Canada, and that we design our payloads such that they could be launched on other launch vehicles without unreasonable difficulty, so as to prevent failing to have the launch vehicle in time from stopping us from doing anything.

One other thought on launch vehicles: If our design is dependant on SpaceX and so on for launches, it becomes directly beneficial for them to help us succeed. If we bring useful and interesting space missions within the reach of smaller countries and corporations, not to mention universities, eccentric wealthy people and random groups like us, they stand to gain as a provider of cheap launch services. Likewise, the economies of scale that such a "space rush" would allow would probably bring down launch costs, making it even more attainable for more groups, and so on, until it starts to reach the actual limits of the technology and SpaceX's desired profit margin. That same sort of end result would, of course, apply if we built our own launch vehicles, perhaps even to a greater extent, but  we wouldn't have the initial boost that possible support from SpaceX could give us. Anyway, we'd still have to see if they expressed interest in this. They are sending someone to SpaceUp, so I suppose I could ask in person.

Main work groups: Propulsion (booster), Spacecraft Engineering, Computer Systems, Navigation and Guidance (software)

7:42 pm
February 7, 2010


Luke Maurits

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Your plan with regards to the unmanned stuff sound great.  If we do go with this approach we should definitely make a big, explicit deal about maximising technology sharing between the CM and unmanned stuff.  As much as possible they should use the same batteries, communications and general computing hardware, software, everything.  Not only does this minimise the amount of extra work involved, but it gives us an opportunity to test how this stuff works in space a bit in advance.  I would feel much less nervous during the first manned launch of the CLLARE CM if I knew that identical, or "genetically related", hardware/software had been flown on unmanned satellites before.  Curiously enough, nobody has ever done this approach before, as far as I know, which is yet another point of uniqueness in our favour.

Re: big, clustered hybrid launchers: I was under the impression that this was still on the board for the smaller CLLARE configurations.  The full blown lunar landing stack has been more or less designed around the Falcon 9, but the smaller stacks are a little more up in the air.  I've learned that an improved version of the Falcon 1 is planned, the Falcon 1e, which will have a LEO payload of 1000 kg, so that would be a possibility for CM+OSM launches if things turn out a little lighter than planned.  I have no idea what we would use, commercially speaking, for a suborbital CM launch, and the circumulnar stack is a little up in the air too, although a Soyuz rocket may suffice.  We also need to think about what commercial options we might have for launching low-mass satellites.  Basically, I think we should use commercial launch vehicles where we can and when it makes financial sense, but it would be nice if we were developing our own, independent launch vehicle technology in parallel, so that we were not dependent on external groups and so that we could do launches cheaper, with more control over things like insertion altitude/inclination.  I guess the ideal would be that one day we would do 100% of our own launches, but during the long, long time before we get there we will use our launch vehicles where we can and use the cheapest commercial alternative otherwise.

That said, your ITAR concerns are valid, although ruling out the US and Canada would be quite restricting.  I'll look into whether or not Australia has an ITAR equivalent.  If not it may be a sensible choice, since there is plenty of sparsely inhabited desert in the middle of the country where launches would be relatively safe.  There's even a small, government-owned rocket and missile testing range in the desert part of my state that I guess we may conceivably be able to use/hire.

As for your final comments about SpaceX…did you leave something out?  You explained why it would be beneficial to them for us to succeeed (and I agree), and then finish up saying "we'd still have to see if they expressed interest in this", apparently without explaining what "this" is.  Did you have some kind of official partnership in mind?

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

1:00 am
February 8, 2010


brmj

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I like your thoughts about using the unmanned stuff for testing as we go. If we wanted to test something like our full landing configuration, we could even deploy supplies for a short-term base with an unmanned derivative of the lander. Once again, though, we ought to be minimizing project bloat and the amount of separate launches. Each launch may be cheap as spaceflight goes, but we are still talking $50 million for a full stack, plus the payload.

