Oh no boys,
You'll have to phone NASA.
It's been a lively couple of days down at the Special Projects Bureau, with the first of our Rocketry Experimental High Altitude Barosimulator (REHAB) experiments, designed to determine whether solid propellant rocket motors will fire under simulated high altitude conditions. Click here for a bigger version of the LOHAN …
You'll have to phone NASA.
Instead of relying on a single Copperhead, is it possible to insert (say) three into the propellant and fire them all at the same time.
What about one or more igniters cast in the engine using something like crushed rocket fuel and some sort of weak binding agent?
Fancy crushing some rocket fuel? I'm not sure I do.
However, the idea of casting the igniters into a block of something fuelly, pressing into place, and then popping a smidge of silicone outside that seems rather appealing. Then the silicone seal is against something solid, and there's no pressure differential across it until you press "go!".
Aye, bigger hammer.
Was there any sign of contact in the fuel? Had it caught at all? Any charring?
A small bit of magnesium ribbon wrapped around the Copperhead would generate a nice sustained heat for a second if the heat of the propellant in the engine is an issue, but it would need a source of free oxygen for it to burn. Sort of a secondary igniter. I am trying to think of a powder that might do the trick. Finely powdered ferrous oxide?
Any other suggestions?
If you want to use finely powdered ferrous oxide, you may as well go for thermite. But all this talk of adding home-made rocket fuel to the combustion chamber seems dangerous to me - let's just see what happens with a simple burst plug first.
I bigger actually better?
If ignition requires air to transfer heat from the head to the fuel there is no way it will work. What you need is direct heat impingement from say a small motor with integral igniter if there is such a thing. Looks like you might be stuffed.
It is a good job you did a ground test.
Never mind mucking about with rocket fuel - just get hold of a set of waterproof matches, and slice them up with a razor blade. For glue, a little melted wax should do the job.
Not sure a sacrificial silicon seal would be strong enough, it's gonna be seeing close to 14 pounds per square inch which will probably mean it'll just pop off before you get a chance to fire the motor. Maybe a weakened perspex disc bonded to the nozzle would be better but if it is too strong it could make the motor go bang rather than burn, bit of a balancing act getting it right.
The lack of strength of a silicone seal crossed my mind, too. We need to mull this one for a bit, to find the best solution.
Even if the seal does not pop off, the chances are that the air will slowly leak from inside the motor. The body of the motor may not be leak-proof in the first place, and as the temperature drops imperfections of the sealing will be getting worse. Even it works in REHAB it may fail at launch as it will spend hours in near vacuum and in the cold.
I would rather try to find some substance that could act as "ignition booster" to put between the igniter and the "main" fuel.
The air leakage is certainly an issue. Reading the comments today, I'm inclined to agree that we first have to try to give the igniter some more oomph.
We have suffered the same problems as you with low pressure ignition. The flame front from the burning igniter products dissipates too quickly (thanks to the low ambient pressure), before it's had enough time to transfer enough thermal energy into the propellants to get the party started.
You can either plug the motor (would have to be done very well to hold a seal for the couple of hours of balloon ascent) or modify the igniter. We have in the past used some special sauce that was a bit of pyrogen dissolved in water (which makes a paste) with aluminium powder and iron oxide powder (rust). This paste (I call it rocket bbq sauce, but I am silly) can be applied to the igniter head in several layers (dip, let dry, dip, let dry, etc for 5 or 6 times, like coats of paint) and then will produce a lot more energy, the thermiting ali and rust powder especially are in liquid phase (molten iron) rather than gaseous as they react, which helps with gets you round the hot gases dissipating in the low pressure. You'll get molten iron being sprayed onto the inside of the motor. This will get it started.
The flame front from the burning igniter products dissipates too quickly (thanks to the low ambient pressure)
Rather the inverse. AIr conducts heat (by convection, mostly). Lack of air means lack of convection means lack of heat transfer: the principle of the thermos flask.
I'd say the igniter has to be well bonded to the rocket fuel, ideally with some goop that burns (and fairly easily ignites) while supplying its own oxygen.
I love the SPB articles & experiments. Everything about it is classic El Reg. It's nice to see some real science & technology news instead of opinion pieces.
Also, can citizens get SPB shirts? I'd like to purchase a few if it helps fund LOHAN.
Well done to the SPB team, for finally bringing this experiment together and getting us some excellent results. We wanted to know if the rocket would burn at low pressure, and now we know. This is a milestone, not a setback.
Worth trying a 1 Ohm small resistor which will get hot and blow fairly pronto - may be enough to start the reaction when the tiny copperhead thingy had already blown open circuit?
