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3:27 am July 1, 2010
| Luke Maurits
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In my post a few days ago discussing a more cohesive and structured set of proejcts for CSTART, and part of that (which so far has not drawn any criticism) was expanding OHKLA into a multi-staged hybrid rocketry project, looking kind of like this:
- Stage 1: Minimalist Suborbital – carry 5 kg of payload (in addition
to all onboard systems) above 100 km (this stage is what OHKLA
currently is).
- Stage 2: "Useful" Suborbital – carry larger payloads on higher
suborbital trajectories, possibly with control of the trajectory, i.e.
control of time in weightlessness – this could be a revenue raiser by
selling scientific payload space.
- Stage 3: Manned Suborbital – carry a < 1000 kg single-person
minimalist spacecraft above 100 km (an Ansari X-Prize capable rocket).
This is to support Simple Manned Spaceflight Project below.
- Stage 4: Minimalist Oribtal – put a 1U, 2U or 3U Cubesat into orbit.
- Stages >5: Useful Orbital – something on the scale of Falcon 1? Higher? OTRAG-style cluster?
Today I learned that SpaceDev, the company who built the N2O/HTPB hybrid engine for SpaceShipOne, once had a program rather like this, called Streaker. They're not pursuing it anymore (they seem to have absored some of the ideas into another project of theirs), but you can still find some info about it on the web – here's an AIAA paper on the idea.
The Streaker family of vehicles were numbered with a two-part decimal system, kind of like software, which I actually rather like. Streaker 1.0 is a single-stage suborbital rocket, for instance, whereas Streaker 1.1 is a minimalist orbital vehicle – it's a small hybrid second stage stacked on top of a Streaker 1.0. At a higher end of the spectrum, Streaker 3.1 is three Streaker 1.0 boosters strapped together with the second stage from Streaker 1.1 on top. Basically they have a wide family of gradually more capable vehicles, with lots of common infrastructure between them (the Striker 1.0 suborbital rocket is the basic building block of the whole family, it seems).
I think it would be really neat to have this kind of plan and numbering scheme for our hybrid rocket project. The current OHKLA project – a bare bones suborbital sounding rocket – could be PROJECTNAME 1.0 (we could have a poll to choose PROJECTNAME) and then we could work forward from there with more ambitious projects, eventually making our way to orbit with 3.0 or some such. Even if actually getting that far is years away, having a simple plan that shows a steady progression building on experience and technology as we acquire it will make the whole thing seem more purposeful.
If people like this idea we can use this thread to plan a progression.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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5:02 am July 1, 2010
| rpulkrabek
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I think the numbering scheme makes sense. There's no harm, and it's also informative for how far it has been developed. As for the project name, what's wrong with the current OHKLA name? Is it just because if it were to be developed into stage 5 that it is no longer just an Open Hybrid Karman Line Attempt?
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5:16 am July 1, 2010
| Luke Maurits
| | Adelaide, Australia | |
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| posts 1483 | |
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Precisely that – my only worry with the name OHKLA is that the "Karman Line Attempt" part of the name really sounds like the entire point is a just-over-the-edge suborbital rocket, which isn't really suitable for a program of rockets more like Streaker, where the eventual goal is, presumably, the heaviest lifting orbital hybrid we can develop.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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5:31 am July 1, 2010
| rpulkrabek
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I have become quite attached to the OHKLA name, but after all, it is just a name. What's important is the development.
If the community prefers to have the numbering scheme and a new name, a poll is the way to go. Perhaps, something similar to the way the motto was chosen.
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6:11 am July 1, 2010
| Luke Maurits
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You could always try to come up with something else OHKLA could stand for which would make more sense in the new context. :p
I agree it's not really that important, and if most people are strongly attached to OHKLA we should keep it – we could always just stop saying that it stands for Open Hybrid Karman Line Attempt and treat it like a proper name, perhaps switching to Ohkla.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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8:12 am July 1, 2010
| joe.haydu
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We could alway refer to the underlying design as Projectname 1.0, 1.1, etc, and call the actual vehicle OHKLA, just like ships have classes and actual names.
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1:16 am July 2, 2010
| Luke Maurits
| | Adelaide, Australia | |
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| posts 1483 | |
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joe.haydu said:
We could alway refer to the underlying design as Projectname 1.0, 1.1, etc, and call the actual vehicle OHKLA, just like ships have classes and actual names.
That's not a bad idea, and in fact there is something like this in the Streaker project. The Streaker 1.0 suborbital rocket is generally referred to by itself as the "Common Core Booster" (CCB). We could always refer to the Projectname 1.0 rocket as Ohkla.
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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3:30 am July 2, 2010
| Luke Maurits
| | Adelaide, Australia | |
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| posts 1483 | |
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Post edited 10:35 pm – July 2, 2010 by Luke Maurits
A rough sketch of a possible program structure:
- Ohkla 0.1: A 1/4 scale test model of Ohkla 1.0
- Ohkla 0.2: A 1/2 scale test model of Ohkla 1.0
- Ohkla 1.0: The result of the current OHKLA project – minimum suborbital sounding rocket
- Ohkla 1.x: Improvements of and extensions to Ohkla 1.0. We could probably fit on a second stage powered by a completely off-the-shelf hybrid engine for hobbyists?
- Ohkla 2.0: A suborbital "workhorse", which we can sell payload space on to scientists, etc.
- Ohkla 3.0: A larger suborbital rocket for launching a minimal manned capsule – basically our version of Copenhagen Suborbital's HEAT
- Ohkla 4.0: Our most basic orbital rocket – 3 Ohkla 2.0 rockets strapped together with a smaller final-stage rocket atop the center one. The two side Ohkla 2.0 rockets burn together as the first stage, then the central rocket burns as the second, and the final-stage as the third.
- Ohkla 4.1: Same arrangement as above but the central rocket in the group of 3 is an Ohkla 3.0 rocket.
- Ohkla 4.2: Same arrangement as above but all rockets in the group of 3 are Ohkla 3.0 rockets.
Some explanations:
- I've called everything "Ohkla x.y" for the sake of having a consistent naming system – the name can obviously be whatever it wants.
- We haven't discussed actually flying 1/4 and 1/2 scale version of OHKLA before, just static testing 1/4 and 1/2 scale engines, but it occurs to me that we really have no more experience with flying than with engine construction at this point, so we should probably practice flying earlier on too. Unless people have good arguments why not?
- I think Ohkla 2.0 could basically just be a scaled up version of Ohkla 1.0. I've found HDPE rods in 400 mm diameters now, which will be significantly more massive than what Ohkla 1.0 uses. If we combining this larger fuel grain with a better mass fraction (at this stage of the program and on this larger scale we could probably justify switching steel to aluminium) we should be able to lift heavier payloads on higher trajectories. A cold gas RCS solution could give us some trajectory control, so that we can control the total time spent in weightlessness according to customer requirements.
- I'm not sure if Ohkla 3.0 could just be another scale up – The CS HEAT rocket is 600 mm in diameter, and I haven't been able to find HDPE rods of that size. I'm not sure if we would need to go quite as large as 600 mm – I think HEAT has a lower Isp than our plans – but we may still be exceeding the size of readily available HDPE rods. This would mean either melting some HDPE down and casting our own grains (and if we were to go to that much trouble we may as well switch to HTPB) or, say, using a cluster of 2 or 3 smaller rockets. Something to consider much further down the road, though.
- The central concept for the 4.x series – three large rockets strapped together as the lower two stages – is basically taken directly from the Streaker 3.x concept.
Thoughts?
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Main CLLARE workgroups: Mission Planning, Navigation and Guidance. I do maths, physics, C, Python and Java.
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