The rockets: All right. You rais esome good points. One thing to consider is the fact that the benefits of a highly scalable modular booster scale with how many configurations it is used in. Not a huge thing, since complexity scales similarly but with a lower constant as far as I can tell, but it is worth thinking about. I would be unopposed to developing our own booster architecture, as long as it didn't sap too much effort from the rest of the project and we maintained the option of using commercial boosters in case our booster design lagged behind. I am concerned, though, that it would prove too difficult to be feasible while also working on our other stuff, unless we got some serious funding. Perhaps it would be a bit easier if we could base as much as possible off of the Copenhagen Suborbitals' HEAT design. As for the specific boosters you mentioned, I think a Falcon 9 might also be suitable for our circumlunar missions, considering that they cost less to launch when launched with that kind of load and we would save some work by having to design one fewer payload adapter and interface. Australia for booster development: I see no problem inherent in this, if you guys have no ITAR.

As for your final comments about SpaceX…did you leave something out?  You explained why it would be beneficial to them for us to succeeed (and I agree), and then finish up saying "we'd still have to see if they expressed interest in this", apparently without explaining what "this" is.  Did you have some kind of official partnership in mind?

I actually wrote exactly what I intended to, but it was insufficiently clear. Basically, since everyone involved stands to benefit I was thinking some form of partnership or sponsorship might be appropriate, though we'd need to make sure we didn't get too locked in and that a partnership didn't infect our stuff with their patents without a perpetual, irrevocable and royalty-free license if there was technology sharing involved.

Main work groups: Propulsion (booster), Spacecraft Engineering, Computer Systems, Navigation and Guidance (software)

2:35 am
February 8, 2010


Luke Maurits

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I absolute agree we should try to reduce project and launch bloat, with the qualification that these are actually good if they can lead to a source of income, i.e. if we can sell module space on unmanned satellites or probes and thereby finance CLLARE then I say the more launches of those the better.

The more I think of it, the more the proposal just seems to make sense.  If we aim to have the CM basically be our unmanned satellite frame bolted onto a pressure vessel with life support wrapped up in a heat shield, then the additional unmanned project adds minimal extra work and gives us the opportunity to test how our off-the-shelf hardware approach works in space much, much sooner and cheaper than the alternative of testing it via an unmanned CM flight.  This advantage combined with a potential revenue source selling satellite module space makes it a pretty compelling overall approach.

As for rocket options: the circumlunar stack has a fuelled mass of about 3700 kg, i.e. just a little more than a third of a Falcon 9's capacity.  Falcon 9 launches are cheaper if you use less than 80% of the payload ($45 million, I think), but we're still paying for 8000 kg and using less than half of it.  Possibly we could share the launch with another project (CSTART or otherwise), although external groups may be nervous about sharing a fairing with a third party LH2/LOX tank.  I absolutely agree that basing our hybrid cluster designs of HEAT is a good idea.  In fact, ideally, after Copenhagen Suborbitals achieve their goals and are looking for something else to do, they may decide to help out with our cluster.

On the basis of some brief preliminary googling, I don't think Australia has an ITAR equivalent.  I've realised, however, that Australia would make a lousy place to actually launch from, given how far it is from the equator.  We could always construct the boosters in Australia and ship them somewhere nearer the equator for launch, but this increases costs and also raises the problem of wherever we launch potentially having restrictions on importing launch vehicles.  Lousy laws!

As for SpaceX partnership: I would have no objection to this (providing the patent related concerns you mention are dealt with satisfactorily), but, much like Rocket's suggestion of getting funding from NASA, I sincerely doubt that we have the credibility, just yet, to pull either of these off.  Still, it can't help to ask at SpaceUp if the opportunity arises and you get a decent vibe about it.  I wonder to what extent a single SpaceX employee at a conference could give much of an authoritative answer, though.

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

6:07 am
February 8, 2010


Rizwan

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Post edited 6:08 am – February 8, 2010 by Rizwan


I think that currently we shouldn't be adding a complete LV to the project stack, we will end up spreading ourselves too thin.