1 ohm might be a little too low. It would probably burn out before it can inject enough heat.
Hackaday recently featured a post about using resistors to launch fireworks: http://hackaday.com/2012/07/04/a-resistors-fiery-death-used-to-launch-fireworks/
I'm not sure however that these rockets are launched by just heat or if there is more at play here.
To ignite the propellant components must first be vapourised, then the vapours should mix to form fuel, only then the ignition is possible. The igniter will vapourise the propellant even at low pressure but then the gases will be vented immediately before they have a chance to form fuel mixture.
I should think a simple plastic or rubber plug in the igniter hole would be enough. It should not be gas-tight and be able to withstand the full pressure differential. In fact, I'm afraid that if it will be so strong it will blow up the motor. The task of the plug will be to prevent just enough gas escaping the motor to initiate the burn...
Probably all true from Vladimir above, I'm no expert on this but bear in mind that when you fit the plug you'll be doing so under normal atmospheric pressure (close to 1 bar) but you'll be evacuating the chamber to around 20 mbar pretty soon afterwards. You'll want the plug to be loose enough or porous enough that the ambient pressure air inside the motor can be extracted along with the surrounding air.
There is also the question of how the copperhead igniter works... does it try to eject a small amount of burning gas in the general direction of the motor's fuel core? If so, it might be that the burning hot gas dissipates too fast in the 20 mbar environment (and in doing so, cools down too fast).
I'd think that if you laid an elongated horseshoe of manganin resistance wire physically inside the hole that runs through the rocket fuel core, then you could energise that. It would heat up to red or orange heat if you got the sums right, and being in contact with the rocket fuel *ought* to set it off.
What about testing the motor in an environment that lacks any O2 i.e. in a an airtight pit that's filled with dryice. They you could rule in(or out) the lack of oxygen being the issue rather than the low pressure.
It's not lack of O2 that's the problem; the fuel incorporates its own O2.
Caveat: I have a lot of experience igniting engines, but just the black-powder type, not composite engines.
That being said, in my position of knowing just enough to be stupid, I have a suggestion.
Estes now ships little plastic igniter plugs with its engines, but they didn’t 20 years ago. Back then I found out, through plenty of trial and error, that physical contact between the fuel and igniter is essential to ensure reliable ignition. (Using the plastic plugs they ship now, I have *never* encountered an igniter firing without lighting the engine.) My solution was to place the igniter in the engine and stuff a wad of tissue paper tightly in place, and then capping the whole deal with adhesive tape.
Now, of course, the physical construction of the composite engines you use here (and the fragility of the igniters) make that approach impractical. However, this might work:
1. Before assembling the engine, thread the igniter through the ignition slot such that the end protrudes out the far side.
2. Place a small wad of tissue at or slightly below the igniter chemicals on one side of the igniter; pull the igniter and paper into the fuel. The chemicals should be held firmly against the AP composite propellant.
3. Assemble the motor really carefully to avoid wrecking the igniter.
4. Apply burst cap silicone and let dry.
This should (a) maintain nearly ground-level air pressure and (b) ensure physical igniter/fuel contact.
Ah - you think you want maintain circa 1 bar pressure inside the motor do you? I was assuming (see post further up) that the pressure plug was just to cause pressure to rise and stop gas being lost as just the first couple of grams of fuel ignited.
If you rely on holding 1 bar pressure in the motor, it might work in REHAB but would be hard to maintain those conditions under a helium balloon that might take an hour to reach launch height.
If you have ever looked at the CCTV footage of the ignition phase of a LOX rocket, you'll notice an industrial strength sparkler is used to maintain a strong ignition source. Sparklers are essentially "Thermite" which burns hot enough to melt Iron.
Humor me and try this, take a few Ohio Bluetip or other strike anywhere Matchheads and gently peel the head from the wooden match. Crush them gently and use them to fill the end of the rocket motor nozzle with the ignitor making good contact. That matchhead stuff is typicallly a form of ammonium perchlorate and fuel that burns very well since it is both fuel and oxidizer in one. This "ignitor" MUST contact the rocket motor "Fuel". You can use alot more matchhead than is provided with an "ignitor" so there is way more flame that lasts longer. Then follow the proceedure from "Poor Coco" in covering the materials so they don't fall out.
Before electric ignitors for Estes model rockets were commonly available, we used to make them ourselves using a loop of thin stranded bare copper wire and electrical tape for insulation. We also tried using cannon fuse wrapped with copper wire. We used alligator clips attached to a 120 VAC extension cord and a light switch for power. The wire vaporized, broke the circuit and never even blew the circuit breaker. This ALWAYS provided reliable ignition (even when damp or windy) and worked with car batteries as well. For even more heat, the "Ni-Chrome" heating element wire from an old toaster worked quite well and glowed white hot.
Blimey... You just reminded me of what I used to as a, errm, teenager engaged in making things go bang... (it really was a long time ago).
I'd 'developed' an explosive mixture using potassium permanganate and magnesium powder. For some reason i also had a small supply of used 12 bore cartridge cases (I really can't remember where I got them - the chemicals came from *cough* school).
I used to run a loop of light gauge copper wire inside the case and pack the mixture round it. Then, with a very long cable (enough to reach the bottom of the garden!) I'd connect it up to the 240 ac in my bedroom. Pressing the switch would elicit an almighty bang, a satisfying purple mini mushroom cloud and several very irate neighbours + dogs.....
Ah.... Those were the days!!
Nooo the "fizzy sparklers" are there to ignite hydrogen gas - before it forms pockets inside the rocket and blows the crap out of panels etc., when it ignites.
This is not correct I'm afraid. The sparkers are there to burn off any leaking fuel before the engines start, so it doesn't gather somewhere and explode at some later time.
All the ignition is done inside the combustion chamber itself by the rocket engine. The sparkers play absolutely *no* role in the ignition.
You and I seem to have shared similar aspirations as teenagers. Yes, those were the days indeed, halcyon days of summer blowing up the sandbox with anything that could be made, bought or "liberated". I certainly gave the old man a few gray hairs. I like the purple smoke concept. I doubt any of us will ever have as much fun as back in those days. They'd shoot us all dead on sight today.
Copper pipe and shotgun powder worked best for me. See I had been making my own black powder since I was 11 but never seemed to get the ratios correct. Premade powder worked best. Matchheads came in a close second but were way too energetic for safety let alone the first time I tried it and just cut the head off the match instead of peeling it off (with the wood still below the blue stuff) when the "fireworks" went off, little flaming matchheads also flew all over the back yard and me.
The stuff you were using was almost Thermite (aluminum powder mixed with iron oxide instead of magnesium) but you had the ratios off (not so much potassium permanganate ). An old encyclopedia we had from the early 1900 had all sorts of great recipes for interesting combustibles. If you had added a few drops of Glycerine to the potassium permanganate it would have begun spontaneous combustion which would have made enough heat from the aluminum and rust mixture to melt through an engine block. They used this stuff to weld railroad rails. Your mixture sounds very "energetic"!
We had a great pharmacy that stocked sulphur, activated charcoal and potassium nitrate all of which could be bought by a teen ager with nothing more than a forged note. Mind you they each had to be bought at different times and the excuse for the potassium nitrate was it was for the sausages we were making.
That could never happen today.
BTW, others comments about the "sparkler" being for excess hydrogen doesn't jive. There is NO SUCH THING AS EXCESS HYDROGEN on a NASA rocket engine, If you had any significant leak, the launch did not happen. Yes, there was "Venting" but that happened at the top of the liquid fuel and oxidizer tanks, NOT at the nozzle of the engines.
You ALWAYS have to light the hydrogen BEFORE you open the valve for the oxygen, otherwise the whole thing goes BOOM like a cutting torch will with the wrong gas mix. My old man told me that was what they were for and he should know. He was a project manager for Thiokol and Bell Aerospace during the 60's and 70's working on Saturn, Agena, various ICBM rocket engines (See where I get it from?). There were SEVERAL methods for ignition used back then but on the pad they electrically ignited the "sparklers" then had different ways to ignite the liquid fuel boosters in space for secondary burns (High voltage spark ignition) Lighting the solid fuel boosters involved what amounted to a fireworks "Fountain" of sparks designed to contact a large surface area of the solid fuel inside the booster to get it burning evenly (thus even thrust). You know what happens when there is not "even thrust" combined with leaking O rings.
Nooooo very cold liquid hydrogen is COLDER and DENSER than air, so it sinks from where ever it's venting / leaking from - including things like priming the engines etc... and before they get lit...
As it warms up... it rises and forms pockets of very explosive gas mixes in what ever will confine it.
Rockets are fairly huge, and very expensive and fairly dangerous if they get damaged when full or fuel or when in flight and a few cubic meters of hydrogen / air mix.... underneath the rocket, around the engines, panels, bulkheads etc... and it tends to migrate UP inside of things...
Get a cupful of petrol and spray that around inside an abandoned car - that has all of it's windows, then arrange to have some sort of ignition from some distance or with a time delay (long piece of twisted up news paper going down into the partly open window?)