Apart from that building a LV has its fair share of problems; laws, safety, workspace etc. Using a commercially available launch vehicle seems to be the best bet for now. It eliminates quite a few problems also we might be able to get an expert opinion on the lander and CM.

As for OHKLA, I believe this project should give us a idea about creating a LV but the main goal with this project should be propaganda, slap in a reddit logo and a couple of other sponsors on the rocket, attach a camera, do a live web-cast of the launch and see the open source community stroke its ego. If we are able to pull this off within the second anniversary of the project we would have definitely accomplished more than something. Any cost estimates for OHKLA?

I agree with unmanned craft but wasn't this our plan from the beginning? That we would do a few tests before the final manned mission? So isn't an extendable unmanned craft included in that by default?

8:08 am
February 8, 2010


Luke Maurits

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Post edited 8:09 am – February 8, 2010 by Luke Maurits


Rizwan said:

As for OHKLA, I believe this project should give us a idea about creating a LV but the main goal with this project should be propaganda, slap in a reddit logo and a couple of other sponsors on the rocket, attach a camera, do a live web-cast of the launch and see the open source community stroke its ego. If we are able to pull this off within the second anniversary of the project we would have definitely accomplished more than something. Any cost estimates for OHKLA?


I agree that OHKLA would be a fantastic piece of propaganda and a huge achievement, but I don't think it would be any less of these things if it were the first milestone of a long term project to build a full scale booster, as opposed to a one off project.  In fact, arguably it would be more exciting for the open source community because it would be the first step in a long and awesome road.  Of course, it would already kind of be the first step on such a road because presumably after it we would start a second project that was just a bigger version of OHKLA.  Rather than defining a new project after each launch (eating up project names and Wiki namespaces, etc), why not just have one cohesive long term project from the start?

Rizwan said:

I agree with unmanned craft but wasn't this our plan from the beginning? That we would do a few tests before the final manned mission? So isn't an extendable unmanned craft included in that by default?


Yes, we have always planned to do simple, unmanned launches before launching any of the CLLARE hardware, but currently (i) there is nothing to make this clear anywhere on the website/Wiki (and, as we know, it is a very common comment to hear "you should do something simpler first) and (ii) no details on what this will look like.  If we are more explicit about this as a separate project we can emphasise the technology sharing between it and CLLARE.

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

3:27 am
February 9, 2010


Luke Maurits

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Some more thoughts: Suppose we decide not to have a clustered hybrid booster project on the books (I am coming around to this line of thinking as I consider more the huge legal hoops we will have to jump through for it to remain open source).  This immediately causes an existential crisis for OHKLA.  The reason we started OHKLA in the first place was because we were planning to build a large clustered hybrid booster, and we wanted experience with hybrid rockets.  No large clustered hybrid = no need for experience with hybrid rockets = no need for OHKLA.

This means that if we want to look like we're going about organising CSTART in any kind of rational manner (and I submit that we absolutely do if we want people to take us seriously) we either (i) abandon OHKLA or (ii) come up with a justification for it.  Presumably nobody wants to do (i) (I don't!) so we need a justification for OHKLA.

This is not just to make us look sensible, it will also influence design decisions for OHKLA.  If we know that we want the technology used in OHKLA to be recyclable for <Project X> later, then that might help us make some choices.  E.g. if we knew that we were going to strap OHKLA rockets to the sides of unmanned satellites to put them into high orbits on on transplanetary trajectories, that might tip the scales in favour of N2O as an oxidiser instead of LOX because non-cryogenic oxidisers are easier to store in space.  Purely an example but I think I've made my point.

So this means we either do have a large clustered hybrid booster project or we come up with another good reason for OHKLA.  "Propaganda", while important, is probably a poor sole-justification for OHKLA because it gives no guarantee that the experience and technology OHKLA produces will be worth having.