That is ONLY the volume of the inside of a car - but it will go off with a hell of a bang and it will shake a building 1 block away... "Fucking WHAM"
Hydrogen has a wayyyyyyyyyyyyyyy faster flame speed, and while it's energy density is lower, it's pressure wave is far more intense - if there is enough of it, it will just "shatter" things....
Remember that reactor with the confined hydrogen gas in the concrete containment building in Fukishima?
Granted that there was a lot of it... but Frightened to Death of it....
This is what the sparklers are for - to ignite any hydrogen gas, (or other fuel / oxygen mixtures) so it does not form "explosive pockets of gas" inside and underneath things like the shuttle or other rockets...
I like the video! Very cool.
The commentator comments that your motor is a "100N" motor which I thought might mean that it can generate 100 Newtons of thrust. If so, it would be able to lift 10 kg at ground level, which I think looks a bit optimistic...
Your kitchen scales bears this scepticism out showing a reading of 1797 grams when the motor lights (notice though that for most of the burn, the reading is more like 1400 g). Please note that thrust shouldn't be measured in grams as claimed at the end of the video. Keep thrusts in Newtons please, or you'll likely be headed for an accident.
The scales are actually measuring force, but "helpfully" converting this to equivalent mass assuming normal earth gravity of 9.81m/s². You ought to convert back. If you get a reading of 1797 g (which is 1.797 kg), then that's 1.797 * 9.81 which is a thrust of about 17.6 N
However, 1.4 * 9.81 - i.e. 13.7 N would be more representative of most of the burn time.
[ Additionally, since the motor was sitting on the scales and firing upwards (thrusting downwards) you needed to subtract the dead weight of the motor from the indicated scales-readings before multiplying by 9.81 to get the generated thrust. ]
This brings me back to the original comment. Why is the motor apparently claiming 100 N thrust. It's not even generating a sixth of that. Is the "100N" just an arbitrary part of the model number, nothing to do with the thrust?? Or what?
100Ns = 100 Newton-seconds, which is how rocket motors are rated. Thus, it can produce 100 Newtons for 1 second, or, more usually, 10 Newtons for 10 seconds., or any mathematical combination there-of.
It's a measure of the impulse of an engine:
P.S. It's been a LONG time since I've done much with rocket engines.
That would tie up fairly well. Thank you for that.
Been a genius Pyrotechnica...
Me thinks that the HUGE drop in temperature, like some 80+*C below normal ambient, will soak up enough of the heat from the bridge wire, as it heats up the ignitor compound, and that with the air gap and all between it and the very cold propellant, is enough to quench the ignition process.
Get some enameled copper wire from an electric guitar pickup, polish up a thin toothpick or polished steel wire from a base guitar or electric guitar string core, make a copper wire tail of about 3cm, then wind say 10 - 12 fine pitched turns around the tooth pick - be careful of the tension, too tight and it breaks and too loose and you don't get a neat winding, and you want a little "spring back"...
Then mix a paste of either some flash powder formula, or finely ground black powder whetted with some dilute gelatin in water (weak jelly mix) , and then dip your coil in the slurry.... enough to make a small pellet or rod of powder inside and around the core, then dry it and let it set.
Then use this as your electrically driven bridge wire ignitor.
You need a bigger, slower and longer lasting flash to ignite your very COLD propellant.
Did you attempt to fire the rocket motor again at ambient after the experiment? I only ask because, not knowing the fuel composition, it might be that one of the ingredients or binders that make up the solid fuel sublimates at low pressure leaving a non-viable mix in the combustion chamber. I know it isn't fun just burning through rocket motors (actually it kinda is) but it would be an easy test to see if the life was sucked out of the poor thing.
Fair point. I'll give the AeroTech one a blast...
You might want to look at these:
Yes, some of these are at the top of my list.
One of the concerns with sealing the end of the engine is that too firm of a plug may cause a blowout at the other end of the engine (Been there, done that, got to see the engine flying backwards out of the body of the rocket, whoopsie!).
For that matter, igniting a solid fuel rocket engine (or, for that matter, even a liquid fuel rocket engine) is a study in thermodynamics as well as acoustics. When the fuel ignites, you're going to have a pressure wave radiating outwards from the point of ignition. As more and more of the fuel ignites, the pressure wave may build. It will also reflect off of solid surfaces (other wall of the fuel, nozzle, sealed top end of the engine, etc.), resulting in a constructive interference pattern. The magnitude of this pressure wave can, under the wrong circumstances, build to a value that things give way. It's very possible to either blow out the nozzle, blow out the top end of the engine seal, or even fracture the grain of propellant. Note that you do NOT want to fracture the propellant grain, since this results in an increased surface area, which is where the burning will occur. A fractured propellant grain will cause a more rapid consumption of the propellant, resulting in increased pressures, perhaps even enough to blow out the engine casing (which is VERY bad news).
Thus, before stuffing anything in the void in the center of the solid fuel propellant grain, give some thoughts as to pressure waves, and how they may behave. You not only want to cause a reliable ignition; you want to do so in a relatively gentle manner that does not cause an echoing pressure wave.
There are various propellants and explosives readily available. Unfortunately, some propellants can turn into explosives under the wrong conditions, and you do NOT want an explosive as an ignition assist. For example, black gunpowder is typically regarded as an explosive, so you probably don't want it in the engine. Other propellents, such as nitrocellulose, with a bit of nitroglycerine added as a stabilizing agent (I'm being serious here!), may function as you want. Maybe. But, remember burn rates, pressure waves, etc.
There has been quite a lot of research done on this. Sadly, most of it is classified due to the potential applications to military weapons. Thus, you may have to redevelop some of the theories on your own, and do some experimentation.
On the basis that the problem is due to the low ambient pressure resulting in the too rapid dispersal of the initially vaporised fuel, before it can ignite the rest of the fuel, I started thinking along the lines of using an equalising chamber to maintain pressure in the combustion chamber. For example, imagine two small balloons attached neck-to-neck, with one balloon inside the chamber and the other threaded through the nozzle to the outside, this double-balloon then being inflated to just above ambient ground-level pressure: as the ambient pressure drops both balloons will start to expand, the inner balloon expanding into and filling the combustion chamber and maintaining pressure within it. Once the rocket motor has fired I wouldn't expect it to have problems burning through the balloons as it's got to burn out the igniter wire anyway.
The tricky bit is ensuring an air-tight seal around the ignition wires and the balloon neck as they pass through the nozzle and enter the combustion chamber although as the balloons expand they'll tend to occupy any gaps and improve the seal. Of course, you'd also need to take into account the fact that the igniter wire will have to run around the inflated balloon within the combustion chamber i.e. against the walls which will mean more wire in the chamber than usual.
Alternatively, if you think that the motor would be able to burn through a fine nylon mesh, just stick a small balloon inside the chamber that's prevented from expanding out through the nozzle by a fine nylon mesh placed over the inside of the nozzle opening. However, the same issues re the routing of the igniter wire apply.
Ah, sort of like putting a balloon on the nozzle end of the engine. Interesting! That way, it'll hold pressure in the engine, and have enough capacity to handle small leaks. Plus, once the engine fires, it should blow/burn away from the nozzle quite rapidly. The upper end of the engine will have to be sealed, of course.
There'll need to be a bit of calculation as to how large the balloon can swell to in the reduced pressure of high altitude without bursting itself. But, it is an interesting idea!
I had the same thought when the too-rapid dispersal of gases was mentioned, but what popped into my head was not balloons, but a condom. A balloon would be better due to the tighter neck. Either should burn through quickly once ignition has been achieved.
I'm not sure how much new data it will give you, but have you tried setting off just an igniter? You can probably put the camera much closer and see if it's igniting correctly at low pressure, or if the problem is with the motor.
Were I doing this here in the US, I'd just half-fill the cavity with a little loosely-packed, slow burning double-base smokeless rifle powder, put the igniter in, put some more double-base over it (again: loosely), and then some electrical tape (or Duct tape) over the bottom.
DO NOT USE HONEST-TO-PETE BLACKPOWDER. Or fast-burning stuff like for a pistol.
gave you considered phoming North Korea for advice?
With people doing stuff around their latest rocket, quite close to the countdown time, I got the impression they were going to push-start it.
How about fitting the igniter and then pouring in a little fireworks type powder followed by a squirt of silicone to hold all in place? That should ensure a hotter burn to fire the real fuel and if the plug is allowed to harden even a little pressurisation?
Lighting it is going to be the least of your problems (burst diaphragm). You have very low air density to provide the stability your rocket is going to need, it's not going to be moving fast enough by the time it leaves the launch rod, asymmetry in the rocket's centre of gravity will cause it loose stability and tumble. According to research I've read, at 100,000ft you need 71.6x the travel distance before your fins are going to provide the stability that you get at sea level. The speed of sound is lower at that altitude, 35.5meters per sec @ 100,000ft so your rocket needs fins and nose cone designed for super sonic flight too. I guess the long and short of it is spin the rocket up to get stability, design it for supersonic flight and to overcome transonic drag, shoot it straight up _through_ the balloon.