Obvious justifications I can come up with are:

  1. If we have some kind of suborbital research project, OHKLA could be a part of that.  This would involve us figuring out a decent sized list of useful experiments one can do with suborbital sounding rockets, figuring out what kind of constraints these experiments place on the overall project, and then making sure OHKLA is designed so that it is a logical step in that direction.
  2. If we have an unmanned satellite project, then we may want to (as discussed) use hybrid rockets for putting them into very high orbits, etc.

Thoughts?

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

7:46 am
February 9, 2010


Rocket-To-The-Moon

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I think that we can justify it as nothing more than a team building exercise. I believe that we should pitch it at SpaceUp as such and actively invite people to join the team. It will give us experience in bridging the online/offline aspects of the project and will be an overall learning experience in how to work together.

Plus being the third "amateur" rocket in space would just be awesome. I have never been ashamed of a bronze medal.

Completely offline from 8-14 March. Main Workgroups: Propulsion & Spacecraft Engineering

9:26 am
February 9, 2010


brmj

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I've got an idea for a direction we could head with OHKLA. Though we can use commercial options for pretty much everything else, I doubt there is anything comercially avaliable for largeish suborbital payloads. Also, a sounding rocket is a cheap way to test components for how they perform in space. My thought is that OHKLA becomes a research project and later becomes important in testing components for the rest of our stuff, then something we base off of OHKLA (or directly off of HEAT, if that looks more apealing) handles our suborbital flights. This would still have some of the same legal issues, but presumably not to the same degree. Launching paid research cargos, for example, and eventually suborbital space tourism, could also be an important early funding source.

If anyone knows of a comercial option for our suborbital option, I would advise that we use that. As it is, I know of no such option, though perhaps we could partner with the Copenhagen Suborbitals for this or contract it out to them.

Main work groups: Propulsion (booster), Spacecraft Engineering, Computer Systems, Navigation and Guidance (software)

9:33 am
February 9, 2010


Luke Maurits

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Okay, so I've got the fairly strong impression that there is not wide support for creating a formal LV project by breaking the Selene concept off of CLLARE and absorbing OHKLA.  That's fair enough.

In that case, do we agree to formally abandon Selene and make CLLARE a commercially launched project?

Are people generally happy to keep OHKLA around just for its own sake?

I haven't got too clear of a signal on how we feel about creating a formal unmanned satellite project and committing to technology reuse between it and CLLARE.  Can people give specific yes/no answers on this?

To be honest, even I have gone off my earlier idea of rebranding CLLARE as a "mere" manned spaceflight project, although I do still rather like the idea of giving the CM a separate, catchier name.  How did people feel about that?

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

9:40 am
February 9, 2010


brmj

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In that case, do we agree to formally abandon Selene and make CLLARE a commercially launched project?

I'm in agreement.

Are people generally happy to keep OHKLA around just for its own sake?

I suppose, as long as we make sure the end result is useful for component testing, for example.

I haven't got too clear of a signal on how we feel about creating a formal unmanned satellite project and committing to technology reuse between it and CLLARE.  Can people give specific yes/no answers on this?

Yes, I am in favor of this.

To be honest, even I have gone off my earlier idea of rebranding CLLARE as a "mere" manned spaceflight project, although I do still rather like the idea of giving the CM a separate, catchier name.  How did people feel about that?

I suppose I would support a catchier name. I have no strong feelings on this topic.

Main work groups: Propulsion (booster), Spacecraft Engineering, Computer Systems, Navigation and Guidance (software)

9:40 am
February 9, 2010


Luke Maurits

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brmj said:

I've got an idea for a direction we could head with OHKLA. Though we can use commercial options for pretty much everything else, I doubt there is anything comercially avaliable for largeish suborbital payloads. Also, a sounding rocket is a cheap way to test components for how they perform in space. My thought is that OHKLA becomes a research project and later becomes important in testing components for the rest of our stuff, then something we base off of OHKLA (or directly off of HEAT, if that looks more apealing) handles our suborbital flights. This would still have some of the same legal issues, but presumably not to the same degree. Launching paid research cargos, for example, and eventually suborbital space tourism, could also be an important early funding source.

If anyone knows of a comercial option for our suborbital option, I would advise that we use that. As it is, I know of no such option, though perhaps we could partner with the Copenhagen Suborbitals for this or contract it out to them.


I think the suborbital research project is a really good direction to go in.  Do we want to rename/rebrand OHKLA and have the current OHKLA plan be the first milestone of that larger project, or are we happy to leave OHKLA as it is and create a new, more general project after it?  If we go with the latter option, would we feel comfortable at least giving the future project a prospective name and one paragraph blurb, so that we can produce a "CSTART roadmap" that shows where things are going?  Such a roadmap would be a very nice thing to have.

I am quite happy with contracting the CS guys to launch our CM if they are up for it when the time comes (assuming, of course, the Tycho Brahe flies well!).

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

9:48 am
February 9, 2010


brmj

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Luke Maurits said:

I think the suborbital research project is a really good direction to go in.  Do we want to rename/rebrand OHKLA and have the current OHKLA plan be the first milestone of that larger project, or are we happy to leave OHKLA as it is and create a new, more general project after it?  If we go with the latter option, would we feel comfortable at least giving the future project a prospective name and one paragraph blurb, so that we can produce a "CSTART roadmap" that shows where things are going?  Such a roadmap would be a very nice thing to have.

I am quite happy with contracting the CS guys to launch our CM if they are up for it when the time comes (assuming, of course, the Tycho Brahe flies well!).


I have no strong feelings on the issue of rebranding OHKLA as part of a larger project, but I think I am slightly against it. It would be a bit of work to scour our site for references to OHKLA and change them all, and though OHKLA then becomes part of a larger effort, it won't be directly built upon in the way the the CM will be built upon for our more complicated missions. If we go with this option, I think your suggestion about giving it a name and a blurb is a very good idea. The roadmap would indeed by a very nice thing to have.

Main work groups: Propulsion (booster), Spacecraft Engineering, Computer Systems, Navigation and Guidance (software)

10:03 am
February 9, 2010


Luke Maurits

Adelaide, Australia

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Okay, I think the roadmap is a very good and important idea.   It should satisfy my need to feel like we have a clear big picture.

In this roadmap OHKLA will lead to an as-yet unnamed project which is focused on flying suborbital payloads of a decent size.

Our unmanned satellite project could lead to a project for orbital probes of the moon / planets?

CLLARE could lead to…well, lots of things.  A more useful 2 or 3 crew craft that can properly dock with things.  A space station of our own (the Falcon 9 heavy would be wonderful for this, and we could follow Bigelow Aerospace's lead with inflatable structures)?  A Mars mission?

Obviously the future projects could have levels of certainty associated with them.  E.g. the suborbital payload testing project coming out of OHKLA would be fairly certain.  A Mars mission would have gigantic question marks all over it.

If we get a few more affirmative answers on the unmanned satellite question that should be sufficient grounds to start drawing up a roadmap like the above.

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

4:02 am
February 10, 2010


Luke Maurits

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I don't mean to put pressure on any of those directors who have not yet given an explicit yes or no on the unmanned satellite project idea, but in the interests of making the scope and purpose of this proposed project as clear as possible, I've created a Wiki page for "Project X" (which can be renamed or deleted later depending on how things go) which gives a two paragraph summary of how I envision the project.  Those who are in favour of seeing this project become official can feel free to edit the page if you think there are good changes to be made.

Starting a new TA job next week, might be busy for a while! Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.

5:43 am
February 10, 2010


rpulkrabek

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Post edited 5:55 am – February 10, 2010 by rpulkrabek


Yes.

Let's do it. For one, I have the bulk of my work put towards OHKLA, and I have been enjoying the work and the learning experience. I am also keen on results and data. It seems do-able that we can send a rocket to space and gather some sort of data. This can then provide a great start towards satellites and such.

I also say we continue to use the OHKLA name and can then use OHKLA in a currently unnamed project.

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